Post on 11-Feb-2022
MS-364, BERNARD LINDENBAUM VERTICAL FLIGHT RESEARCH COLLECTION
Collection Number: MS-364
Title: Bernard Lindenbaum Vertical Flight Research Collection
Dates: 1918-1999 (Bulk 1945-1980)
Creator: Lindenbaum, Bernard, 1916-2002
Summary/Abstract: Bernard Lindenbaum was an aeronautical engineer with the Air Force Flight Dynamics Laboratory (AFFDL) at Wright-Patterson Air Force Base in Dayton, Ohio from the mid-1940s until the mid-1970s. During his time with the laboratory, he was involved in the research and development of many types of vertical take-off and landing aircraft (VTOL) including the Avro “Avrocar,” a number of Sikorsky helicopters, the Vought XC-142 tilt wing, and many other similar aircraft. His collection of vertical flight research material contains numerous technical reports chronicling the development of military helicopters and V/STOL aircraft, a variety of conference reports and notes, many NACA/NASA technical notes, blueprints of several V/TOL aircraft, 190 reels of 16mm film and 10 VHS tapes of helicopter and V/STOL testing.
Quantity/Physical Description: 126.3 linear feet
Language(s): English
Repository: Special Collections and Archives, Paul Laurence Dunbar Library, Wright State University, Dayton, OH 45435-001, (937) 775-2092
Restrictions on Access: There are no restrictions on accessing material in this collection.
Restrictions on Use: Copyright restrictions may apply. Unpublished manuscripts are protected by copyright. Permission to publish, quote or reproduce must be secured from the repository and the copyright holder.
Preferred Citation: (Box Number, Folder Number), MS-364, Bernard Lindenbaum Vertical Flight Research Collection, Special Collections and Archives, University Libraries, Wright State University, Dayton, Ohio
Acquisition: The collection was donated by Stephen Lindenbaum of Marietta, Georgia, son of Bernard Lindenbaum, on March 24, 2003.
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Separated Material: Aviation books and Vertiflight Magazine, received with the collection, have been cataloged and placed on the shelves in the Special Collection and Archives Reading Room.
16 mm film contained in the collection is located in the Special Collections and Archives Film vault located in the basement of the Wright State University Medical Sciences Building. Researchers should call in advance to view the film.
Additional Sources: Lindenbaum, Bernard, “V/STOL Concepts and Developed Aircraft, Volume I: A Historical Report (1940-1986), Universal Energy Systems, Inc., Dayton, Ohio, Report Number A973571, 26 Jun 1986.
Processing Information: This collection has been minimally processed and minimally organized. Each box has been fully inventoried and a list of items included in the container listing. No effort was made to replace folders with acid-free folders and reports remain in their original cover.
Processed by: Ed O’Shaughnessy (Archives Volunteer) and John Armstrong, 2010-2011.
Arrangement: The collection is arranged in twelve series.
Series I: Rotary Wing Handbook Series II: NACA & NASA Reports Series III: AVRO Avrocar Series IV: Helicopters Series V: Helicopter Aerodynamics Series VI: Convertiplane, Autogiro, Composite Research Vehicle and Stowed Rotor Series VII: SR-175, Tri-Service Transport and V/STOL Transports Series VIII: Vertical Lift Theory and Aerodynamics – Non-Helicopter Series IX: Escape Systems, Crash and Rescue Series X: Power Plants, Propellers, RPV, Drone, Small Tactical Aerial Vehicle, and STAMP Series XI: Microfilm Series XII: Film
Biographical/Historical Note: Bernard Lindenbaum was born in 1916. In 1943 he was appointed a de la Cierva Fellow at New York University’s College of Engineering. In 1944 he received his Master of Aeronautical Engineering.
Lindenbaum has held a variety of positions during his engineering career ranging from Junior Aeronautical Engineer to Deputy for Analysis in the V/STOL Technology Division of the Flight Dynamics Laboratory. Some of the projects he participated in include: Sikorsky R-5, Kellett XR-8 “Synchropter,” Firestone XT9 A&B, Kellett XR-10 Synchropter transport, Bell XR-12 utility and light transport, Firestone XR-14 twin tail rotor helicopter, Piasecki XH-16 tandem
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rotor transport, Hughes XH-17 pressure jet rotor helicopter, Sikorsky H-19 light transport, Piasecki H-21 Artic Rescue, American H-26 pulse jet driven rotor, Bell H-40 (renamed UH-1), Kaman H-43 local base rescue, Bell XV-3 tilt rotor, Hiller X-18 tilt wing, Curtiss-Wright X-19 tilt propeller, Vought XC-142 tilt wing, AVRO “Avrocar,” Hawker P-1127, and others.
Lindenbaum retired from the United States Air Force in 1974. He served on the National Advisory Committee for Aeronautics (NACA) Helicopter Subcommittee and was a U.S. Data Exchange Officer on V/STOL Aircraft with the Federal Republic of Germany and France. He authored the definitive Volume 1 of V/STOL Concepts and Developed Aircraft for the U.S. Air Force and Navy.
Lindenbaum is a founding member of the American Helicopter Society (AHS) and a member of the society since 1945. He participated on the AHS Board of Directors as a Midwest Vice President. In 1970 he was awarded an AHS Honorary Fellowship and in 1974 he was chosen to receive the Society’s highest honor, the Alexander Klemin Award.
Bernard Lindenbaum died in 2002.
Scope and Content: The Bernard Lindenbaum Vertical Flight Research Collection is a very large collection documenting the history and development of helicopters and V/STOL aircraft from the mid1940s to the 1990s. The collection contains research reports, conference reports, blueprints, and film documenting this development. Researchers should be aware that the collection was minimally processed in that each box was fully inventoried, but no effort was made to place the material in acid-free folders, number folders, or relocate similar material together. As a result, some boxes will have more than one-topic and the same reports may appear in multiple boxes in the same series or under different series. When researching the collection, researchers should look through all of the boxes with similar headings to locate material. The collection has been organized into twelve, broad series topics.
Series I, Rotary Wing Handbook, consists of one Record Center box containing eight of the eighteen volumes of the Rotary Wing Handbook. The series also contains Part I and II of the 1960 Russian book “The Aerodynamic Design of Helicopters.”
Series II, NACA & NASA Reports, consists of five Record Center boxes containing National Advisory Committee on Aeronautics (NACA), and its successor, the National Aeronautics and Space Administration (NASA), reports on helicopters, V/STOL aircraft, VTOL aircraft, air foils, and tilted rotors. The date span for the reports is 1929 to 1977. There are also NACA annual reports from 1934 to 1941 and the proceedings of V/STOL Technology and Planning Conference held September 23 to 25, 1969.
Series III, AVRO Avrocar, consists of three Record Center boxes containing reports, progress reports, and photographs on the development of the Avrocar. The reports span a period beginning in 1958 and ending in 1990. There is also film of the Avrocar in Series XII.
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Series IV, Helicopters, is a fairly large series consisting of eight Record Center boxes containing reports spanning a period from1934 to 1997. The series includes early, pre-1960 reports on helicopters, blueprints of Kellett and Piasecki aircraft, and helicopter history articles and photographs. The series also contains helicopter brochures and information on early helicopters and towed helicopters.
Series V, Helicopter Aerodynamics, is a large series consisting of twenty Record Center boxes documenting helicopter aerodynamics from 1918 to 1993. The series includes reports on: helicopter dynamics, performance, and theory; rotors, rotor blades, and rotor aerodynamics; rotor blade test and helicopter controls; helicopter airfoils; helicopter vibration; aerial utility vehicles; hot cycle rotors and wing composite aircraft; and aerodynamics and the Kaman Model K-190. The series also contains American Helicopter Society Forum Reports from the 1970s and reports from the 1980 Propeller Propulsion Conference.
Series VI, Convertiplane, Autogiro, Composite Research Vehicle and Stowed Rotor, is another large series consisting of seventeen Record Center boxes containing reports from 1923 to 1999. This series contains reports on: the Convertiplane Model XV-1; stoppable and stowed rotors; convertiplane composite research aircraft; autogiros; compound helicopters; autogiro gliders and kites; tip-mounted power; and compound and rigid rotor helicopters.
Series VII, SR-175, Tri-Service Transport and V/STOL Transports, consists of nineteen Record Center boxes containing reports from 1938 to 1990. The topic of these reports center on triservice and V/STOL transports. Included in this series are reports from the 1st National V/STOL Aircraft Symposium held November 3-4, 1965. The series also includes a wide-variety of other topics including: the Bell SR-175 and ducted propellers; the tilt-wing propelloplane; lift fans and fans in wings; V/STOL short-haul transports; the Bell X-22A program, and reports on tilt wing V/STOL aircraft including the CL-84, X-18, VC-400, and XC-142A. The series also contains reports from the Academic VTOL and American Helicopter Society Proceedings and the First Convertible Aircraft Proceedings, and American Helicopter Society Forum reports from 1947 to 1972.
Series VIII, Vertical Lift Theory and Aerodynamics – Non-Helicopter, is one of the largest series in the collection spanning twenty-five Records Center boxes. The reports span a period from 1932 to 1989. Included in this series are reports on: tri-service transports, the Harrier; V/STOL propeller technology concepts; lift-fan flight research; high-lift devices; V/TOL and GETOL ground effects; tilt-wing aircraft; downwash and ground effects; shrouded propellers and propulsion systems; stopped rotor compound helicopters; and ducted and shrouded propellers.
Series IX, Escape Systems, Crash and Rescue, is a small series consisting of three Record Center boxes. This series includes reports from 1929 to 1999 that include information on escape systems and crash rescue helicopters.
Series X, Power Plants, Propellers, RPV, Drone, Small Tactical Aerial Vehicle, and STAMP, is another small series consisting of four Record Center boxes. The series includes information on: drone aircraft; remotely piloted vehicles; power plants; propellers; and the Small tactical Aerial Mobility Platform (STAMP). The series also contains reports from the Conference on Propeller
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Propulsion held April 22-24, 1980 and a copy of Lindenbaum’s presentation on “V/STOL Concepts and Developed Aircraft: A Historical Review.”
Series XI, Microfilm, is located in one box (Box 106) and includes the records of the Prewitt Aircraft Company, Clifton Heights, Pennsylvania. The microfilm contains reports on the history of the helicopter and rotary wing aircraft history.
Series XII, Film, consists of 190 reels of 16 mm film and 10 VHS cassettes documenting vertical flight reports and history from 1938 to 1977. Some of the film is in poor condition and all need to be converted to a VHS or DVD format for viewing. The series includes film of the XC-4B Hummingbird, the Bell XC-142, and the AVRO Avrocar, plus film of many other vertical flight aircraft.
Subject Terms
Persons/Families Lindenbaum, Bernard, 1916-2002
Organizations/Corporate Names Air Force Flight Dynamics Laboratory (U.S.)
Places Dayton (Ohio) Wright-Patterson Air Force Base (Dayton, Ohio)
Subjects (General) V/STOL Technology and Planning Conference (1969: Las Vegas, Nev.) Helicopters
Convertiplanes Jet helicopters Military helicopters Rotors (Helicopters) Sikorsky helicopters
Helicopters - - Aerodynamics Vertical rising aircraft Tilt rotor aircraft Avrocar (VTOL airplane)
Material Types Technical reports Blueprints Film Books Photographs Microfilm
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Occupations Aeronautical Engineer
Collection Inventory
SERIES I: Rotary Wing Handbook, 1943-1969
Box File Description Date
1 1 Volume 9 of 18: Rotor Blade Handbook Contract No. W33-038 ac-21804 (20695)
1958
2 Volume 5 of 18: Rotor Wing Handbook, Weight and Balance PB 121097
1954
3 Volume 6 of 18: Rotor Wing Handbook, Aerodynamics and Performance of Helicopters PB111390
1954
4 Volume 7 of 18: Rotary Wing Handbook, Vibrations Handbook for Helicopters 111289
1954
5 Volume 10 of 18: Rotary Wing Handbook, Stability and Control of Rotary Wing Aircraft PB111521
1954
6 Volume 11 of 18: Rotary Wing Handbook, Special Types of Rotary Wing Aircraft PB111633
1954
7 Volume 13 of 18 Rotary Wing Handbook– Convertible Aircraft Contract# W33-038 ac-21804 (20695)
1954
8 Volume 14 of 18: Rotary Wing Handbook, The Rotary Wing Industry PB111391
1954
9 Rotary Wing Handbook, Contractor’s Correspondence Project R-458-393 WCLSR 3
Jun 8 1954
10 Aerodynamic Investigations of Rotary Wing Configurations Project R458-393
1952-1954
11 General Investigations of Airplanes, Rotorcraft and Missile Stability + Control and Performance 1365-13541A
1950-1956
12 Early Rotary Wing Gliders, Pictures and Specifications 1943-1948 13 Rotary Wing Aircraft Handbook, Correspondence 1956 14 Wind Tunnel Tests on XR-10 Helicopter Model Volume I Mar1945 15 Wind Tunnel Tests on XR-10 Helicopter Model Volume II Apr 1945 16 A Preview of 18 Volumes of the Rotary Wing Handbooks
and History Project May 10 1950
17 NASA TT F-494 Helicopters, Calculation and Design Volume 1 Aerodynamics
Sep 1967
18 FTD TT 62-815 Problems of the Aerodynamics of Helicopter Lifting Rotors
Oct 3 1962
19 FSTC-HT-23-549-71 Helicopter Aerodynamics USSR 1969 20 F-TS-9794/V The Aerodynamic Design of Helicopters Part
I USSR Apr 1960
21 F-TS-9794/V The Aerodynamic Design of Helicopters Part II USSR
Apr1960
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SERIES II: NACA & NASA Reports, 1929-1977
Box File Description Date
2 1 NASA TN D-243 Tables and Charts for Estimating Stall Effects on Lifting-Rotor Characteristics
May 1960
2 NASA TN D-317 Wind-Tunnel Tests of a Circular Wing with an Annular Nozzle in Proximity to the Ground
1960
3 NASA TN D-326 Large-Scale Wind Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft – Preliminary Results
Jun 15 1960
4 NASA TN D-372 A Flight Study of the Conversion Maneuver of a Tilt-Duct VTOL Aircraft
Nov 1960
5 NASA TN D-376 High-Tip-Speed Static-Thrust Tests of a Rotor Having NACA 63(215)A018 Airfoil Sections with and without Vortex Generators Installed
May 1960
6 NASA TN D-382 Effect of Blade Cutout on Power Required by Helicopters Operating at High Tip-Speed Ratios
Sep 1960
7 NASA TN D-397 Data from a Static-Thrust Investigation of a Large Scale General Research VTOL-STOL Model in Ground Effect
Aug 1960
8 NASA TN D-444 Lateral Stability and Control Characteristics of a Four-Propeller Deflected-Slipstream VTOL Model Including the Effects of Ground Proximity
Jan 1961
9 NASA TN D-445 Investigation of Longitudinal and Lateral Stability Characteristics of a Six-Propeller Deflected-Slipstream VTOL Model with Boundary-Layer Control Including Effects of Ground Proximity
Jan 1961
10 NASA TN D-624 A Preliminary Study of V/STOL Transport Aircraft and Bibliography of NASA Research in the VTOL-STOL Field
Jan 1961
11 NASA TN D-658 Ground Influence on a Model Airfoil with a Jet-Augmented Flap as Determined by Two Techniques
Feb 1961
12 NASA TN D-730 Aerodynamic Characteristics of Propeller-Driven VTOL Aircraft
Mar 1961
13 NASA TN D-731 Induced Interference Effects on Jet and Buried-Fan VTOL Configurations in Transition
Mar 1961
14 NASA TN D-733 Review of Basic Principles of V/STOL Aerodynamics
Mar 1961
15 NASA TN D-736 Noise Considerations in the Design and Operation of V/STOL Aircraft
Apr 1961
16 NASA TN D-737 Some Recent Studies in Structural Dynamics of Rotor Aircraft
Mar 1961
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17 NASA TN D-774 Operational Technique for Transition of Several Types of V/STOL Aircraft
Mar 1961
18 NASA TN D-775 Aerodynamic Characteristics of a Large-Scale Model with a High Disk-Loading Lifting Fan Mounted in the Fuselage
Jul 25 1961
19 NASA TN D-776 A Wind Tunnel Investigation of a 4Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing
Feb 27 1961
20 NASA TN D-812 Effects of Gyroscopic Cross Coupling Between Pitch and Roll on the Handling Qualities of VTOL Aircraft
Apr 1961
21 NASA TN D-818 Method for Calculating Induced Velocities at the Blades of a Slightly Inclined Propeller with Constant Circulation
May 1961
22 NASA TN D-901 Aerodynamic Characteristics of a Four-Propeller Tilt-Wing VTOL Model with Twin Vertical Tails, Including Effects of Ground Proximity
Jun 1961
23 NASA TN D-920 Stability and Control Characteristics of a Small-Scale Model of an Aerial Vehicle Supported by Two Ducted fans
Aug 3 1961
24 NASA TN D-933 Tables of Interference Factors for Use in Wind-Tunnel and Ground-Effect Calculations for VTOL/STOL Aircraft Part I-Wind Tunnels Having Width-Height Ratio of 2.0
Jan 1962
25 NASA TN D-935 Tables of Interference Factors for Use in Wind-Tunnel and Ground-Effect Calculations for VTOL/STOL Aircraft Part III-Wind Tunnels having Width-Height Ratio of 1.0
Jan 1962
26 NASA TN D-936 Tables of Interference Factors for Use in Wind-Tunnel and Ground-Effect Calculations for VTOL/STOL Aircraft Part IV-Wind Tunnels having Width-Height Ratio of 0.5
Jan 1962
27 NASA TN D-937 Stability and Control Characteristics of a Model of an Aerial Vehicle Supported by Four Ducted Fans
Aug 1961
28 NASA TN D-970 Effect of Ground Proximity on the Aerodynamic Characteristics of Aspect-Ratio-1 Airfoils with and Without End Plates
Oct 1961
29 NASA TN D-973 Effects of Gyroscopic Cross Coupling Between Pitch and Yaw of the Handling Qualities of VTOL Aircraft
Nov 1961
30 NASA TN D-981 Aerodynamic Characteristics of a Powered Semispan Tilting-Shrouded-Propeller VTOL Model in Hovering and Transition Flight
Jan 1962
31 NASA TN D-989 Summary of Flight-Test Results of the VZ-2 Tilt-Wing Aircraft
Feb 1962
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32 NASA TN D-995 Aerodynamic Loads on an Isolated Shrouded-Propeller Configuration for Angles of Attack from -10 to +110 Degrees
Jan 1962
33 NASA TN D-996 An Analytical Trend Study of Propeller Whirl Instability
Apr 1962
34 NASA TN D-1032 STOL Characteristics of a Propeller-Driven Aspect-Ratio-10, Straight-Wing Airplane with Boundary-Layer Control Flaps, as Estimated from Large-Scale Wind-Tunnel Tests
Jun 1961
35 NASA TN D-1034 Large-Scale Wind-Tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flaps
Jun 1961
36 NASA TN D-1201 A Preliminary Piloted Simulator and Flight Study of Height Control Requirements for VTOL Aircraft
Feb 1962
37 NASA TN D-1234 Force-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellers
Apr 1962
38 NASA TN D-1235 Flight-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellers
Apr 1962
39 NASA TN D-1257 Division of Aerodynamic Loads on a Semispan Tilting-Ducted-Propeller Model in Hovering and Transition Flight
May 1962
40 NASA TN D-1272 Aerodynamic Characteristics in Pitch of Several Ring-Wing-Body Configurations at a Mach Number of 2.2
Apr 1962
41 NASA TN D-1301 Aerodynamic Characteristics of a 4Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing
Apr 1962
42 NASA TN D-1382 Slipstream Flow Around Aeveral Tilt-Wing VTOL Aircraft Models Operating Near the Ground
Sep 1962
43 NASA TN D-1430 Longitudinal Trim Characteristics of a Deflected Slipstream V/STOL Aircraft During Level Flight at Transitional Flight Speeds
Oct 1962
44 NASA TN D-1481 Aerodynamic Characteristics of Four-Duct Tandem VTOL-Aircraft Configurations
Jan 1963
45 NASA TN D-1509 Propeller Slipstream Effects as Determined from Wing Pressure Distribution on a Large-Scale VTOL Model at Static Thrust
Dec 1962
46 NASA TN D-1517 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for a Utility Type of Helicopter
Dec 1962
47 NASA TN D-1650 Aerodynamic Characteristics of a Large-Scale Model with Two High Disk-Loading Fans Mounted in the Wing
Jan 17 1963
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48 NASA TN D-1766 Wind-Tunnel Tests of Two VTOL Propellers in Descent
c.a.1963
49 NASA TN D-1857 Large-Scale Wind-Tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust
Oct 1964
50 NASA TN D-2014 Wing Pressure Measurements within the Propeller Slipstream for a Large-Scale V/STOL Wind-Tunnel Model Simulating Transition
Oct 1963
51 NASA TN D-2231 A Flight Investigation of the Performance, Handling Qualities, and Operational Characteristics of a Deflected Slipstream STOL Transport Airplane Having Four Interconnected Propellers
Mar 1964
52 NASA TN D-2254 Transition Characteristics of a VTOL Aircraft Powered by Four Ducted Tandem Propellers
Apr 1964
53 NASA TN D-2477 Effects of Gross Changes in Static Directional Stability on V/STOL Handling Characteristics Based on a Flight Investigation
Oct 1964
54 NASA TN D-2538 Wind-Tunnel Investigation of a Tilt-Wing VTOL Airplane with Articulated Rotors
Mar 1965
55 NASA TN D-2788 A Visual Flight Investigation of Hovering and Low-Speed VTOL Control Requirements
Apr 1965
56 NASA TN D-3936 Comparison of Flight-Measured Helicopter Rotor-Blade Chordwise Pressure Distributions with Static Two-Dimensional Airfoil Characteristics
May 1967
57 NASA TN D-4062 Full-Scale Investigation of the Aerodynamic Characteristics of a Model Employing a Sailwing Concept
Jul 1967
58 NACA TN 492 The Aerodynamic Analysis of the Gyroplane Rotating-Wing System
Mar 1934
59 NACA TN 1192 Charts Showing Relations Among Primary Aerodynamic Variables for Helicopter-Performance Estimation
Feb 1947
60 NACA TN 1250 Effect of Blade Stalling on the Efficiency of a Helicopter Rotor as Measured in Flight
Apr 1947
61 NACA TN 1289 Full-Scale Investigation of the Aerodynamic Characteristics of a Typical Single-Rotor Helicopter in Forward Flight
May 1947
62 NACA TN 1430 A Theoretical Study of the Dynamic Properties of Helicopter-Blade Systems
Nov 1948
63 NACA TN 1666 Flight Investigation of Effects of Rotor-Blade Twist on Helicopter Performance in the High-Speed and Vertical-Autorotative-Descent Conditions
Aug 1948
64 NACA TN 1698 Effect of Wind Velocity on Performance of Helicopter Rotors as Investigated with the Langley Helicopter Apparatus
Oct 1948
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65 NACA TN 1906 An Analytical Study of the Steady Vertical Descent in Autorotation of Single-Rotor Helicopters
Jun 1949
66 NACA TN 1983 Longitudinal Flying Qualities of Several Single-Rotor Helicopters in Forward Flight
Nov 1949
67 NACA TN 2226 Theoretical Analysis of Oscillations in Hovering of Helicopter Blades with Inclined and Offset Flapping and Lagging Hinge Axes
Dec 1950
68 NACA TN 2277 Effects of Compressibility on the Performance of Two Full-Scale helicopter Rotors
Jan 1951
69 NACA TN 2474 Empirical Relation Between Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors
Oct 1951
70 NACA TN 2656 A Blade-Element Analysis for Lifting Rotors That is Applicable for Large Inflow and Blade Angles and Any Reasonable Blade Geometry
Jul 1952
71 NACA TN 2665 An Extension of Lifting Rotor Theory to Cover Operation at Large Angles of Attack and High Inflow Conditions
Apr 1952
72 NACA TN 2847 Section Characteristics of a 10.5-Percent-Thick Airfoil with Area Suction as Affected by Chordwise Distribution of Permeability
Dec 1952
73 NACA TN 2943 The Attenuation Characteristics of Four Specially Designed Mufflers Tested on a Practical Engine Setup
May 1953
74 NACA TN 3022 Method for Studying Helicopter Longitudinal Maneuver Stability
Oct 1953
75 NACA TN 3182 Manual of the ICAO Standard Atmosphere Calculations by the NACA
May 1954
76 NACA TN 3237 Hovering Performance of a Helicopter Rotor Using NACA 8-H-12 Airfoil Sections
Aug 1954
77 NACA TN 3238 Review of Information on Induced Flow of a Lifting Rotor
Aug 1954
78 NACA TN 3241 Airfoil Section Characteristics at High Angles of Attack
Aug 1954
79 NACA TN 3242 Preliminary Results from Flow-Field Measurements Around Single and Tandem Rotors in the Langley Full-Scale Tunnel
Nov 1954
80 NACA TN 3304 Investigation of the Aerodynamic Characteristics of a Model Wing-Propeller Combination and of the Wing and Propeller Separately at Angles of Attack up to 90 degrees
Nov 1954
81 NACA TN 3354 Gust Experience of a Helicopter and an Airplane in Formation Flight
Dec 1954
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82 NACA TN 3361 Aerodynamic Characteristics of NACA 0012 Airfoil Section at Angles of Attack from 0 to 90 Degrees
Jan 1955
83 NACA TN 3366 A Method for Studying the Transient Blade-Flapping Behavior of Lifting Rotors at Extreme Operation Conditions
Jan 1955
84 NACA TN 3440 Hovering Flight Tests of a Four-Engine-Transport Vertical Take-off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream
May 1955
85 NACA TN 3616 Charts for Estimating Rotor-Blade Flapping Motion of High-Performance Helicopters
Mar 1956
86 NACA TN 3625 Investigation of the Propulsive Characteristics of a Helicopter-Type Pulse-Jet Over a Range of Mach Numbers and Angles of Yaw
Jan 1956
87 NACA TN 3630 Hovering-Flight Tests of a Model of a Transport Vertical-Take-Off Airplane with Tilting Wings and Propellers
Mar 1956
88 NACA TN 3745 Transition-Flight Tests of a Model of a Low-Wing Transport Vertical-Take-Off Airplane with Tilting Wing and Propellers
Sep 1956
89 NACA TN 3850 Experimental Investigation on the Langley Helicopter Test Tower of Compressibility Effects on a Rotor Having NACA 63sub2-015 Airfoil Sections
Dec 1956
90 NACA TN 3855 The Effect of Forward-Flight Speed on the Propulsive Characteristics of a Pulse-Jet Engine Mounted on a Helicopter Rotor
Jan 1957
91 NACA TN 3690 Normal Component of Induced Velocity in the Vicinity of a Lifting Rotor with a Nonuniform Disk Loading
Apr 1956
92 NACA Technical Note TN 3691 Analysis and Comparison with Theory of Flow-Field Measurements Near a Lifting Rotor in The Langley Full-Scale Tunnel
Apr 1956
93 NACA TN 3921 Approximate Solution for Streamlines About a Lifting Rotor Having Uniform Loading and Operating in Hovering or Low-Speed Vertical Flight Conditions
Feb 1957
94 NACA TN 4124 Effect of Ground Proximity on the Aerodynamic Characteristics of a Four-Engine Vertical-Take-Off-And-Landing Transport-Airplane Model with Tilting Wing and Propellers
Sep 17 1957
95 NACA TN 4131 Transition-Flight Investigation of a FourEngine-Transport Vertical-Take-Off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream
Dec 1957
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96 NACA TN 4239 Experimental Investigation of the Drag of Flat Plates and Cylinders in the Slipstream of a Hovering Rotor
Apr 1958
97 NACA TN 4356 Effects of Compressibility on Rotor Hovering Performance and Synthesized Blade-Section Characteristics Derived from Measured Rotor Performance of Blades Having NACA 0015 Airfoil Tip Sections
Sep 1958
98 NACA TN 4357 Lift and Profile-Drag Characteristics of an NACA 0012 Airfoil Section as Derived from Measured Helicopter-Rotor Hovering Performance
Sep 1958
3 1 Air Ministry Aeronautical Research Committee – Reports and Memoranda No. 1132. On the Vertical Ascent of a Helicopter by H. Glauert, M.A.
Nov 1927
2 NACA TM No. 367 Application of the “Magnus Effect” to the Wind Propulsion of Ships
Nov 17 1924
3 Induced Flow Near a Rotor and Its Application to Helicopter Problems by Harry H. Heyson
Apr 16-20 1958
4 NASA TM X-680 Wind-Tunnel Investigation of the Aerodynamic and Structural-Deflection Characteristics of an Inflatable Airplane
Aug 1962
5 NASA TR R-14 A Method for Calculation of Hydrodynamic Lift for Submerged and Planning Rectangular Lifting Surfaces
1959
6 NASA TR R-124 Linearized Theory of Wind-Tunnel Jet-Boundary Corrections and ground Effect for VTOL-STOL Aircraft
1962
NACA ANNUAL REPORTS 4 1 National Advisory Committee on Aeronautics (NACA)
Twentieth Annual Report Numbers 475-507 1934
2 National Advisory Committee on Aeronautics (NACA) Twenty-Fourth Annual Report Numbers 612-644
1938
3 National Advisory Committee on Aeronautics (NACA) Twenty-Fifth Annual Report Numbers 645-680
1939
4 National Advisory Committee on Aeronautics (NACA) Twenty-Sixth Annual Report Numbers 681-703
1940
5 National Advisory Committee on Aeronautics (NACA) Twenty-Seventh Annual Report Numbers 704-726
1941
6 Large Photo of Convair XFY-1 Undated 7 Miscellaneous Helicopter Photos and Negatives Undated
5 1 Proceedings of V/STOL Technology and Planning Conference AFFDL
Sep 23-25 1969
2 Photos of Helicopters and 1962 Redesignation Letter Various
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3 Vertical Take Off and Landing Concepts Applicable to Drones/RPVs(U) Appendix G-11
1974
4 Helicopter Photos Various 5 Folder of NACA Reports – Reports No. 352, 460, 537,
586, 628, 664, 586, 573, 574, 648, 651, 678, 627, 665, 575, 540, 642, 680, 592, 662, 652, 546.
1933-1939
NACA REPORTS - BOUNDARY LAYER CONTROL, JET CIRCULATION
6 1 Report No. 77-0076 Circulation Control – An Updated Bibliography of DTNSRDC Research and Selected Outside References
Sep 1977
2 Research on Elliptical Airfoil with Jet Circulation Control Contract# N00014-67-A0126 Univ. of Texas
Jan 1969
3 Proposal No. 148 Theoretical and Experimental Analysis of the Jet Circulation Control Airfoil Nielsen Engineering & Research, Inc.
Mar 7 1968
4 The Laminar Flow Control Presentation for the Aeronautical Systems Division Northrop
May 3-4 1962
5 Boundary Layer Control by Porous Suction by H.G. Lew & R.D. Matieu Penn. State Univ. Contract# AF18(600)575
Jun 1954
6 Report No. 071 Suction and Blowing Tests on the Cessna 309 Mock-Up by Friedrich Wagner Univ. of Wichita
Apr 1952
7 Research Report No. 15 A Simplified Procedure for Calculating Boundary Later Control Systems for Unflapped Airfoils by J.J. Cornish, III Miss. State Univ.
Feb 28 1958
8 Research Report No. 19 Practical High Lift Systems Using Distributed Boundary Layer Control by J.J. Cornish, III Miss. State Univ.
Dec 10 1958
9 TR No. 8 Simplicity with Accuracy in the Computation of Spanwise Lift Distribution Stout Skycraft Corp.
Jan 20 1941
10 A.R.C. TR C.P. No. 82 Power Requirements for Distributed Suction for Increasing Maximum Lift UK Ministry of Supply
1952
11 WADC TR 52-196 Design of Boundary-Layer-Control Suction and Blowing Ducts with Arbitrary Flow Distributions
Sep 1952
12 AGARD-CP-126 Military Applications of V/STOL Aircraft Volume 1
Oct 23-25 1972
13 AHS 30th Annual Forum – Paper 823 U.S. Navy VTOL Automatic Landing System Development Program by Robert S. Buffum, Richard W. Huff & Capt. Gerard L. Keyser Flight Test Div., Pax River
May 1974
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14 Document No. 12055-FR1 Experimental Investigations of Flight Control Surfaces Using Modified Air Jets Contract# N00019-67-C-0260 Honeywell
Nov 1969
15 Background, Recent Developments and Objectives in V/STOL Aircraft Fairchild
C.A. 1965
16 NASA Memo 2-27-59A Low-Speed Tests of Semispan-Wing Models at Angles of Attack from 0o to 180o
Mar 1959
17 NASA TN D-316 Study of the Aerodynamic Forces and Moments on Bodies of Revolution in Combined Pitching and Yawing Motions
Apr 1960
18 NASA TN D-660 Effects of Various Arrangements of Slotted and Round Jet Exits on the Lift and Pitching-Moment Characteristics of a Rectangular-Base Model at Zero Forward Speed
Feb 1961
19 NASA TN D-720 Effect of Ratio of Jet Area to Total Area and of Pressure Ratio on Lift Augmentation of Annular Jets in Ground Effect under Static Conditions
Mar 1961
20 NASA TN D-727 Ground Interference Effects Apr 1961 21 NASA TN D-786 Investigation of the Longitudinal
Characteristics of a Large-Scale Jet Transport Model Equipped with Controllable Thrust Reversers
Mar 1961
22 NASA TN D-789 Aerodynamics of a Fan-In-Fuselage Model
May 1961
23 NASA TN D-818 Method of Calculating Induced Velocities at the Blades of a Slightly Inclined Propeller with Constant Circulation
May 1961
24 NASA TN D-969 Effect of Groundboard height on the Aerodynamic Characteristics of a Lifting Circular Cylinder Using Tangential Blowing from Surface Slots
Oct 1961
25 NACA TN No. 323 Wind Tunnel Tests on Airfoil Boundary Later Control Using a Backward Opening Slot
Oct 1929
26 NACA TN No.340 Full Scale Drag Tests on Various Parts of Fairchild (FC-2W2) Cabin Monoplane
May 1930
27 NACA TN No.507 The Effects of Equal-Pressure Fixed Slots on the Characteristics of a Clark Y Airfoil
Oct 1934
28 NACA TN No.624 Performance Characteristics of Venturi Tubes Used in Aircraft for Operating Air-driven Gyroscopic Instruments
Nov 1937
29 NACA TN No.640 Interference of Wing and Fuselage from Tests of 18 Combinations in the NACA Variable-Density Tunnel - Combinations with Split Flaps
Mar 1938
30 NACA TN No.641 Interference of Wing and Fuselage from Tests of 17 Combinations in the NACA Variable-Density Tunnel – Combinations with Special Junctions
Mar 1938
15
31 NACA TN No.642 Interference of Wing and Fuselage from Tests of Eight Combinations in the NACA Variable-Density Tunnel – Combinations with Tapered Fillets and Straight-Side Junctions
Mar 1938
32 NACA TN No.691 Some Elementary Principles of Shell Stress Analysis with Notes on the Use of the Shear Center
Mar 1939
33 NACA TN No.692 Some Fundamental Considerations in Regard to the Use of Power in Landing an Airplane
Mar 1939
34 NACA TN No.695 The Effects of Some Common Surface Irregularities on Wing Drag
Mar 1939
35 NACA TN No.699 Tests of NACA 23012 Airfoil with Slotted Deflector Flap
Apr 1939
36 NACA TN No.702 Wind-Tunnel Tests of Several Forms of Fixed Wing Slot in Combination with a Slotted Flap on an NACA 23012 Airfoil
Apr 1939
37 NACA TN No.705 Wind-Tunnel Investigation of Ground Effect on Wings with Flaps
May 1939
38 NACA TN No.714 Flight Tests of Retractable Ailerons on a Highly Tapered Wing
Jun 1939
39 NACA TN No.715 Wind-Tunnel Investigation of an NACA 23012 Airfoil with Two Arrangements of a Wide-Chord Slotted Flap
Jun 1939
40 NACA TN No.719 The Effects of Partial-Span Slotted Flaps on the Aerodynamic Characteristics of a Rectangular and a Tapered NACA 23012 Wing
Jul 1939
41 NACA TN No.728 Wind-Tunnel Investigation of an NACA 23012 Airfoil with Two Arrangements of a 40Precent-Chord Slotted Flap
Sep 1939
42 NACA TN No.732 A Simplified Method of Obtaining Span Load Distributions
Oct 1939
43 NACA TN No.837 Notes on the Stability and Control of Tailless Airplanes
Dec 1941
44 NACA Technical Note 2502 Examples of Three Representative Types of Airfoil-Section Stall at Low Speed
Sep 1951
45 NACA Technical Note 2659 A Miniature Electrical Pressure Gage Utilizing a Stretched Flat Diaphragm
Apr 1952
46 NACA Technical Note 3918 Wind-Tunnel Investigation of Effect of Propeller Slipstreams on Aerodynamic Characteristics of a Wing Equipped with a 50-Percent-Chord Sliding Flap and a 30-Percent-Chord Slotted Flap
Feb 1957
47 NACA TM No. 475 Recent researches on the Air Resistance of Spheres
Aug 1928
48 NACA TM No.557 Measurement of Profile Drag on an Airplane in Flight by the Momentum Method Part I
Mar 1930
16
49 NACA TM No.558 Measurement of Profile Drag on an Airplane in Flight by the Momentum Method Pt. II
Mar 1930
50 NACA TM No.545 The Balance of Moments and the Static Longitudinal Stability of Airplanes
Dec 1929
51 NACA TM No. 563 Balanced and Servo Control Surfaces May 1930 52 NACA TM No. 567 The Magnus Effect in Theory and in
Reality May 1930
53 NACA TM No. 612 Static Longitudinal Stability of “ENTE” Airplanes
Mar 1931
54 NACA TM No. 794 Chief Characteristics and Advantages of Tailless Airplanes
May 1936
55 NACA TM No. 850 Engines and Propellers for Powered Gliders and Light Airplanes
Mar 1938
56 NACA TM No. 867 Theoretical Study of Various Airplane Motions After Initial Disturbance
Jun 1938
57 NACA TM No. 900 The Effect of the Masses of the Controls on the Longitudinal Stability with Free Elevator
Jul 1939
58 NACA TM No. 906 Forces and Moments on a Yawed Airfoil
Aug 1939
59 NACA TM No. 974 Boundary Layer Removal by Suction Apr 1941 60 NACA TM No. 990 Contribution to the Aerodynamics of
Rotating-Wing Aircraft Part II 1941
61 NACA TM No. 1011 Pressure Distribution on Wings in Reversed Flow
Apr 1942
62 NACA Report No. 315 Aerodynamic Characteristics of Airfoils – VI
1929
63 NACA Report No. 331 Collection of Wind-Tunnel Data on Commonly Used Wing Sections
1929
64 NACA Report No. 400 The Aerodynamic Characteristics of a Slotted Clark Y Wing as Affected by the Auxiliary Airfoil Position
1931
65 NACA Report No. 411 Theory of Wing Sections of Arbitrary Shape
1931
66 NACA Report No. 419 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –I-Ordinary Ailerons on Rectangular Wings
1932
67 NACA Report No. 422 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –II- Slotted Ailerons and Frise Ailerons
1932
68 NACA Report No. 423 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack – III-Ordinary Ailerons Rigged Up 10o When Neutral
1932
69 NACA Report No. 424 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack – IV-Floating Tip Ailerons on Rectangular Wings
1932
17
70 NACA Report No. 437 The Effect of Area and Aspect Ratio on the Yawing Moments of Rudders at Large Angles of Pitch on Three Fuselages
1932
71 NACA Report No. 439 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –V-Spoilers and Ailerons on Rectangular Wings
1932
72 NACA Report No. 444 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –VI-Skewed Ailerons on Rectangular Wings
1932
73 NACA Report No. 450 The Calculation of Take-Off Run 1932 74 NACA Report No. 494 A Flight Investigation of the
Lateral Control Characteristics of Short Wide Ailerons and Various Spoilers with Different Amounts of Wing Dihedral
1934
75 NACA Report No. 496 General Theory of Aerodynamic Instability and the Mechanism of Flutter
1935
76 NACA Report No. 499 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –XII-Upper-Surface Ailerons on Wings with Split Flaps
1934
77 NACA Report No. 517 Flight Investigation of Lateral Control Devices for Use with Full-Span Flaps
1935
78 NACA Report No. 518 The Drag of Airplane Wheels, Wheel fairings and Landing Gears – II Nonretractable and Partly Retractable Gears
1935
79 NACA Report No. 530 Characteristics of the NACA 23012 Airfoil from Tests in the Full-Scale and Variable-Density Tunnels
1935
80 NACA Report No. 541 Aerodynamic Characteristics of Wings with Cambered External-Airfoil Flaps, Including Lateral Control with a Full-Span Flap
1935
81 NACA Report No. 552 Wind-Tunnel Tests of 10-Foot-Diameter Autogiro Rotors
1936
82 NACA Report No. 554 Wind-Tunnel Investigation of Ordinary and Split Flaps on Airfoils of Different Profile
1936
83 NACA Report No. 573 Aerodynamic Characteristics of NACA 23012 and 23021 Airfoils with 20-Percent-Chord External-Airfoil Flaps of NACA 23012 Section
1936
84 NACA Report No. 579 A Study of the Two-Control Operation of an Airplane
1936
85 NACA Report No. 586 Airfoil Section Characteristics as Affected by Variations of the Reynolds Number
1937
86 NACA Report No. 602 Wind-Tunnel and Flight Tests of Slot-Lip Ailerons
1937
87 NACA Report No. 605 Resume and Analysis of NACA Lateral Control Research
1937
18
88 NACA Report No. 654 General Airplane Performance 1939 89 NACA Report No. 669 Airfoil Section Data Obtained in
the NACA Variable-Density Tunnel as Affected by Support Interference and Other Corrections
1939
90 NACA Report No. 677 Wind-Tunnel Investigation of an NACA 23021 Airfoil with Various Arrangements of Slotted Flaps
1939
91 NACA Report No. 679 Wind-Tunnel Investigation of an NACA 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flap
1939
92 NACA Report No. 716 A Simplified Theoretical Method of Determining the Characteristics of a Lifting Rotor in Forward Flight
1941
93 NACA Wartime Report CB 3E27 Characteristics of an NACA 66,S-209 Section Hydrofoil at Several Depths
May 1943
94 NACA Wartime Report L4C28 Preliminary Tank Experiments with a Hydrofoil on a Planing-Tail Seaplane Hull
Mar 1944
95 NACA Wartime Report L5A13a Wind-Tunnel Tests of a Dual-Rotating Propeller Having One Component Locked or Windmilling
Jan 1945
96 NACA Wartime Report L4C24 On the Flow of a Compressible Fluid by the Hydrograph Methods – I-Unification and Extension of Present-Day Results
Mar 1944
97 NACA Wartime Report L4D06 Preliminary Tank Tests of an Outboard Float Having the Form of a Streamline Body of Revolution Fitted with a Hydrofoil
Apr 1944
98 NACA TN No. 1683 An Experimental Investigation of an NACA 631-012 Airfoil Section with Leading Edge Suction Slots
Aug 1948
99 NACA TN No. 1741 Exploratory Wind-Tunnel Investigation of the Effectiveness of Area Suction in Eliminating Leading-Edge separation over an NACA 641A212 Airfoil
Nov 1948
Series III: AVRO Avrocar, 1958-1990
Box File Description Date
7 1 AVRO/SPG/TR 125 Issue 6 Airplane Weight Moment of Inertia and C. of G. Status – AVROCAR-
Feb 1959
2 AVRO/SPG/TR267 Test Data Report for The Full Scale 20o Wingtip Segment of the AVROCAR Contract# AF33(600) 37496 AVRO
May 1959
19
3 AVRO/SPG/TR 265 Part 2 & 3 Test Data Report for 1/5 Scale AVROCAR Model, Forward Flight Characteristics Contract# AF 33(600)-30161 AVRO
Dec 1959
4 AVRO/SPG/TR183 Mass Flow and Thrust Calibration of Transonic Sting Model Contract# AF33(600)30161 AVRO
Jul 1958
5 AVRO/SPG/TR264 Force Data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO
Apr 1959
6 AVRO/SPG/TR 275 System 606A VTOL Fighter-Bomber Project Load and Stress Survey Turborotor Contract# Af33(600)-30161 AVRO
Jan 1959
7 AVRO/SPG/TR264 Appendix Force Data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO
Apr 1959
8 AVRO 500/AREO TEST/408 Avrocar Continuation Test Program Report on Phase 2 Tests of an Avrocar in the 40x80 Foot Wind Tunnel at NASA Ames research Center Vol. 1Contract# AF33(600)-42163 AVRO
May 1961
9 AVRO/SPG/TR 276 System 606A VTOL Fighter-Bomber Project: Notes on the Preliminary Performance Calculations Contract AF33(600)-30161 AVRO
Jan 1961
10 AVRO 600 (PROJ) 2 Preliminary Trade-Off Study Contract# AF33(600)-39722 AVRO
Jan 1960
11 AVRO/SPG/TR 310 Further Tests on J69 Exhaust Ducting for AVROCAR Contract# AF33(600)-37496 AVRO
Jan 1960
12 AVRO 500/AERO TEST/410 Avrocar Continuation Program Data Report for 1/20 Scale Avrocar Model Contract# AF33(600)-42163 AVRO
Jan 1961
13 AVRO/SPG/TR 187 Report on Avrocar Analog Computing Program Phase 1 and Phase 2 Contract# AF33(600)30161 Supplementary Agreement No. 5 AVRO
Nov 1958
14 AVRO Progress Report No. 6 AVROCAR 1: US Army Designation VZ-9A V Contract# AF33(600)37496 AVRO
Feb. - Mar 1959
15 AVRO 500/PERF/411 Summary Review of the Continuation Test Program for the Avrocar: Including Review of Allied Programs Contract# AF33(600)-42163 AVRO
May 1961
16 AVRO/SPG/TR 205 ISSUE 1 Strength Summary and Operating Restrictions Contract# AF33(600)-37496 AVRO
Apr 1959
17 AVRO/SPG/TR 304 Tethered and Free Flight Tests of the AVROCAR Fitted with Nozzle Spoiler Controls Contract# AF33(600)-37496 AVRO
Dec 1959
18 Evolution of an Engineering Miracle; Flight Dynamics Laboratory Article
Oct 1988
19 AVRO P450/PERF/1 Mobile Ground Effect Machine Preliminary Report AVRO
Jun 1960
20
20 AVRO/SPG/TR 308 Data Report for the 1/20 Scale Avrocar Model Focusing Ring Control Static Tests Contract# AF33(600)-37496 Supplementary Agreement No. 1 AVRO
Undated
21 AVRO/SPG/TR 254 The Avrocar Design Contract# AF33(600) 30161 AVRO
Jan 1959
22 The AVRO VZ-9 Experimental Aircraft (AVROCAR) Lessons Learned AVRO
Sep 17-19,1990
23 AVRO P470/THEORETICAL AERO/3 The Two Dimensional Airfoil in Incompressible Flow with Arbitrary Mass Flow Through a Central Gap AVRO
Jun 1960
24 AVRO/SPG/TR265 Part 1 Data Report for the 1/5 Scale Avrocar Model Tests Contract# AF33(600)-30161 AVRO
Nov 1959
25 AVRO/SPG/TR 263 The Effect of the Incorrect Assumptions on Avrocar Static Thrust and Turborotor Running Conditions Contract# AF33(600)37496 Supplementary Agreement No. 5 AVRO
Nov 1958
26 Avrocar Turborotor Test Specifications Contract# AF33(600)-37496 Supplemental Agreement Proposal AVRO
Jan 22 1959
27 AVRO/SPG/TR264 Force Data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO
Apr 1959
8 1 AVRO Review of AVRO G.E.T.O.L/V.T.O.L Future Development
Dec 8-9 1959
2 AVRO/SPG/TR 205 Issue 1 Strength Summary and Operating Restrictions AVROCAR 1 Contract# AF33(600)-37496 AVRO
Apr 1959
3 AVRO/SPG/TR 308 Data Report for the 1/20 Scale AVROCAR model Focusing Ring Control Static Tests Contract# AF33(600)-37496 Supplemental Agreement No. 1 AVRO
Undated
4 Model Specification AVRO Aircraft Project AVROCAR 1 US Army Designation VZ-9AV
May 20 1958
5 AVRO/SPG/TR 254 The AVROCAR Design Contract# AF33(600)-30161
Jan 1959
6 AVRO/SPG/TR 249 Report on AVROCAR Analog Computing Program Phase 3 Contract# AF33(600)-30161 Supplementary Agreement No. 5 AVRO
Feb 1959
7 Progress Report No. 3 AVROCAR 1 US Army Designation VZ-9AV Contract# AF33(600)-37496
Aug 1 1958 –Sep 30 1958
8 AVRO/SPG/TR 197 ADDENDUM No. 1 Specification for Tests of an AVROCAR in the 40 Foot X 80 Foot Wind Tunnel at NASA Ames Aeronautical Laboratories Contract# AF33(600)-37496 Supplemental Agreement No. 1 AVRO
Feb 1960
21
9 AVRO System 606A Bi-Monthly Progress Report No. 11 1 November 1958 -31 December 1958 Contract# AF33(600)30161 Supplemental Agreement No. 5 AVRO
Jan 20 1959
10 AVRO Program Planning Report Pre-Phase 1 Part 1 and Part 2 – Development Program VTOL Supersonic Aircraft AVRO
Sep 30 1959
11 AVRO/SPG/TR 280 Test Specification for the Research Flight Test Program AVROCAR 1 AVRO
Undated
12 500/AERO TEST/405 AVROCAR Continuation Test Program Specification for the Phase 2 Tests of an AVROCAR in the 40x80 Foot Wind Tunnel at NASA Ames Research Center Contract# AF33(600)-42163 (S.W.8) AVRO
Dec 1960
13 AVRO/SPG/TR 312 Note on the AVROCAR Simulator for Hovering and Low Speed Flight AVRO
Feb 1960
14 Report CR-300 Summary TR AVROCAR Turborotor Development Program I.D. No. 60 RDZ-2227
Feb 1960
15 AVRO/SPG/TR 195 AVROCAR Ground and Flight Test Specifications AVRO
Nov 1958
16 500/S&C/428 Canadian Government Program for the AVROCAR Phase 1 Stability and Control Contract# T.B.570345 and Serial No. 9-BX-0-8 (S.O.W. Para 2.1.4)
May 1961
17 500/AERO TEST/415 Issue 2 AVROCAR Continuation Test Program Instrumentation Specification For AMES Tunnel Tests 1st AVROCAR Vehicle Contract# AF33(600)-42163 (S.W.5) AVRO
Dec 1960
18 Progress Report No. 10 AVROCAR 1 US Army Designation VZ-9AV Contract# AF33(600)-37496 and Supplemental Agreement No. 1 AVRO
Oct - Nov 1959
19 500/PROJ/6 Progress Report No. 3 AVROCAR 1 US Army designation VZ-9AV Contract# AF33(600)-42163 (S.W. 11) AVRO
Nov 1960
20 AVROCAR 1 US Army Designation VZ-9A V Cumulative Cost Report Supplement to AVROCAR Progress Report No. 5Contract# AF33(600)37496 AVRO
Feb 28 1959
21 Progress Report No. 11 AVROCAR 1 US Army Designation VZ-9AV Contract# AF33(600)-37496 and Supplemental Agreement No. 1 AVRO
Dec 1959 - Jan 1960
22 AVRO/SPG/TR 304 Tethered and Free Flight Tests of the AVROCAR Fitted with Nozzle Spoiler Controls Contract# AF33(600)-37496 Supplemental Agreement No. 1 AVRO
Dec 1959
23 500/PROJ/1 Progress Report No. 1 Canadian Government Program for the AVROCAR AVRO
Jul 31 1960
22
24 500/PERF/430 Canadian Government Program for the AVROCAR Phase 1 – Comparison of the Direct Operating Costs of the Light Aircraft with Developed Versions of the AVROCAR Contract# TB570345 Serial No. 9-BX-0-8 (S.O.W. Para 2.1.5) AVRO
Apr 1961
25 AVRO/SPG/TR 300 Revision of Propulsion Estimates AVROCAR 1 Contract# AF33(600)-37496 AVRO
Dec 1959
26 AVRO Program Planning Report AVROCAR 1 US Army Designation VZ-9AV
May 1 1958
27 AVRO/SPG/TR 305 Tests of the AVROCAR in the Static Rig Contract# Af33(600)-37496 Supplemental Agreement No. 1 AVRO
Dec 1959
28 Review of AVROCAR Development Prospects Apr 6-7 1960 29 AVRO/SPG/TR 174 A Brief Technical Description of the
AVROCAR Contract# AF33(600)30161 Supplementary Agreement No. 3 AVRO
May 1958
30 Progress Report No. 5 AVROCAR 1 – US Army Designation VZ-9AV Contract# AF33(600)37496 AVRO
Dec 1 1958 –Jan 31 1959
31 Progress Report No. 1 AVROCAR 1 – US Army Designation VZ-9AV Contract# AF33(600)37496 AVRO
Feb 1 – Jun 30 1958
32 500/PERF/427 Canadian Government Program for the AVROCAR Phase 1 – Performance- Contract# TB570345 Serial No. 9-BX-0-8 (S.O.W. Para 2.1.5)
Mar 1961
9 1 AVRO/SPG/TR 242 Tests on J69 Intake and Exhaust Ducting For AVROCAR Contract# AF33(600)-37496 Supp. Agree. #1 AVRO
Apr 1959
2 AVRO/SPG/TR 264 Appendix – Force data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO
Apr 1959
3 AVRO/SPG/TR 265 Part 2 & 3 1/5 Scale AVROCAR Model Forward Flight Characteristics Contract# AF33(600)-30161 Supp. Agree. #5 AVRO
Dec 1959
4 AVRO/SPG/TR 266 Data Report for the 1/20 Scale AVROCAR Model Tests Contract# AF33(600)-37496 AVRO
Jun 1959
5 AVRO/SPG/TR 300 Revision of Propulsion Estimates AVROCAR 1 Contract# AF33(600)-37496 AVRO
Dec 1959
6 AVRO/SPG/TR 308 Data Report for the 1/20 Scale AVROCAR Model Focusing Ring Control Static Tests Contract# AF33(600)-37496 Supp. Agree. #1 AVRO
C.A. 1960
7 AVRO/SPG/TR 408 AVROCAR Continuation Test Program Report on Phase 2 Tests of an AVROCAR in the 40x80 Foot Wind Tunnel at NASA Ames Research Center Contract# AF33(600)-42163 (S.W. 9) AVRO
May 1961
23
8 NASA TN D-1432 Large-Scale Wind-Tunnel Tests of a Circular Plan-Form Aircraft with a Peripheral Jet for Lift, Thrust, and Control AVRO
Feb 1963
9 The AVRO VZ-9 Experiment Aircraft – Lessons Learned by Daniel C. Murray Wright Research & Development Center – Original Manuscript Plus Copies
C.A. 1962
10 AVROCAR Photos C.A. 1960 11 Comparative Paper of AVROCAR 1, ADAM III, Short
SC-1, Dassault Mirage IIIV, Entwicklungsring Sud EWR VJ 101C, Verinigte Flugtechnische werke VAK-191B, US/FRG V/STOL Tactical Fighter and Dornier 31. (partial package)
C.A. 1972
12 The AVRO VZ-9 Experiment Aircraft – Lessons Learned by Daniel C. Murray Wright Research & Development Center – Slide Presentation Associated with #9 above (20 slides)
C.A. 1962
13 Progress Report No. 2 – AVROCAR 1 (Army VZ-9AV) Jul 1 1958 to Jul 31 1958 Contract# AF33(600)-37496
Aug 30 1958
14 Progress Report No. 6 – AVROCAR 1 (Army VZ-9AV) Feb and Mar 1959 Contract# AF33(600)-37496
C.A. Apr 1959
15 Progress Report No. 9 – AVROCAR 1 (Army VZ-9AV) Aug and Sep 1959 Contract# AF33(600)-37496 and Supp. Agree. #1
C.A. Oct 1959
16 System 606A Bi-Monthly Progress Report No. 17 Contract# AF33(600)-30601 and Supp. Agree. #3,5,6.
C.A. Jan 1960
17 Proposal for AVROCAR No. 2 C.A. 1960 18 Proposal for AVROCAR No. 3 C.A. 1960 19 AVROCAR Documents (3) 1959-1960 20 Report No. AVRO/SPG/TR157 Frequency Response Tests
of a Pneumatic Control System – System 606A- Contract# AF33(600)30161 AVRO
May 1958
21 Report No. AVRO/SPG/TR296 Results of Frequency Response Tests of the Pilot Control Bellows for the AVROCAR Contract AF33(60)-30161 AVRO
Jan 1960
22 Report No. AVRO/SPG/TR311 Static Rig and Flight Tests of the AVROCAR Fitted with the Focusing Ring Control Contract# AF33(600)-37496 Supp. Agreement No. 1 AVRO
Feb 1960
23 Report No. 600/PERF/17 Vertical Take-Off & Landing Performance Using an Ejector Lift Augmentation System Contract# AF33(600)-39722 AVRO
Jul 1960
24 Report No. 500/PERF/411 Summary Review of the Continuation Test Program for the AVROCAR Contract# AF33(600)-42163 AVRO
May 1961
25 Report No. FTC-TDR-61-56 AVROCAR Flight Evaluation AFFTC
Jan 1962
24
SERIES IV: Helicopters, 1934-1997
Box File Description Date
EARLY (PRE-1960) HELICOPTERS 10 1 Report D200-099-001 Estimated Performance for Bell
Model D-200 Gas Turbine Helicopter Sep 7 1951
2 Report D200-099-002 Proposal Summary for Bell Model D-200 Gas Turbine version of the H-13D – HTL-4 Helicopter
Oct 2 1951
3 Report D200-099-003 Comparative Payloads and Durations Provided by the Principle Helicopter Rotor Propulsion Systems
Sep 10 1951
4 Report D200-947-001 Detail Specification for Bell Model D-200 Gas Turbine Two Bladed Helicopter
Apr 7 1952
5 D200 Turbine Powered Helicopter Brochure Bell Sep 1951 6 Bell Model D-200 Blueprints 1951 7 NAVAER SD-377 Detail Specification for Model XHJD-1
Helicopter (Flight Test Article) (Twin Rotor) (Convertible) Contract# NOa(s)-3703
May 8 1944
8 Hiller Helicopter Blueprints 1947 9 BIS-21139 FT36-141 Model HRS-1 Helicopter, BuNo
127783 and Model HRS-2, BuNo 129017: Limited Tests, Report No. 2
Jun 18 1952
10 Report NV-1016 Evaluation of Wind- Tunnel Tests of a Dynamic Model of the XH-17 Helicopter Rotor Contract# AF 33(038)-8907 Hughes
Apr 5 1954
11 Report WCT 2366 Phase II Flight Tests of the Seibel YH24SE Helicopter, USAF No. 51-5113
Oct 22 1951
12 Report AFFTC-TR-58-15 ARDC XH-40 Air Force Flight Evaluation
May 1958
13 Proposal to the US Army for the Procurement of Model 720 Vol.I Hiller
Sep 1951
14 Proposal to the US Army for the Procurement of Model 720 Vol.II Hiller
Sep 1951
15 Report 22-A-14 H21A Fairing Evaluation Contract# AF33(038)-12881 Piasecki
Nov 28 1953
16 Report 1460.16 An Analytical Approach to Directional Stability of a Synchropter Using the Energy Method Kellett
Nov 1945
17 Report SD-529-1 Detail Specification for HTK-1K Helicopter Single Engine Contract# NOas 57-619c
Feb 25 1957
18 Report No.230.34 A determination of the Blade Motion About the Horizontal Hinge for a Syncropter Type Helicopter in Hovering Flight Kellett
Mar 1945
25
19 Report No. 1430.25 A Study of the Hovering Stability of the XH-17 Kellett
Sep 1948
20 Report AFFTC-TR-57-15 KAMAN K-600-3 Limited Flight Evaluation
Aug 1957
21 Report R-167 Photographs of the KAMAM Model K-600 Local Crash Rescue Helicopter for the USAF
Dec 1 1956
22 Report AFFTC-TR-58-1 Flight Evaluation of Directional Stability and Control of KAMAM K-600 with Various Empennage Configurations and Stability Augmentation
Feb 1958
23 HOK-1 Blueprint – General Arrangement Dec 22 1952 24 Report 163-K-3 Rotor Development XA-5 Helicopter
Engineering Data Contract# AF 33(038) 6099 Sep 10 1952
25 Report AFFTC-TN-59-4 Limited Performance Evaluation of the H-43A Helicopter
Mar 1959
26 Report R-550 HH-43F Huskie KAMAN Aug 1964 rev. May 18 1967
27 Report R-165 KAMAN Model K-600 Weight and Balance Report
Dec 1 1956
28 AN-260HB-3 Handbook Structural Repair Navy Model HOK-1 Helicopter
Nov 15 1955
29 AN-01-260HBA-2 Handbook Maintenance Instructions Navy Model HOK-1 Helicopter
Jul 15 1955
30 Report SER-5005 Actual Weight Report – Last Aircraft_ Fifty-Fifth Aircraft (Government #55-4944 – S.S. #55996) Model H-19D Contract# AF33(600)-28552
Jul 9 1956
31 Report AFFTC-TR-55-26 H-21C Phase IV – Performance Evaluation
Dec 1955
32 Report MCRFT-2222 Phase II Flight Tests of the Piasecki HRP-1 Helicopter
May 4 1949
33 Report MCRFT-2265 Accelerated Service Test of the HRP-1 Helicopter
Feb 24 1950
34 Report SER-2078 Stress and Motion Survey of S-55, YH19, HO4S-1 Rotor Head and Main Rotor Blades
Dec 15 1950
35 H-21C Blueprints Piasecki 1951 36 XR-8 Blueprints Kellett 1945 37 Report 1420.5 Proposal Specification for Three Place
Naval Helicopter Kellett Serial Number 16 and 16A Sep 1945
38 Report 1420.6 Proposal Specification for Three Place Naval Helicopter Kellett Serial Number 16B
Sep 1945
39 Report P-46 Flight Manual Performance Data Substantiation H-43B Local Crash Rescue Helicopter Contract# AF33(600)-36190 KAMAN
Feb 23 1959
40 KAMAN Model K-190 Utility Helicopter Brochure 1947 41 UH-2C Seasprite Brochure KAMAN Undated 42 BO-105 Boeing-Boelkow Helicopter Brochure Undated 43 Report 58-67 Three Place Instrument Trainer Helicopter May 1958
26
44 Report DR-212Preliminary Performance Report Model LZ-5-3 Helicopter DOMAN
Jul 27 1956
45 Do 132 Light Four-Seater Helicopter Brochure Dornier 1968 46 Report 8025-099-011 Research Study of a High
Performance Iriquois Helicopter Bell Apr 4 1961
47 Report R-414 Twin Turbine Utility Helicopter The Huskie III KAMAN
Oct 8 1962
48 Report 175-H-6 Preliminary Aerodynamic and Performance Analyses of MX-1660 Helicopter Rotor System Contract# AF33(600)-15613
Nov 1 1952
49 Report AR-117 Preliminary Aerodynamic Analysis of the Model A Quadrotor Convertiplane Convertawings
Nov 10 1952
50 Report R-164 A Proposal for the Local Crash Rescue Helicopter for the USAF KAMAN Model K-600
Dec 1 1956
51 Report 48-978-001 Performance Estimation for XR-12 Helicopter (Model 48) Bell
Dec 13 1946
11 1 AGARD Conference Proceedings No. 22 Fluid Dynamics of Rotor and Fan Supported Aircraft at Subsonic Speeds
Sep 1967
2 Report No. PB 111632 Rotary Wing Aircraft Handbooks and History Vol. 8 Mechanical Design and Description Contract# W33038 ac-21804(20695)
1954
3 Report No. F-TS-5408-RE The Power Requirements of the Ideal helicopter by G. Sissingh (from German)
Apr 1948
4 R. & M. No. 1730 The Flight of the Helicopter by H.B. Squire Air Ministry
1936
5 Report No. F-TS-1007-RE Investigation of the Influence of High Subsonic Velocities on the L/D of Rotary Wing Aircraft by G. Sissingh (from German)
Sep 1946
6 Report No. F-TS-1005-RE Theory of Oscillations of Blades in the Plane of Rotation by Dr. Kurt Hohenemser (from German)
Sep 1946
7 Aero Data Report No. 20 Wind-Tunnel Tests of Several Full-Scale Helicopter Rotor-Tip Lights at Subsonic Speeds
Apr 1954
8 Report No. 373 An Economical Technique for the Construction and Hovering Flight Evaluation of Dynamically Similar Helicopter Models Contract# Nonr27015 Princeton Univ.
Nov 1956
9 Report No. TB-707-S-2 Helicopter Handling Qualities Investigation Phase II Analysis of Helicopter Stability and Control Problem Part B Physical Discussion of Helicopter Handling Qualities Contract# NOa(s)-12151 Cornell
Jun 1955
10 Proposal for a Variable Stability Helicopter Cornell Nov 1957 11 Report No. D4-943-001 Preliminary Performance
Estimates for Proposed Helicopter (Model D-4) Bell Jan 9 1942
12 Report No. E-65 Bell Aircraft Corp. Wind Tunnel Tests of Nov 15 1945
27
a #8-25-44 Anti-Torque Propeller Georgia Tech 13 Report No. E-68 Wind Tunnel tests of a Model 47 Anti-
Torque Propeller Georgia Tech Feb 1946
14 Report No. E-72 Bell Aircraft Corporation Wind Tunnel Tests of a No. 47 Anti-Torque Propeller Georgia Tech
Apr 1946
15 Report No. E-79 Wind Tunnel Tests of an X47-642-010-4 Straight Twist Anti-Yorque Propeller Georgia Tech
Jun 1946
16 Aero Data Report No.774 Report C-246 Wind-Tunnel Tests of a 0.10-Scale HRP-2 Helicopter Without Rotors Part I – Longitudinal and Lateral Characteristics with Original Afterbody
Aug 1949
17 Report No. 59V-10-3 Non-Uniform Rotor Blade Free and Forced Uncoupled Flap Bending Aero-Elastic Vibrations – Theory- Contract# AF 33(616)-238 Kellett
May 1953
18 Local Crash Rescue Considerations Brochure Bell Undated 19 Instrument Flight Investigation in Helicopters by Owen Q.
Niehaus Bell Undated
20 Practical Instrument Flying in the Helicopter by Joseph A. Cannon & Owen Q. Niehaus Bell
Undated
21 Report No. NAES INSTR 38-47 Development of Helicopter Attitude Indicator
Dec 1 1947
22 YH-16B Vibration Study without Enclosures Undated 23 Report No. SM-18311 Helicopter Vibration 1945 Douglas Apr 9 1954 24 Report No. W.T.T.#197 Aerodynamic Characteristics of
the 1/12 Scale Model of the XR-6 Helicopter Fuselage Contract# W534 ac-35340 Sikorsky
Oct 22 1943
25 Elementary Aerodynamics of Compound Rotorcraft Chapters II, III and IV
Undated
26 Report No. HTC-AD-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 5 Stability, Control and Flying Qualities Hughes
May 1966
27 Report No. 30-929-101 Engine & Rotor Tests in Hovering Flight Bell
Jul 23 1943 Dec 23 1944
28 Report No. GAE 52-4 ATI 162780 Effect of Disc Loading on the Payload Range Spectrum of a 60,000 Pound Helicopter AFIT
Aug 1952
29 Report No. YA-1532 Aerodynamic Performance of the M30 Quadrotor Transport Helicopter Convertawings
Undated
30 Report No. AF TR 6272 Draft Performance Testing Methods for Helicopters
Undated
31 Report No. 157X90-1 Proposed Mechanical Stabilization for the Kaman H-43B Helicopter Kaman
Dec 29 1958
32 Report No. 66A-10-9 Theoretical Study of a Helicopter Rotor Employing Large Flapping Hinge Offsets; Aerodynamics Kellett
Feb 15 1954
33 Report No. R-598 Model K-120 Composite Helicopter Jul 30 1965
28
5
10
15
20
25
Brochure Kaman 34 Report No. LR 20807 Composite Aircraft Program
Retracted Rigid Rotor Lockheed-California Jul 1967
HELICOPTER ARTICLES AND PHOTOS 12 1 Helicopter History – Early Helicopters Photos & Articles Undated
2 Helicopter History – German Helicopters Articles Undated 3 Helicopter History – Germany 1939-1945 Articles,
Diagrams 1939-1945
4 Helicopter History – Historical Resume 1483-1954 Undated Bibliography of Rotary Wing Aircraft Undated
6 Helicopter History – Summary of Rotary Wing Projects of Aircraft Projects Section, Rotary Wing Branch
Jan 1947 – Feb 1947
7 Principles of the Helicopter by Dr. Alexander Klemin Articles
Undated
8 Helicopter Pamphlets/Photos Super Puma as332, ASTAR 350C, SA365 dauphin 2, UN-8B
Undated
9 AHS Semi Technical Bulletin Number 1 by James A. J. Bennett
May 1944
Helicopter History – 2 articles 1) Contemporary Helicopter Layouts; 2) From Rotorcraft Magazine – Specifications
1954
11 Lindenbaum Presentation to AHS The Autogiro in Prospective and Advanced Design Possibilities
May 2 1974
12 Helicopter History – Miscellaneous Articles, Proposals and Photos
Undated
13 Helicopter Transparencies for The Helicopter – A Historical Perspective – by Lindenbaum
Sep 15 1981
14 Journal of the AHS Volume 1, Number 1 Jan 1956 Helicopter Pilot’s Aerodynamic Outline – Bell Helicopter Training School
1951
16 Helicopter History – BELL Photos Undated 17 Military Products Reference Data – BELL Undated 18 Helicopter History – BELL Pamphlets and Photos Undated 19 Helicopter History – BOEING VERTOL Pamphlets and
Photos Undated
Helicopter History –BOLKOW Helicopter Articles and Pamphlets
Undated
21 Helicopter History – CESSNA Yh-41 Photo Undated 22 Helicopter History – DOMAN Articles and Photos Undated 23 Helicopter History – DORNIER (German)Photos Undated 24 Helicopter History – FI RESTONE Photos Undated
Helicopter History – FOCKE (German)Photo Undated 26 Helicopter History – GYRODYNE Photos Undated 27 Helicopter History – HILLER Photos and Newsletter Nov 1969
28 Helicopter History – HUGHES Articles, Photos and Undated
29
Pamphlets 29 Helicopter History – KAMAN Photos and Articles Undated 30 Helicopter History – KAMOV (Russian) Photos and
Articles Undated
31 Helicopter History – KELLETT Photos Undated 32 Helicopter History – LANDGRAF Article and Photo 1944 33 Helicopter History – LOCKHEED Pamphlet and Photo Undated 34 Helicopter History – McCULLOCH MOTORS Proposals
MC-9 Helicopter 1952
35 Helicopter History – McDONNELL (early) Photos Undated 36 Helicopter History – MIL (Russian) Articles Undated 37 Helicopter History – PIASECKI Photos Undated 38 Helicopter History – PLATT-LEPAGE Photos Undated 39 Helicopter History – SEIBEL Photo Undated 40 Helicopter History – YAK and ANTONOV Articles 1961
13 1 No. X-417-13 Model Specification for Army Air Forces Helicopter Model YR-1A (Manufacturer’s Model PL-7) Platt LePage
Jan 16 1945
2 FT-56R-67 AD820490 Naval Air Test Center TR Final Report Evaluation of the Bell Model 206A(Jetranger) Light Turbine-Powered Helicopter
Sep 14 1967
3 No. X-417-14 Rotary Wing Aircraft Specifications Vol. II AAF Model XR-6A
Feb 20 1945
4 McDonnell Model 4JP2-MD-5 Blueprints Aug 19 1957 5 Report 5930A Model Specification Helicopter Final
Corrected data Model XR-5 Contract# W535 ac-29845 and DA W535 ac-2514 Sikorsky
Dec 1 1944
6 Report SER-130 Model Specification Helicopter (Tentative) Model YR-5C Contract#W535 ac-41023 Sikorsky
Mar 22 1945
7 Report SER-499A Model Specification Helicopter Model R-5D Contract# W535 ac-41023 Sikorsky
Feb 20 1947
8 Report SER-257 Airplane-Helicopter AAF Model R-5F Sikorsky
Dec 12 1946
9 AF TR No. 6163 XH-10 Helicopter Development of Kellett Model
May 1950
10 Report SER-1556 Model Specification Helicopter Model E-5G Sikorsky
Nov 22 1948
11 Report 204-947-030 Detail Specification for H-40A Utility Helicopter Bell
Jan 10 1957
12 Report 54-947-001 Model Specification XR-15 Bell May 22 1946 13 Report SER-3309 Detail Specification, Model H-19D
Helicopter, 12-Place, Single Engine – Sikorsky Nov 17 1953
14 Report SD-530-1-6 Detail Specification for Model UH-2B FY 1964
30
(HU2K-1U) 15 Sikorsky Contractor Technical Compliance Conference
Model H-34A Helicopter Jan 24-26 1955
16 Report SD-516-1 Detail Specification for Model HUL-1 Helicopter Class HU (Single Engine) Contract# NOas 55485
Mar 22 1955
17 Model XH-3 Blueprints Higgins Sep 28 1945 18 Report 133 Detail Specification for Design and
Construction of H-3 Helicopter Higgins Sep 27 1945
19 Report R-100 Model Specification Helicopter Model X-2A Rotor-Craft Corp.
Mar 14 1945
20 Report 57-123 Detail Specification for Model XROE-1 Rotorcycle Class RO Hiller Helicopter
Undated
21 Report SD-511 Detail Specification for Model XROE-1 Rotorcycle Class RO Contract# NOas 55-387c
Sep 29 1954
22 Report S-157-b Model Specification, Model XH-26 Single-Place Helicopter Contract# AF33(038)-27961
Jun 8 1951
23 Development of the XH-26 Helicopter Sep 1956 24 NASA TN D-3060 Flight Tests of the One Man Helicopter
and a Comparison of Its Handling Qualities with Those of Larger VTOL Aircraft
Oct 1965
25 XH-26 Development Engineering Inspection Sep 15-16 1953 26 The XA-5 Pulse Jet Powered Helicopter Jun 1 1950 27 The Pinwheel Rocket Propelled Strap on the Back
Helicopter Rotor-Craft Presentation Undated
28 Gyrodyne Reconnaissance/Surveillance Drone, Model QH50C Letter with Attached Brochure
May 7 1965
29 Report PTR AC-4031 Contractor’s Part II Structural and Aerodynamic Demonstration of Goodyear Model GA400R-3J One Man Helicopter, Report no. 1 Final Report
Apr 26 1957
30 Hughes 500 Helicopter Brochure Undated 31 Report 22-X-201 Rev. C Model Specifications H-21B
Helicopter Piasecki Mar 16 1951
32 Detail Specification for Model HUP-2 Helicopter Class HU Single Engine, Twin Rotor Contract# NOas 51-035
Nov 19 1951
33 NAVAER SD-418 Detail Specification for Model XHJP-1 Helicopter Class HJ (Twin Rotor) Contract# NOa(s)-7935
Mar 4 1946
34 Report 190-1 Specification for Model 190 Helicopter Hughes
Apr 5 1951
35 Report SD-363-2 Detail Specification for Model HRP-2 Helicopter Class HR (Twin Rotor) Contract# NOa(s) 9978
Jun 21 1948
36 Report SER-5004 Detail Specification, Model H-19D Helicopter, 12-Place, Single Engine Contract#AF33(600)33862 Sikorsky
Jun 29 1956
37 HC-65A-1 Mechanical Description and Aerodynamic Dec 5 1950
31
Analysis Heli-Craft, Ltd. 38 Report MCRFT-2270 Phase II Flight Tests of the Sikorsky
H-5H Helicopter Mar 10 1950
39 Helicopter (unnamed) Configuration Drawings with Boeing 502-10C Gas Turbine
Undated
40 Report 161518 and 161523 CIRCOL OFFLINE OUTPUT 3 reports
Aug 1972
41 HUL-1 Drive Assembly Blueprints Bell Mar 18 1955 42 Report SER-2556 Summary Report Long Range
Helicopter Design Study Contract AF33(616)-2628 Two Copies
May 27 1955
43 Report SER-2553 Long Range Helicopter Results and Analyses Compound Helicopter Configuration
May 16 1955
44 NAVWEPS 01-260HCA-2-4 Handbook Maintenance Instructions Navy Model HU2K-1 Helicopter – Transmission System
Dec 1 1961 rev Jul 1 1962
45 WADC TR 55-468 General Design Study of Performance Improvement of Helicopters
Jan 1956
46 KAMAN Aircraft Annual Report 1956 1956 47 Monte-Copter, Inc. Press Release/Brochure Jan 13 1966 48 NAVWEPS 01-260HCA-2-5 Handbook Maintenance
Instructions Navy Model UH-2A/UH-2B(HU2K-1) Helicopter – Rotor System
Oct 15 1962 rev Feb 1 1963
49 Model QH-50C Drone Description and Capabilities Gyrodyne
Sep 17 1964
50 Boeing-Vertol Model-137 Dynamics Jan 27 1961 51 Boeing-Vertol Model-137 Power Plant Analysis Jan 27 1961 52 Boeing-Vertol Model-137 Reliability Jan 27 1961 53 Grumman Design 242 Tri-Service VTOL Aircraft Proposal
Drawings Apr 3 1961
54 Grumman Design 242 Tri-Service VTOL Aircraft Carrier Design Compromises
Apr 3 1961
14 1 Military Products Reference Data Bell Helicopter Oct 1 1973 2 Report ADR-01-03-61.1 Aerodynamic Design & Stability
Analysis of a Rotating Wing Towed Glider Grumman Aug 1961
3 AFFTC-TR-60-2 Appendix III YHO-2HU Air Force Flight Evaluation
May 1960
4 Report No. 130-13 A Chart Method for Calculating Helicopter Performance – II Kellett
Nov 1946
5 Rocket Propeller Mini-Copter C.A. 1975 6 Report 22-A-05 Report on Methods and Computations
Used in Selecting Rotor Physical Characteristics and Efficiencies for the H-21 Helicopter Contract# AF33(038)12881 Piasecki
Apr 1951
7 Report 42-A-03 H-21B & C Helicopter Rotor Blade Dec 11 1951
32
Airload Report Contract# AF33(038)-12881 Piasecki 8 Report 22-S-41 Control System Analysis – Rotor
Contract# AF33(038)-12881 Piasecki Jan 15 1952
9 Report 42-S-10 H-21B & C Rotor Blade Stress Analysis Contract# AF33(038)-12881 Piasecki
Feb 13 1952
10 WADC TR 52-256 Low-Range Air-Speed Indicator for Helicopters
Oct 1952
11 Report MCREXB-582-7-2 Stress Survey of Sikorsky H-5 Main Rotor Blades
Jan 19 1949
12 Report SER-246 Preliminary Experimentation Single Blade Rotor Model Sikorsky
Apr 7 1945
13 Nagler Rocket Rotor System 1951 14 Presenting the Firestone Helicopter 1946 15 Proposal 157-7 Description of Container for the Aerial
Delivery of the XH-26 Collapsible Helicopter Jan 25 1952
16 Bell H-13 Helicopter Brochure Undated 17 American Helicopter Model 175 brochure Undated 18 Air Material Command Letters (5) 1947-1950 19 McCulloch Motors Proposal – R&D Projects Feb 24 1953 20 Blueprint Packet KAMAN Helicopter 1947 21 Helicopter Research Laboratory Blueprints and Notes –
Lindenbaum 1947
22 Helicopter Material – General File – Lindenbaum Undated 23 Miscellaneous Blueprints C.A. 1945 24 Flight within Earth’s Atmosphere May 16-18 1966 25 AIAA Paper No. 69-199 Research and Development of
Advanced Rotorcraft Concepts by Evan A. Fradenburgh Sikorsky
Feb 17-19 1969
26 Multivariable Search and Its Application to Aircraft Design Optimization by W.Z. Stepniewski & C.F. Kalmbach, Jr. Boeing-Vertol
Sep 15 1969
27 Present and Future Roles of the Helicopter by L.L. Douglas & J.J. Schneider Boeing-Vertol
May 1965
28 The Piasecki Story of Vertical Lift Undated 29 An Investigation into the Rotor Torque Problem of the
Hafner Helicopter Sep 1938
30 Specification – Hafner Helicopter P.D.6 Sep 1938 31 Specification – Hafner Helicopter P.D.7 Sep 1938
HELO PHOTOS, BROCHURES 15 1 Box of Photos Undated
2 AIAA Symposium – Evolution of Aircraft Wing Design Mar 18-19 1980 3 Charts – Rotary Wing 1934-1946 4 Airplane Charts & Data C.A. 1944 5 Photos – Early Helicopters Various 6 Helicopter Photos and Articles Various
33
7 Advancing Blade Concept 1966 8 CH-53E Super Stallion Brochure Sikorsky Undated 9 Sikorsky UTTAS Brochure Oct 1975 10 Sikorsky 76 Brochure Undated 11 Helicopter Articles Various 12 Helicopter Brochures Various 13 R-4 First Landing on Ship (Photos) Undated 14 Theory of Flight of Sikorsky Helicopters Jan 16 1953 15 AHS Quarterly Vol. 1 No. 1 Jan 1946 16 Pilot Operating Instructions for 1) R-5A/HO2S-1 and 2) R
6A and HOS-1 1944-1945
17 General Comments on Sikorsky R-4, R-5, R-6 Helicopters Dec 18 1945 18 Report NO. X-417-13 Rotary Wing Aircraft Specifications
Vol. I (Model YR-1A) Platt-LePage Jan 16 1946
EARLY HELICOPTERS & TOWED HELICOPTERS 16 1 Report No. TB-641-F-1 Transient Responses of an H-13
Helicopter to Longitudinal Stick Pulses as Measured in Flight Cornell
Nov 15 1950
2 Kaman K-800 Brochure Undated 3 Report No. FTC-TIM-68-1006 Helicopter Range/Speed
Extension, Mother-Daughter Approach May 1968
4 Report of Helicopter Aerial Tow Accident of Aug 25 1950 with Photos
Oct 6 1950
5 Powered Long Line Loiter System (POLLLS) documents and Photos Aerial Mobility Inc.
1994
6 Report No. 55McC103R Full Scale Investigation of Rotor Hub Fairing for a Sikorski H-5 Rotor Hub Contract# AF 18(600)-176
Apr 1955
7 Effects of Operating and Design Variables on Helicopter Performance by Alfred Gessow
Jan 27 1949
8 Helicopter Brochures Undated 9 Mechanical Description and Aerodynamic Analysis of
Model HC-65A Helicopter Utility Metal Products, Inc. Jul 16 1954
10 MI-26 Halo as Viewed by an American Presentation Jan 20 1997 11 AFFTC-TR-59-41 High Altitude Take-Off and Landing
Tests of the H-37A Equipped with Narrow Chord Blades Dec 1959
12 The de Bothezat Helicopter Articles and Photos C.A. 1922 13 Flight Within Earth’s Atmosphere – VTOL Aircraft 1975
1985 Briefing Boeing-Vertol May 16-18 1966
14 Specification – Hafner Gyroplane A.R.4 Sep 1938 15 Report No. SER-1775 Tow Tests of H-5 (S-51) Helicopter
Contract# AF 33(038)-7878 Oct 19 1950
16 Report of Test Project NR AVN 5258/59(D) Desert Test of the YHO-2HU Helicopter
Oct 14 1959
17 Performance Substantiation for Kinedyne Proposal Cessna Feb 5 1958
34
18 Comparative Evaluation of the Kinedyne 1958 19 Proposal Model CH-3 Kinedyne Apr 21 1958 20 AHS 13th Annual Forum Theoretical and Experimental
Study of the Coupled Flap Bending and Torsion Aero-Elastic Vibrations of a Helicopter Rotor Blade by Peter F. Leone Vertol
May 8-10 1957
21 H-5D Helicopter Aerial Tow Tests Letter Oct 25 1948 22 Report No. E-57-1065 Flight Evaluation of the Bell Model
47G-2 Hiller Sep 9 1957
23 MIL-S-8698(ASG) Structural Design Requirements, Helicopters
Aug 1 1950
24 Report No. 127A90-4 The Effects of Airframe Shape on Helicopter Performance and Stability Contract# AF 33(616)-5420 Kellett
Jul 31 1958
25 Report No. D34-947-001 Specification for Single Engine Two Bladed helicopter Bell
Sep 29 1945
26 Report SER-257 Model Specification – Helicopter R-5F Sikorsky
Dec 12 1946
27 AHS Western Forum Air Force Test Experience with Turbine Powered Helicopters by James S. Hayden AF Flight Test Center
Sep 25-26 1958
28 AFFTC-TR-59-33 YH-40 Performance Evaluation Jan 1960 29 Introduction to Helicopter Aerodynamics Vol. 1 –
Performance by W.Z. Stepniewski Piasecki 1950
30 Report No. SER-86 Description of Sikorsky Experimental Blades Contract W535 AC-41023 Sikorsky
Mar 13 1945
31 Final ER on Various Helicopter Rotor Tip[-Path Plane Data and Transmission Systems Contract# NOas 54-485C
1955
32 AFFTC-TR-60-57 HU-1 Stability and Control Evaluation Dec 1960 33 Wirtschaftlichkeit des Hubschrabers by W. Lambert, E.
Skubinna & H. Brusberg (in German) Sep 1959
34 Lateral-Directional Stability and Control of Helicopters. Effect of Design Parameters by W. Just, H. Georgi & U. Schwellinger
1958-1959
35 Helicopter – Miscellaneous Various 36 Project No. PTR AD 3097 Navy Evaluation of the Model
YHC-1A Helicopter Report No. 1 Final Report May 5 1960
37 USAAVLABS TR 69-78 A Flight Envelope Expansion Study for the XH-51A Compound helicopter
Oct 1969
38 WADC TN 59-88 YH-40 (UH-1) Helicopter Extreme temperature Arctic Evaluation
Aug 1959
39 WADC TR 55-438 The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part III Contract AF 33(616)-5361
Sep 1959
17 1 NASA TR R-41 Normal Component of Induced Velocity 1959
35
for Entire Field of a Uniformly Loaded Lifting Rotor with Highly Swept Wake as determined by Electromagnetic Analog
2 NASA TR R-71 Jet-Boundary Corrections for Lifting Rotors Centered in Rectangular Wind Tunnels
1960
3 NASA TT F-43 A Vibration Absorber for Two-Bladed Helicopters (from French)
Nov 1960
4 NASA TT F-55 Response of a Helicopter Rotor to an Increase in Collective Pitch for the Case of Vertical Flight (from French)
Jan 1961
5 NACA TN 2870 Power-Off Flare-Up Tests of a Model helicopter Rotor in Vertical Autorotation
Jan 1953
6 NASA TN D-31 A Dynamic Model Investigation of the Effect of a Sharp-Edge Vertical Gust on Blade Periodic Flapping Angles and Bending Moments of a Two-Bladed Rotor
Sep 1959
7 NASA TN D-43 An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect
Sep 1959
8 NASA TN D-58 The Effect of Various Combinations of Damping and Control Power on Helicopter Handling Qualities During Both Instrument and Visual Flight
Oct 1959
9 NASA TN D-186 A Flying-Qualities Study of a Small Ram-Jet Helicopter
Apr 1960
10 NASA TN D-245 Compressibility Effects on the Hovering Performance of a Two-Bladed 10-Foot-Diameter Helicopter Rotor Operating at Tip Mach Numbers up to 0.98
Apr 1960
11 NASA TN D-251 A Summary of Operating Conditions Experienced by Two Helicopters in a Commercial and a Military Operation
Apr 1960
12 NASA TN D-335 Full-Scale Wind-Tunnel Tests of Blowing Boundary-Layer Control Applied to a Helicopter Rotor
Sep 1960
13 NASA TN D-382 Effects of Blade Cut-Out on Power Required by Helicopters Operating at High Tip-Speed Ratios
Sep 1960
14 NASA TN D-393 Measurements of the Time-Averaged and Instantaneous Induced Velocities in the Wake of a Helicopter Rotor Hovering at High Tip Speeds
Jul 1960
15 NASA TN D-394 Equations for the Induced Velocities Near a Lifting Rotor with Nonuniform Azimuthwise Vorticity Distribution
Aug 1960
16 NASA TN D-432 A Summary of Operating Conditions Oct 1960
36
Experienced by Three Military Helicopters and a Mountain-Based Commercial Helicopter
17 NASA TN D-458 Experimental Smoke and Electromagnetic Analog Study of Induced Flow Field About a Model Rotor in Steady Flight Within Ground Effect
Aug 1960
18 NASA TN D-464 Effects of Control-Response Characteristics on the Capability of a Helicopter for Use as a Gun Platform
Sep 1960
19 NASA TN D-534 Hovering Measurements for Twin-Rotor Configurations with and Without Overlap
Nov 1960
20 NASA TN D-633 An Analysis of the Flapwise Bending Frequencies and Mode Shapes of Rotor Blades Having Two Flapping Hinges to Reduce Vibration Levels
Dec 1960
21 NASA TN D-742 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for Flying-Crane Type of Helicopter
Apr 1961
22 NASA TN D-737 Some Recent Studies in Structural Dynamics of Rotor Aircraft
Mar 1961
SERIES V: Helicopter Aerodynamics, 1918-1993
Box File Description Date
HELICOPTER AERODYNAMICS AND THEORY 18 1 TSEAL-2-4202-2-23 Calculated Directional Stability
Characteristics of XR-8 Helicopter Contract# W535 ac40711
20 Mar 1945
2 Report No.ENG-6838 Chart Method for Calculating Helicopter Performance Project MX-558 Kellett
16 Jan 1945
3 UAAAMRDL TR 72-16 An Analytical Evaluation of the Controllable Twist Rotor Performance and Dynamic Behavior Contract# DAAJ02-67-C-0068
May 1972
4 The Boundary Layer and Skin Friction for a Figure of Revolution at Large Reynolds’ Numbers –Article – Dr. Norton B. Moore
1935
5 NACA TN-2318 Full Scale Tunnel Investigation of the Static-Thrust Performance of a Coaxial Helicopter Rotor
Mar 1951
6 NACA TN 3236 Wind-Tunnel Studies of the Performance of Multirotor Configurations
Jun 1954
7 Report ACR No. L4H07 Charts for Estimation of the Characteristics of a Helicopter Rotor in Forward Flight I-Profile Drag-Lift Ratio for Untwisted rectangular Blades
Aug 1944
8 Report ACR No. L5E04 Charts for Helicopter Performance Estimation
Aug 1945
9 NACA Report No. 538 Altitude-Pressure Tables Based on 1942
37
the United States Standard Atmosphere 10 Report No.SC-4139(TR) Stability of an Aerodynamic
Body with a Rotor Dec 1957
11 NACA TN 2665 An Extension of Lifting Rotor Theory to Cover Operation at Large Angles of Attack and High Inflow Conditions
Apr 1952
12 NACA TN 3323 Charts for Estimating Performance of High-Performance Helicopters
Jan 1955
13 NACA TN 3482 Supplementary Charts for Estimating Performance of High-Performance Helicopters
Jul 1955
14 Report No. FT-67R-67 NATC Evaluation of the Hughes OH-6A (Cayuse) Light Turbine-Powered Helicopter
Oct 17 1967
15 TM 816 The Gyroscope – Its Principles and Its Possibilities by Louis Breguet
Jan 1937
16 Historic Rotorcraft – Kellett Collection Oct 17 1954 17 Helicopter Fundamentals by Wayne Wiesner Jan 1955 18 NACA Report No. 20 Aerodynamic Coefficients and
Transformation Table 1918
19 NACA Report No. 311 Aerodynamic Theory and Test of Strut Forms
1929
20 NACA Report No. 335 Aerodynamic Theory and Test of Strut Forms – II
May 1929
21 NACA Report No. 716 A Simplified Theoretical Method of Determining the Characteristics of a Lifting Rotor in Forward Flight
1941
22 Biological and Aerodynamic Problems of Animal Flight Article by Erich von Holst & Dietrich Kuchemann
Jun 13 1941
23 Results from the Deutsche Forschungsanatalt Fur Segelflug Smoke Tunnel Article by A. Lippisch
Dec 15 1938
24 NACA TN 4409 Flight Measurements of the Vibration Experienced by a Tandem Helicopter in Transition, Vortex-Ring State, Landing Approach and Yawed Flight
Sep 1958
25 Introduction to Rotorcraft Part I & II by Franklin D. Harris 1994 26 Role of the Rotary Wing in Future Short-Haul
Transportation Pamphlet Lockheed Undated
27 NASA TN D-4820 A Hovering Investigation of an Extremely Flexible Lifting Rotor
Oct 1968
28 Sketch of Hiller 12C Helicopter Undated 29 Report No. R-700 Analytical Study to Determine Optimum
Design Criteria of Non-Servo Flap Controlled Rotors Contract# Now 64-0488f Kaman
Jun 1967
30 Report No. FFA 123 Disk Approximation for a Helicopter Rotor in Forward Flight
1972
31 Report No. 065298 CIRCOL OFFLINE OUTPUT – General Design of the Dornier Tail Rotor System
Aug 24 1973
32 FSTC-HT-23-480-72 Autorotation of Coaxial Helicopters Aug 24 1972
38
Translation (from Russian) 33 FSTC-HT-23-1174-01 Light Turbine Helicopter DO-123
Translation (from German) Dec 14 1972
34 FSTC-HT-23-107-73 On Cause of Vibrations in Helicopters translation (from German)
Aug 16 1973
35 Report AFFDL-TR-69-113 A Method for Calculating Helicopter Vortex Paths and Wake Velocities
Jul 1970
36 NASA CR-1672 Nonlinear Actuator Dick Theory and Flow Field Calculations, Including Nonuniform Loading
Sep 1070
37 Cessna CH-1 Helicopter Pamphlet Undated 38 Report No. EX-0-2 Studies Relative to the Development of
a One-Man Helicopter Part II Performance, Flying Qualities, Powerplants and Fuels Contract# Nonr 611(00) Amendment 1
Jan 20 1954
39 Report No. 47-947-039 Detail Specification for Bell Model 47J Four Place Helicopter
Sep 1 1955
40 Development of the OH-6A for Maximum Performance and Efficiency
May 13-15, 1964
41 US Army OH-6A Pamphlet Undated 42 Presenting the Firestone Helicopter Pamphlet Undated 42 Report No. EX-0-1 Studies Relative to the Development of
a One-Man Helicopter Part I Contract# Nonr 611(00) Amendment 1
Sep 30 1953
44 Proposal for a Multi-Purpose Turbine Powered Helicopter Model 1082 Pamphlet Hiller
Jan 1958
45 Report No. 55-77 Two Place Observation Helicopter Preliminary Design Study Contract# DA 44-177-TC-421 Hiller
Aug 1957
46 Report No. AU-74 Revision A Helicopter Model Specification 1 Place, Single Engine, Liaison Type Model GA-45B (XR-9) Contract# W-33-038-1708
Dec 20 1943
47 Report No. 63-35 A proposal for a Twin-Engine, High-Performance, Light Observation Helicopter OH-5B
Apr 1963
48 ABC(Advanced Blade Concept) Meeting at ARPA (Advanced Research Projects Agency) Notes
Mar 1971
49 Helicopter Medical Evacuation Techniques at Toulouse Hospital Trip Report
Jul 11 1969
50 Optimization of Design Data for Reaction Drive Helicopters Translation (from German)
Jan 1970
51 FSTC-HT-23-1269-72 Method of Decreasing Vibration in Rotary Wing Aircraft Translation (from Russian)
Jun 19 1972
52 Report No. 8011-099-002 The Weights of Very Large Rotors for Nuclear Powered Helicopters
Apr 23 1959
53 Report No. FTC-TR-69-6 Slope Landing Tests with the CH-3E Helicopter
Apr 1969
54 Report No. 150-P-1006P Proposal to Establish the Weight Jan 1973
39
of a Large Reaction Drive Helicopter Hughes 55 Optimum Pitch Rotor Presentation Hughes Undated 56 Sikorsky S-67 Blackhawk Article Fall 1970 57 Your Flight in the Lockheed Rigid Rotor Helicopter Undated 58 SA 341 Gazelle Helicopter Brochure c.a. 1968 59 Helicopter Pamphlets (Brantley, Kaman, Hughes, Bell,
Boeing, Vertiflite) (13 items) Undated
60 Planning Purpose Proposal for Developmental Research of the Lockheed ABIL (Automatic Blowing Inducted Lift) Rotor
Oct 14 1969
61 Investigation of CH-3E Reynolds Number Effects and Gross Weight/Pressure Ratio Test Techniques
Dec 1968
62 State of the Art Advancement in Helicopter Design (Rigid Rotor) Lockheed
Undated
63 1969 IR&D Studies Aerodynamic Research Rotor Performance Methodology
1969
64 The Helicopter Rotor at High Mach Numbers May 10-12, 1967 65 Rotary Wing Boundary Layer and Related Researches Sep 11-13, 1967 66 Variable Deflection Thrust (VDT) Fluidically Controlled
Rotor System Honeywell 9D-F-1 Mar 13 1969
67 Development of the Kinematic Focal Isolation System for Helicopter Rotors Bell
May 1968
68 Fairchild Hiller 68-4 Reverse Velocity Rotor Task Undated 69 Fairchild Hiller Reverse Velocity Rotor Task 7 Documents 1968 70 Fairchild Hiller 68-7 Desensitized Rotor System Study
Volume I Dec 31 1966
71 Report No. R-846 The Effects of Material Properties on Helicopter Rotor Blade Frequencies
Mar 1970
72 The Flapping/Feathering Ratio of a Second Harmonic Input for an 8 Foot Diameter 4 Blade Articulated Rotor
Apr 24 1972
18A 1 HTC-AD 72-57 150-A-1005P Proposal for Optimum Pitch Rotor System – Analysis and Wind Tunnel Model Program Hughes
Jun 1972
2 HTC-AD 72-57 Supplementary Information to the OPR Proposal for Analysis and Wind Tunnel Model program Hughes
Jul 1972
3 HTC-AD-72-57 150-A-1005P Part II Supplemental Information to the OPR Proposal for Analysis and Wind Tunnel Model Program Hughes
Undated
4 RPV – OPR Remote Piloted Vehicle with Optimum Pitch Rotor System
Mar 1973
ROTORS, AHS FORUM REPORTS
40
19 1 Report No. 360.1 Transport Helicopter Operating Cost Analysis Methods Contract# Nonr-1340(00)
Nov 30 1955
2 26th Annual National Forum of the AHS– An Investigation of the Need for Improved Displays in Heavy-Lift Helicopters by Archie T. Sherbert Jr, - Boeing-Vertol
Jun 1970
3 27th Annual National V/STOL Forum of the AHS– A Method for Predicting Helicopter Wake Geometry, Wake-Induced Flow and Wake Effects on Blade Airloads by S.G.Sadler – Rochester Applied Science Assoc.
May 1971
4 27th Annual National V/STOL Forum of the AHS– Tip Vortices – Velocity Distributions by N.A.Chiger & V.R.Corsigia – NASA Ames
May 1971
5 27th Annual National V/STOL Forum of the AHS– Rotor Stability Derivatives Determined From Wind Tunnel Tests of an Instrumented Helicopter by Robert E. Rohtert & Sally V. LaForge – Hughes Tool, Aircraft Div.
May 1971
6 27th Annual National V/STOL Forum of the AHS – HLH Primary Flight Control System Design by Richard W. Sanford, Peter R. Venuti & Derek Wood – Boeing-Vertol
May 1971
7 27th Annual National V/STOL Forum of the AHS – Application of a Lifting-Surface Theory to the Calculation of Helicopter Airloads by Wayne Johnson – MIT
May 1971
8 27th Annual National V/STOL Forum of the AHS – A Study of the Effects of Nonuniform Swash-Plate Stiffness and Out-of-Blade Track on Rotor Dynamics and Stability by Vincent J. Piarulli – Rochester Applied Science Assoc.
May 1971
9 27th Annual National V/STOL Forum of the AHS – The Method of Multiblade Coordinates in a Linear Analysis of Lifting Dynamic Stability and Gust Response at High Advance Ratio by Sheng-Kuang Yin & Kurt H. Hohenemser – Washington Univ.
May 1971
10 27th Annual National V/STOL Forum of the AHS – Prediction of Control Loads Due to Blade Stall by F.J. Tarzanin, Jr. - Boeing-Vertol
May 1971
11 27th Annual National V/STOL Forum of the AHS – Preliminary Development of an Active Transmission Isolation System by Paul W. vonHardenberg & Paul B. Saltanis – Sikorsky
May 1971
12 27th Annual National V/STOL Forum of the AHS – Analytical Investigation of the Effects of Blade Flexibility, Unsteady Aerodynamics, and Variable Inflow on Helicopter Rotor Stall Characteristics by E.D. Bellinger – United Aircraft
May 1971
13 27th Annual National V/STOL Forum of the AHS – May 1971
41
Detailed Aerodynamic Measurements of a Model Rotor in the Blade Stall Regime by Richard K. Fisher, Jr. & W.J. McCroskey – Boeing & USArmy Air Mobility R&D Lab
14 27th Annual National V/STOL Forum of the AHS – Feel Augmentation and Sensitivity Control in High Speed Helicopters by Sean J. O’Connor - Sikorsky
May 1971
15 27th Annual National V/STOL Forum of the AHS – An Attack Helicopter Weapons Delivery System by John A. Simpson – United Technologies/Norden Division
May 1971
16 27th Annual National V/STOL Forum of the AHS – Head-Mounted Display/Control System in V/STOL Operations by Dr. Dora Dougherty & Hubert W. Upton – Bell Helicopters
May 1971
17 27th Annual National V/STOL Forum of the AHS – Day and Night Fire Power of the Cheyenne by Bernard J. Merritt & John C. Kirby – USAMC & Lockheed-Burbank
May 1971
18 27th Annual National V/STOL Forum of the AHS – The Night Rescue Terminal Navigation Problem by Cecil S. Richardson – Sikorsky
May 1971
19 27th Annual National V/STOL Forum of the AHS – Army Helicopter Performance Trends by Richard B. Lewis – USArmy Aviation Systems Test Activity
May 1971
20 27th Annual National V/STOL Forum of the AHS – The Boeing Model 347 Advanced Technology Helicopter Program by Frank H. Duke & W. Euan Hooper – Boeing-Vertol
May 1971
21 27th Annual National V/STOL Forum of the AHS – Strain Gauge Torquemeters for Use in Helicopter Transmission Systems by Dennis P. Hames – British Hovercraft Corp.
May 1971
22 27th Annual National V/STOL Forum of the AHS – Evaluation of Rotor Controls Designed for Increased Safety by Lawrence D. Barrett & John C. Mack – Boeing-Vertol
May 1971
23 27th Annual National V/STOL Forum of the AHS – Fail-Safety for the H-46 Rotor Blade by George H. Thompson & William L. Weiss – Boeing-Vertol
May 1971
24 27th Annual National V/STOL Forum of the AHS – Fatigue Strength Improvements in Ti-6A1-4V Forgings by John J. Lucas – Sikorsky
May 1971
25 27th Annual National V/STOL Forum of the AHS – AN/ASN-86 Inertial Navigation Set by J. B> Hughes – Litton Ind.
May 19-21 1971
26 Factors Affecting Fuel Control Stability of a Turbine Undated
42
Engine/Helicopter Rotor Drive System by C. Fredrickson, K. Sumford & C. Stephenson – Boeing-Vertol, AVCO/Lycoming & AVSCOM
27 TR AFFDL-TR-69-113 A Method of Calculating Helicopter Vortex Paths and Wake Velocities Air Vehicle Corp.
Feb 1970
28 26th Annual National Forum of the AHS – Collection and Analysis of Helicopter Combat Flight Loads Data from AH-1G Helicopters in Southeast Asia by F. Joseph Giessler & William T. Alexander – Technology Inc. & USArmy Aviation Materials Lab
Jun 1970
29 26th Annual National Forum of the AHS – The CH-47 Cruise Guide Indicator by W.P. Brown & H.H. Steinmann – Boeing-Vertol
Jun 1970
30 26th Annual National Forum of the AHS – Qualitative Report on Flight Test of a Two-Point External Load Suspension System by A.J. Hutto – Boeing-Vertol
Jun 1970
31 CAL Report BB-2584-S-1 On the Feasibility of Replacing a Helicopter Tail Rotor Contract# N00014-68-C-0241 NR212-182
Jul 1968
32 USAAVLABS TR 69-18 Measurement of Rotor Noise Levels and Evaluation of Porous Blade Tips on a CH-47A Helicopter Contract# DA 44-177-AMC-330(T)
Sep 1969
33 NASA TN D-742 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for Flying-Crane Type of helicopter
Apr 1961
34 NASA TN D-1517 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for a Utility Type of Helicopter
Dec 1 1962
35 5th Annual National Forum of the AHS – Design and Construction of the Cornell Fiberglass Helicopter Main Rotor Blades by Harold Hirsch – Cornell Aeronautical Lab.
May 12-13, 1949
36 AHS – Great Lakes regional Dinner Meeting Three (3) ARTICLES: 1) Results of Recent Rotor Blade De-Icing Test on Mt. Washington, Part I by Lt. Comdr. L. Carson Houser – USN Bureau of Aeronautics; 2) Results of Recent Rotor Blade De-Icing Test on Mt. Washington, Part II by Robert R. Lynn – Bell; 3) Helicopter Maneuver Loads in Relation to Recent Specifications and Tests by O. Q. Niehaus – Bell
Jan 7 1952
37 USAAVLABS TR 70-47 Analysis of Measured Helicopter Rotor Pressure Distributions Contract# DAAJ02-69-C0076
Sep 1970
38 NASA TN D-734 Considerations of Methods of Improving Apr 1961
43
Helicopter Efficiency 39 NASA TN D-759 Flight Investigation of Effects of
Selected Operating Conditions on the Bending and Torsional Moments Encountered by a Helicopter Rotor Blade
Apr 1961
40 FTC-TR-66-46 Determination of the Effects of Rotor Blade Compressibility on the Performance of the CH-47A Helicopter
Mar 1967
41 Report No. SG-1195-S-2 A Proposed Test Apparatus For Small Rotorcraft Vol. II Contract# DA-44-177-TC-440
Apr 1958
42 NASA TN D-458 Experimental Smoke and Electromagnetic Analog Study of Induced Flow Field About a Model Rotor in Steady Flight Within Ground Effect
Aug 1960
43 NASA TN D-534 Hovering Measurements for Twin-Rotor Configurations with and without Overlap
Nov 1960
44 NASA TT-F-43 A Vibration Absorber for Two-Blased Helicopters (translated from French)
Nov 1960
45 AMC F-TS-687-RE Stability in Hovering of the Helicopter with Central Rotor Control (Tr. From German)
Aug 1946
46 AMC F-TS-690-RE Contributions to the Dynamic Stability of Rotary-Wing Aircraft with Articulated Blades (tr. From German)
Aug 1946
47 AMC F-TS-692-RE The Pull-Up of the Helicopter (tr. From German)
Aug 1946
48 AMC F-TS-1002-RE The Dynamic Stability of Helicopters with Articulated Blades (Tr. From German)
Sep 1946
49 AMC F-TS-1004-RE The Theory of the Control of the Blade Angle of the Helicopter (Tr. From German)
Sep 1946
50 AMC F-TS-1006-RE Theory of Helicopter Control in Hovering Flight (Tr. From German)
Sep 1946
51 Report No. 179T80-2 An Investigation of VTOL Operational Problems Due to Downwash Effects Contract# Now 60-0450-f Kellett
Jun 12 1961
52 Report No. 20280-1 Proposal for the Study and Development of Design Criteria for High Speed Power Transmission Shafts Kellett
Jan 19 1961
53 Report No. 120X-10-1 Proposal – An Analytical Determination of an Optimum Rotor Blade Twist and Tip Speed for High Performance Helicopters Kellett
Feb 25 1957
54 Report No. 140X90-1 Proposal – Helicopter Instrument Flight Program Kellett
Feb 26 1958
55 Report No. 122V-90-1 Proposal-A Research Program for the Reduction of Helicopter Vibrations Kellett
Mar 15 1957
56 Report No. 1136 Charts for Determining the Aerodynamic Apr 1949
44
Characteristics of Jet Rotors in Hovering Contract AF 33 (038)-937, E.O. No. 582-164 McDonnell Aircraft
57 Report No. 1078 Charts for Estimating Blade Stall for Jet Rotors Contract# AF 33 (038)-937 McDonnell Aircraft
Mar 18 1949
58 Report No. 1079 Charts for Estimating the Autorotative Performance of Jet Rotors Contract# AF 33(038)-937 McDonnell Aircraft
Mar 18 1949
59 Report No. 248 A review of Rotor Induced Velocity Field Theory Contract# N6 onr-27015 Project NR 212-005
Jan 1954
60 AFFTC-TR-61-1 YHC-1A Flight Evaluation Feb 1961 61 AFFTC-TR-61-8 Limited Stability and Control Evaluation
of the S-62A Helicopter Mar 1961
62 Report No. 27-98-4 Report on Rotor Stability Contract# N156s 26506 Prewitt
Apr 20 1949
63 CAL Report No. 75 A Two-Dimensional Approximation of the Unsteady Aerodynamics of Rotor wings Cornell
Oct 1955
64 Report No. AD-210 613 The Computed Instantaneous Velocities Induced at the Blade Axes by the Skewed Helical Vortices in the Wake of a Lifting Rotor in Forward Flight Contract# Nonr 991(05) Georgia Tech
Mar 1959
65 Report No. 15-A-15 Report on Methods and Computations Used in Selecting Rotor Physical Characteristics and Efficiencies Contract# W33-038 AC 21399 Piasecki
Aug 9 1949
66 Report No. 15-A-15 Appendix 14-A-03Report on Methods and Computations Used in Selecting Rotor Physical Characteristics and Efficiencies Contract# W33-038 AC 21399 Piasecki
Aug 9 1949
67 System Concepts and Research Aircraft Bell Helicopter Sep 1972 68 AFFDL-TR-69-34 Three-Axis (Self-Organizing) VTOL
Flight Control System for Comparing Rate, Attitude and Velocity Commands
Jun 1969
69 Letter from Piasecki Aircraft to Mr. B. Lindenbaum concerning Aquagyro
Jul 6 1961
70 Miscellaneous Unidentified Helicopter Photos (4) undated 71 Lockheed Rigid Rotor Report Vol. II, No. 2 Dec 1966 72 AHS Newsletter Vol. 5, No. 12 Dec 1959 73 HC-1B Category I Performance, Stability and Control
Flight Test Plan Mar 1962
74 Report No. R-294 Summary Presentation – USAF SR-175 VTOL/STOL Logistics Aircraft Parameter Study 19651970 Time Period
Apr 8 1960
75 Lockheed Reports Volume XI, Number 2 Mar 1962 76 WADD TR 61-66 A Study to Correlate Flight Measured
Helicopter Vibrations Data and Pilot Comments Boeing/Vertol
Aug 1961
77 AFM 60-19 H-19 Aircrew Standardization/Evaluation Feb 20 1962
45
Manual 78 Report No. ER 10281 ROTOPROP Interim Progress
Report Martin Jul 1958
79 AFV/F380-002 Proposal for the Development of a Helicopter Rotor Martin
Apr 16 1958
80 Trip Report – Purpose of Obtaining Information on Helicopters and Thrust Information
Mar 6-10 1950
81 AHS Newsletter Vol. 8, No. 3 Mar 1962 82 Report No. 533.5 A Proposal for the Study and Test of a
Lightweight Rotor System Hiller Apr 1956
83 Report No. 30-929-109 Response of Helicopter Rotors to Periodic Forces Bell
Oct 12 1944
84 Report No. 02-943-063 Periodic Aerodynamic Forces on Rotors in Forward Flight Bell
Feb 30 1944
85 AIAA Paper No. 71-991 The Reduction of VTOL Operational Noise Through Flight Trajectory Management
Oct 25-28 1971
86 Journal of Aircraft Volume 1 Number 6 Nov-Dec 1964 87 Journal of the Aeronautical Sciences Volume 11, No. 3 Jul 1944 88 Journal of the Aeronautical Sciences Volume 12, No. 1 Jan 1945 89 Journal of the Aeronautical Sciences Volume 13, No. 12 Dec 1946 90 Journal of the AHS Volume 5, No. 1 Jan 1960 91 Journal of the AHS Vol. 10, No. 3 Jul 1965 92 NASA Report 72-04 An Investigation of the Mixing of
Linear and Swirling Flows Contract# N00014-71-C-0226 Feb 15 1971 – Feb 14 1972
93 Report No. MDC-J56/01 Wind Tunnel Tests of Two Airfoils Designed for High Lift Without Separation in Incompressible Flow McDonnell Douglas
Aug 1972
94 Helicopter and V/STOL Noise Generation and Suppression Nov 1968 95 Sikorsky S-64 (Skycrane) Photos and Pictures 6 items 1960 96 ADS TN 68-1 A Study of the Army Hot Day Design
Hover Criterion Aug 1970
97 Bell Flyers Model 214A/B and YAH 63 May 1975 98 Boeing-Vertol Presentation to ASC, WPAFB Jul 26 1968 99 Rotary Wing Aircraft in the 1970-1980 Period Apr 14 1961 100 Results of XR-8 Rigid Rotor Studies Sep 20 1945 101 Vertol Helicopter Pamphlet Model 107 Helicopter Aug 4 1958 102 Piasecki Blueprint Model PH-29 Undated
ROTOR BLADES 20 1 Bell Helicopter Telescoping Rotor Blades – Article and 3
Photos May 5 1947
2 Variable Diameter Rotor Bell Helicopter – Article, Photos (2) and Diagrams Total 9 Items
1964-1968
3-4 Variable Diameter Rotor Study Contract# F33615-71C1186
Est. 1970
5 Variable Diameter Rotor – Grumman, Sikorsky, Piasecki 1968
46
Miscellaneous Documents 6 SER-50709 Variable Diameter Rotor Study Interim TR
Contract# F33615-71-C-1186 Bell Mar 1971
7-8 USAAMRDL TR 73-32 Dymanic Model Wind Tunnel Tests of a Variable Diameter, Telescoping Blade Rotor System (Trac Rotor) Contract# DAAJ02-68-C-0074
Jul 1973
9 AFFDL-TR-70-70 Effect of Root Cutout on Hover Performance Sikorsky
Jun 1970
1011
Report 50718 Variable Diameter Rotor Study Draft Final Report Contract# F33615-71-C-1186
Jul 9 1971
12 AFFDL-TR-70-170 Variable Diameter Rotor Study Sikorsky
Jan 1972
13 Report 243-X-3 Cost Proposal for Investigation of the Techniques for and the Problems of Designing Variable Diameter Rotors Having Large Ratios of Extended to Retract Span Contract# F33615-71-R-1068 Piasecki
Aug 31 1970
14 Report 243-X-2 Proposal for Investigation of the Techniques for and the Problems of Designing Variable Diameter Rotors Having Large Ratios of Extended to Retract Span Contract# F33615-71-R-1068 Piasecki
Aug 31 1970
15 Report P-09-622A Variable Diameter Rotor Proposal Contract# F33615-71-R-1068 Parsons Includes Cover Letter, Proposal and 4 diagrams
Aug 28 1970
16 Development of the Trac Variable Diameter Rotor Concept by Richard M. Segel Sikorsky
Feb 17-19 1969
ROTORS/BLADES 21 1 VTOL – Miscellaneous Concept Photos and Charts 1968-1970
2 Report 12153-FR1(R) Helicopter Application Studies of the Variable Deflection Thruster Jet Flap Contract# N00014-69-C-0267 NR-212-195/1-2-69 (Code 461) Honeywell, Inc
Nov 1970
3 AHS 29th Annual National Forum – The Application of Circulation Control Aerodynamics to a Helicopter Rotor Model by Joseph B. Wilkerson, Kenneth R. Reader and Drew W. Linck
May 1973
4 AHS 30th Annual National Forum – Hingeless Circulation Control Rotor Blade Design by P.H. Kesling and Jaap Schmidt Lockheed
May 1974
5 AHS Midwest Regional Symposium on Rotor Technology – Circulation Control Rotor Flight Demonstrator by David R. Barnes and George A. McCoubrey KAMAM and Douglas G. Kirkpatrick Naval Ship R&D Center
Aug 1976
6 AHS 35th Annual National Forum – The Circulation Control Rotor Flight Demonstrator Test Program by
May 1979
47
Joseph B. Wilkerson, David R. Barnes and Frank A. Gill KAMAN / Naval Ship R&D Center
7 Report 77-0034 Hover Evaluation of the Circulation Control High Speed Rotor by Kenneth R. Reader Naval Ship R&D Center
Jun 1977
8 Report 77-0076 Circulation Control – An Updated Bibliography of DTNSRDC Research and Selected Outside References
Sep 1977
9 Report 77-0084 An Assessment of Circulation Control Airfoil Development Naval Ship R&D Center
Aug 1977
10 The Effects of Dual Controls on the Performance of an Elastically Twisting Rotor Blade Contract# DAAJ02-67-C0068
May 1970
11 SER-2600-24 Engineering Progress Report No. 24 Phase I of Development of Convertiplane (Model S-57) Contract# AF33(038)-28076
Jun 8 1953
12 Classification of Rotor Types (Stowed and Wing) Undated 13 SPB-AF9063-US Stowed Rotor V/STOL Program
Planning Proposal Sikorsky Mar 23 1964
14 LR-21283 A Summary of Stopped Rotor Research and Development at the Lockheed-California Co.
Jan 22 1968
15 Stowable Rotor System for Reusable Launch Vehicle Lockheed-California
Undated
16 Ryan Stoppable Rotor – Photos and Articles 1962-1964 17 Limit Cycle Torsional Motion of Helicopter Blades Due to
Stall by N.D. Ham MIT and M.I. Young Boeing-Vertol Aug 30 1965
18 Report 107-2 Theoretical Determination of Rotor Blade Harmonic Airloads by R.H. Miller MIT Contract# Now 62-0100-d
Aug 1964
19 Report 159A-90-1 TREC 60-43 Stability and Control Handbook for Helicopters Contract# DA 44-177-TC-599 Kellett
Aug 23 1961
20 Report R 242 Fundamentals of Helicopter Stability and Control Contract# Now60-0469-f Boeing-Vertol
Feb 1961
21 PB 121097 Rotary Wing Aircraft Handbook and History Volume 5 Weight and Balance Contract# W33-038 ac21804 (20695)
1954
22 Light Helicopter Drag Chart 1950-1980 Undated 23 NASA MEMO 1-7-53L A Wind-Tunnel Investigation of
Rotor Behavior Under Extreme Operating Conditions with a Description of Blade Oscillations Attributed to Pitch-Lag Coupling
Nov 14 1958
24 NASA MEMO 1-23-59L Maximum Mean Lift Coefficient Characteristics at Low Tip Mach Numbers for a Hovering
Feb 1959
48
Helicopter Rotor Having an NACA 641A012 Airfoil Section
25 NASA MEMO 2-28-59L Comparison of Measured Flapwise Structural Bending Moments on a Teetering Rotor Blade with Results Calculated from the Measured Pressure Distribution
Feb 6 1959
26 NASA MEMO 4-15-59L Charts of the Induced Velocities Near a Lifting Rotor
Mar 26 1959
27 NASA MEMO 5-7-59L Flight Investigation of Effects of Transition, Landing Approaches, Partial-Power Vertical Descents, and Droop-Stop Pounding on the Bending and Torsional Moments Encountered by a Helicopter Rotor Blade
Apr 6 1959
28 Report 347-V-1002 (HTC-AD-64-8) Effects of Blade Stall on Helicopter Rotor Blade Bending and Torsional Loads Final Report Contract# Now-0422-c
May 1 1965
29 Torsional Oscillation of Helicopter Blades Due to Stall by Norman D. Ham MIT and Maurice I. Young Boeing
Jan-Jun 1966
30 Short Takeoff and Landing for the High Speed Aircraft by John K. Wimpress Boeing
Feb 1966
31 An Engineering Approximation for the Aerodynamic Loading of Helicopter Rotor Blades by M. I. Young Boeing-Vertol
Aug 30-Sep 3 1965
32 D210-10379-1 Boeing Vertol Division 1972 Independent Research and Development Program Weight Estimation for Helicopter Design Analysis
May 19-22 1958
33 SER-1775 Tow Tests of H-5 (S-51) Helicopter Contract# AF 33(038)-7878 Sikorsky
Oct 19 1950
34 AHS 5th Annual Western Forum A Study of the Attainable Range of Helicopters by Abraham C. Adler and Helen S. Holm
Sep 25-26 1958
35 Report HTC-AD-65-15 Volume I Summary TR Rotor/Wing Concept Study Contract# Nonr-4588(00) Hughes Tool
Sep 1965
36 Report 7376 Substantiating Data on the Unloaded Rotor V/STOL Transport Aircraft McDonnell Aircraft
Feb 1 1960
37 NASA TN D-3028 Analytical Investigation of a Helicopter Rotor Driven and Controlled by a Jet Flap
Sep 1965
38 Technical Note AL-290 Design and Performance of a Prototype Circulation Control Helicopter Rotor
Mar 1973
39 High Advance Ratio Research and Development Lockheed-California
Feb 1970
40 Composite Aircraft with Rotary and Fixed Wing Components by Dr. J.A.J. Bennett Hiller
1952
41 Performance Characteristics of a Jet-Flap Rotor by John L. McCloud III, William T. Evans and James C. Biggers
Apr 4-5 1966
49
Ames Research Center 42 AHS 54th Annual Forum Compound Interest-A Dividend
for the Future, Revised by D.V. Humpherson Westland Helicopters
May 20-22 1998
43 AHS 54th Annual Forum A Perspective of Future Rotorcraft Technology by P.N. Goddard Westland helicopters
May 20-22 1998
44 Analytical Investigation of the Performance of a Controllable Twist Rotor Contract# DAAJ02-67-C-0068 KAMAN (3 copies)
Undated
45 Report 68-9 Reverse-Velocity Rotor Test Program Fairchild Hiller
May 29 1968
46 SPB 73-A6461-RD Full Scale Wind Tunnel Test of TRAC Sikorsky
Dec 17 1973
47 The Controllable Twist Rotor by Arthur F. Smith KAMAN
Jun 18-20, 1969
48 NASA TN D-2628 Wind Tunnel Investigation of a Lifting Rotor Operating at Tip-Speed Ratios from 0.65 to 1.45
Feb, 1965
49 Report 68-5 Reverse Velocity Rotor Model Wind Tunnel Test Program Results Fairchild Hiller
Jul 5 1968
50 Research and Development of Advanced Rotorcraft Concepts by Evan A. Fradenburgh Sikorsky
1968
51 DOD/NASA Aeronautical Research and Development Studt Rotorcraft Technology
Nov 1972
52 Development of the TRAC Variable Diameter Rotor Concept by Richard M. Segel and Evan A. Fradenburgh Sikorsky
Feb 17-19 1969
53 AHS 28th Annual National Forum The Controllable Twist Rotor, Performance and Blade Dynamics by A.Z. Lemnios and A.F.Smith KAMAN
May 1972
54 AHS 28th Annual National Forum Design Considerations of Circulation Control Rotors by Robert M. Williams and Ernest O. Rogers Naval Ship R&D Center
May 1972
55 Preliminary Investigation of the Karman-Yuan Helicopter Rotor System by S. W. Yuan Contract# AF 33(616)-2087
Undated
56 Technical Note AL-189 Theoretical Performance of a Pure Jet Flap Rotor at High Advance Ratios
Dec 1970
57 The Controllable Twist Rotor Pamphlet KAMAN Undated 58 Miscellaneous Photos (1) Fairey Rotodyne ; (2-3)
Advanced Blade Concept (ABC) Demonstrator Undated
1980 Propeller Propulsion Conference 22 1 Material -1)Cover Page; 2) Bookmark; 3) Sep 29 1982
Cover Letter Apr 22-24 1980
50
2 Lindenbaum Presentation Slides – Part 1 Apr 22-24 1980 3 Neitzel Presentation Slides Apr 22-24 1980 4 Foss Presentation Slides Apr 22-24 1980 5 Scherrer Presentation Slides Apr 22-24 1980 6 Pinson Presentation Slides Apr 22-24 1980 7 Redmond Presentation Slides Apr 22-24 1980 8 Scolatti Presentation Slides Apr 22-24 1980 9 Goldsmith Presentation Slides Apr 22-24 1980 10 Marks Presentation Slides Apr 22-24 1980 11 Slivinsky Presentation Slides Apr 22-24 1980 12 Nored Presentation Slides Apr 22-24 1980 13 Gatzer Presentation Slides Apr 22-24 1980 14 Lyon Presentation Slides Apr 22-24 1980 15 Correspondence Apr 22-24 1980 16 Miscellaneous Apr 22-24 1980 17 Planning Documents Apr 22-24 1980 18 Supporting Document – SAE 760535 Fuel Conservative
Propulsion Concepts for Future Air Transports by D.E. Gray & J.W. Witherspoon Pratt & Whitney
May 18-20 1976
19 Supporting Document- AIAA Paper No. 75-1208 – The Prop-Fan – A New Look in Propulsors by C. Rohrback & F.B. Metzger Hamilton-Standard
Sep 29-Oct 1 1975
20 Supporting Document- AIAA Paper No. 76-667 A Report on the Aerodynamic Design and Wind Tunnel Test of a Prop-Fan Model by Carl Rohrbach Hamilton-Standard
Jul 26-29 1976
21 Supporting Document- ASME 78-GT-201 Evolution of the Turboprop for High Speed Air Transport by G.E. Holbrook Detroit Deisel & G. Rosen Hamilton-Standard
Apr 9-13 1978
22 Supporting Document- SAE 751085 General Characteristics of Fuel Conservative Prop-Fan Propulsion System by B.S. Gatzen Hamilton-Standard & S.M. Hudson Detroit Diesel
Nov 17-20 1975
23 Supporting Document- AGARD Multi-Mission Uses for Prop-Fan Propulsion by A.H. Jackson, Jr. & B.S. Gatzen Hamilton-Standard
Sep 1976
24 Supporting Document- SAE 771009 Advanced Turboprop Propulsion Reliability and Maintenance Costs by Philip C. Stolp Detroit Diesel & James A. Baum Hamilton-Standard
Nov 14-17 1977
25 Supporting Document- AIAA Paper No. 79-1116 Structural Design and Analysis of Prop-Fan Blades by R.W. Cornell & E.A. Rothman Hamilton-Standard
Jun 18-20 1979
26 Supporting Document- SAE 780995 Prop-Fan Propulsion – Its Status and Potential by James F. Dugan, Jr. NASA & Bernard S. Gatzen and William M. Adamson United Technologies
Nov 27-30 1978
27 Supporting Document- AIAA Paper No. 79-0610 Mar 12-14 1979
51
Aeroacoustic Design of the Prop-Fan by F.B. Metzger & C. Rohrbach Hamilton-Standard
28 Supporting Document- B202 Rev A Propeller Progress Hamilton-Standard
Mar 1968
29 Supporting Document- AIAA Article – A Design Perspective on New Technologies for General Aviation by “JB” McCollough FAA
1979
30 Supporting Document- AWST Prop-Fan Powerplant Studies Evolve by Warren C. Wetmore
Jan 3 1977
31 Supporting Document- A fan for Tomorrow by Gene Costello Hamilton-Standard
1978
32 Proceedings of the 1980 Conference on Propeller Propulsion
Apr 22-24 1980
33 Supporting Document- Hamilton Standard Prop-Fan Data Packages
Feb 28 1978
34 Supporting Document- SP 11A77 Prop-Fan Fuel Conservative Propulsion for the 1980’s High Speed Air Transports Hamilton Standard
Oct 1977
35 Supporting Document- SP 07A77 Prop-Fan Technology Status Report
Undated
36 Supporting Document- SP 02A77 Prop-Fan Fuel Conservative Propulsion for the 1980’s High Speed Air Transports Hamilton Standard
Jan 1977
37 Report on Apr 22-24 1980 Propeller Propulsion Conference and Subsequent Activities
Undated
38 Supporting Document- Potential Propeller Technology and Static Thrust Augmentation by George Rosen Hamilton Standard
May 17 1966
39 Supporting Document- Glass Fiber Reinforced Plastic Blades for VTOL/VSTOL Aircraft Propellers Curtiss-Wright
1961
40 Supporting Document- All-Mechanical Propeller Curtiss-Wright
Dec 1958
41 Supporting Document- SP 06A77 Prop-Fan Acoustics – Status Hamilton Standard
Apr 1977
42 Supporting Document- Proposed Propeller Development for High Speed STOL and V/STOL Aircraft
Feb 14 1968
43 Miscellaneous AWST Articles and Advertisements Various 44 Attendees Names and Addresses 45 Support Letters from Industry Various 46 Correspondence Various 47 Technical Correspondence Various 48 Miscellaneous Presentation Pages Undated 49 Supporting Document- EDR10280 A Presentation on
Reduction Gearing by Terry Lyon Detroit Diesel Apr 21 1980
50 Presentation- Review of Propeller Propulsion Progress Up Undated
52
to the 1970s by Charles Scolatti 51 Supporting Document- Review of Propeller Propulsion
Progress Up to the 1970s A Success Story by Charles Scolatti
Undated
52 Marks Presentation Undated 53 Goldsmith Presentation Undated 54 Supporting Document- Soviet TU-95, TU-114 and AN-32
Aircraft Undated
55 Supporting Document- Blueprint of Prop-Fan on C-141A Mar 18 1980 56 Advanced Prop-Fan Engine Technology (APET)
Definition Study – Task II Review Contract# NAS3-23044 GE
Aug 5 1982
57 NASA CR159355 Turboprop Cargo Aircraft Systems Study Phase I Contract#NAS1-15708
Nov 1980
58 Miscellaneous Notes and Contact Lists Undated 59 Prop-Fan Propulsion Briefing Charts Undated 60 Scherrer Presentation Undated 61 Supporting Document- Commuter Traffic Statistics – New
Horizons 1978
62 Miscellaneous Photos Undated
ROTOR/BLADE TESTS & HELO CONTROL 23 1 NACA TN 1245 Summary of Lateral-Control Research Mar 1947
2 NACA TN 2474 Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors
Oct 1951
3 UH2C Pamphlet KAMAN Undated 4 Flight Test of the FRG 32-301 Hover/Transition and
Aerodynamic Damper/EFS – Integrated Fly by Wire SAS 1969
5 Report FT23-4R-64 Final Report Military Research Evaluation of the Lockheed XH-51A Rigid Rotor Helicopter
Jan 7 1964
6 AHS 27th Annual National V/STOL Forum – Forward Flight Performance of a Coaxial Rigid Rotor by Vincent M. Paglino Sikorsky
May 1971
7 ONR Conference VTO-Cargo Aircraft – Letters and Notes Oct 24-25 1955 8 The Driven Rotor Model Design – Sketches Jul 12 1982 9 WADC TR 57-583 – Part I – Helicopter Configuration and
Propulsion Systems Study Part I Statistical Weight Analysis Contract# AF33(616)-3149
Nov 1957
10 WADC TR 57-583 – Part III – Helicopter Configuration and Propulsion Systems Study Part III Aerodynamic Analysis Contract# AF33(616)-3149
Nov 1957
11 WADC TR 57-583 – Part IV – Helicopter Configuration and Propulsion Systems Study Part IV Analytical
Nov 1957
53
Procedure for Predicting Rotor Weight Contract# AF33(616)-3149
12 NASA TN D-809 Tables and Charts of the Normal Component of Induced Velocity in the Lateral Plane of a Rotor with Harmonic Azimuthwise Vorticity Distribution
Apr 1961
13 NASA Memo 3-3-59L Wind-Tunnel Investigation of the Effect of Angle of Attack and Flapping –Hinge Offset on Periodic Bending Moments and Flapping of a Small Rotor
Mar 1959
14 Report F-TS-1045-RE The Power Required of the Ideal Helicopter (from German)
Jan 1947
15 Report F-TS-510-RE Air and Mass Forces on Helicopter Propellers with Inclined Hinge (from German)
Mar 30 1946
16 Report F-TS-616-RE The Sensitiveness of the Human Body to Vibrations (from German)
Sep 1946
17 Report F-TS-692-RE The Pull-Up of the Helicopter (from German)
Aug 1946
18 Report F-TS-1001-RE The Performance Characteristics of the Helicopter (from German)
Sep 1946
19 Report F-TS-1002-RE The Dynamic Stability of Helicopters with Articulated Rotors(from German)
Sep 1946
20 Report F-TS-1003-RE Static Thrust Tests of the Model Helicopter Rotor and Preliminary Research of the Model Helicopter Rotor (from German)
Sep 1946
21 Report F-TS-1004-RE The Theory of the Control of the Blade Angle of the Helicopter (from German)
Sep 1946
22 Report F-TS-1006-RE Theory of Helicopter Control in Hovering Flight (from German)
Sep 1946
23 Report F-TS-1007-RE Investigation of the Influence of High Subsonic Velocities on the L/D of Rotary Wing Aircraft (from German)
Sep 1946
24 Report F-IR-133-RE Helicopter Theory Interview with Dr. Kurt Hohenemser Concerning His Recent Contributions
Sep 1946
25 NACA TM 907 Dynamic Stability of a Helicopter with Hinged Rotor Blades
Sep 1939
26 AF TR No. 6352 Longitudinal Stability Characteristics of a Gyroscopically Stabilized Helicopter in Forward Flight
Mar 1951
27 NACA TN 2721 Initial Results of Instrument- Flying Trials Conducted in a Single-Rotor Helicopter
Jun 1952
28 NACA TN 1430 A Theoretical Study of the Dynamic Properties of Helicopter-Blade Systems
Nov 1948
29 NACA TN 1999 A Theoretical Analysis of Elastic Vibrations of Fixed-Ended and Hinged Helicopter Blades in Hovering and Vertical Flight
Jan 1950
30 NACA TN 2984 Studies of the Lateral-Directional Flying Qualities of a Tandem Helicopter in Forward Flight
Aug 1953
31 NACA TN 3089 One-Dimensional, Compressible, Viscous Dec 1953
54
Flow Relations Applicable to Flow in a Ducted Helicopter Blade
32 NACA TN 3201 Directional Stability Characteristics of Two Types of Tandem Helicopter Fuselage Models
May 1954
33 USAAVLABS TR 68-22B In-Flight Measurement and Correlation with Theory of Blade Airloads and Responses on the XH-51A Compound Helicopter Rotor Volume II Measurement and Data Reduction of Airloads and Structural Loads Appendixes V through IX Contract# DA 44-177-AMC-357(T)
May 1968
34 ER Number 63-26 Preliminary Design Study Notes – Proposal for a Ground Test Research Program –Tip Turbojet Powered Heavy-Lift Rotor System Hiller
1962-1963
35 Project Forecast – High Speed Flexure Hub Rigid Rotor System for Helicopters Lockheed-California
Undated
36 AHS West Coast Forum Application of System Analysis Methods to Helicopter Preliminary Design by John A. DeTore & Eugene L. Brown
Nov 4-6 1954
37 Progress Report for NACA Helicopter Subcommittee Meeting
Apr 16 1958
38 AFFTC-TR-60-2 Air Force Flight Evaluation YHO-2HU Feb 1960 39 NACA TN 2912 The Normal Component of the Induced
Velocity in the Vicinity of a Lifting Rotor and Some Examples of its Application
Mar 1953
40 The Djinn Helicopter Cold Cycle Tip Jet YHO-1DJ Pamphlet Republic
Undated
41 Report No. 362 Stability ond Control of Tandem Helicopters Phase I and II – Static and Dynamic Longitudinal Stability and Control Princeton University
Sep 1956
42 Report XX90-4 Proposal for a Theoretical and Experimental Study of a Helicopter Employing Fixed Wings and Cocked Flapping and Lag Blade Hinges Kellett
Mar 1954
43 NACA TN 2086 Hovering and Low-Speed Performance and Control Characteristics of an Aerodynamic-Servocontrolled Helicopter Rotor System as Determined on the Langley Helicopter Tower
May 1950
44 NACA TN 2154 An Analysis of the Autorotative Performance of a Helicopter Powered by Rotor-Tip Jet Units
Jul 1950
45 NACA TN 3900 Investigation of Vertical Drag and Periodic Airloads Acting on Flat Panels in a Rotor Slipstream
Dec 1956
46 NACA TN 1595 Analysis of Flight-Performance Measurements on a Twisted, Plywood-Covered Helicopter Rotor in Various Flight Conditions
Jun 1948
55
47 NACA TN 3234 Reduction of Helicopter Parasite Drag Jun 1954 48 NACA Helicopter Subcommittee Meeting – Helicopter
Stabilizer with Photo Oct 22 1948
49 Prediction of Helicopter Longitudinal Stability and Control Characteristics – A Comparison Between Flight Test and Theory by Edwin R. Schultz (Master’s Thesis)
May 1958
50 WADC TR 55-437 Part I An Investigation of the Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Part I-Analytical Evaluation of Stabilizers Contract# AF33(616)-2780
May 1957
51 Bell Model 47-J Four Place Multi-Purpose Helicopter Pamphlet
Undated
52 Report FTR 47-2 Skid Landing Gear – Effect on Model 47 Bell
Sep 9 1952
53 Report X-417-11A XR-8 Model Specification Kellett May 3 1945 54 Report FTM 47-6 Drag Analysis of H-13E and Proposed
Configurations Bell Feb 4 1953
55 Report No. 120.30 Specification for Model XR-10 Helicopter Kellett
Mar 21 1944
56 Notes on Visits in Europe by Grover Loening with Photos Ovt 1952 57 NASA TN D-73 Comparison of Calculated and Measured
Stall Boundaries of a Helicopter Rotor at Advance Ratios from 0.3 to 0.4
Sep 1959
58 NASA TN D-393 Measurements of the Time-Averaged and Instantaneous Induced Velocities in the Wake of a Helicopter Rotor Hovering at High Tip Speeds
Jul 1960
59 NASA TN D-112 Experimental Investigation of the Pressure Fluctuations on a Flat Plate and a Cylinder in the Slipstream of a Hovering Rotor
Sep 1959
60 NASA TN D-737 Some Recent Studies in Structural Dynamics of Rotor Aircraft
Mar 1961
61 NASA TN D-742 Hovering Characteristics of a Rotor having an Airfoil Section Designed for Flying-Crane Type of Helicopter
Apr 1961
62 NASA TN D-774 Operational Technique for Transition of Several Types of V/STOL Aircraft
Mar 1961
63 NASA TT F-43 A Vibration Absorber for Two-Bladed Helicopters (from French)
Nov 1960
64 NASA TT F-55 Response of a Helicopter Rotor to an Increase in Collective Pitch for the Case of Vertical Flight (from French)
Jan 1961
65 NASA CR-2009 A Method for Analyzing Dynamic Stall of Helicopter Rotor Blades
May 1972
66 US Army TRC Preliminary Flight Test Data – Xh-51A Nov 1964
56
Rigid Rotor High Speed Flight Program 67 Performance Substantiation for Kinedyne Proposal Cessna Feb 5 1958 68 WADC TR 55-437 Part II An Investigation of the
Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Part II-Flight Test Evaluation of the Optimum Stabilization System Contract# AF33(616)-2780
Jan 1958
69 R. & M. No. 1730 The Flight of a Helicopter by H.B. Squire, M.A. (British Air Ministry)
Nov 28 1935
70 NASA TN D-335 Full-Scale Wind-Tunnel Tests of Blowing Boundary-Layer Control Applied to a Helicopter Rotor
Sep 1960
71 NASA TN D-432 A Summary of Operating Conditions Experienced by Three Military Helicopters and a Mountain-Based Commercial Helicopter
Oct 1960
72 NASA TN D-464 Effects of Control-Response Characteristics on the Capability of a Helicopter for use as a Gun Platform
Sep 1960
73 NASA TN D-534 Hovering Measurements for Twin-Rotor Configurations with and without Overlap
Nov 1960
74 NASA TN D-537 Flight Evaluation of Several Spring Force Gradients and a Bobweight in the Cyclic-Power-Control System of a Light Helicopter
Oct 1960
75 R. & M. No. 885 Some Experiments on Airscrews at Zero Torque, with Applications to a Helicopter Decending with the Engine “Off”, and to the Design of Windmills by C.N.H. Lock, M.A. & H. Bateman, B.Sc. (British Air Ministry)
Sep 1923
76 Technical Note WCT-52-47 Functional Development Test of the YH-24SE Helicopter
Dec 1952
77 WADC TR 55-438 Part I The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part I. Development of Flight Test Instrumentation, Techniques and Analysis Methods Contract# AF33(616)2773
Feb 1958
HELICOPTER AND BLADE AERODYNAMICS 24 1 Report SB-862-S-4 Investigation of Helicopter Rotor
Flutter and Load Amplification Problems Contract# AF 33(616)-440 Cornell
Aug 1956
2 Report No. 299-099-072 Proposal for the Construction and test of an Experimental Rotor Blade Suitable for Operation at High Tip Mach Number Bell
Nov 6 1957
3 NACA TN 3323 Charts for Estimating Performance of High-Performance Helicopters
Oct 1954
4 US Naval Air Test Center Model HRS-1, BuNo 127824 Mar 24 1954
57
Flight Test and Evaluation of JATO Installation Final Report
5 DADC Helicopter Rotor Testing Facilities Propeller Laboratory Design Features
Jun 24 1955
6 Report AVN 1556 Service Test of the HOK-1 Helicopter Mar 1957 7 Report UTR No. 150.1 The Helicopter Control Rotor
United Helicopters, Inc. Mar 19 1947
8 The “SKEETER” Mark 6 Helicopter Sanders-Roe Limited C.A. 1949 9 Report No. G-113-6 Flutter Analysis of the KAMAN K
16B VTOL/STOL Research Aircraft Contract# NOa(s) 56549c
Oct 15 1959
10 Report No. 269-S-1 Final Design Specification for Hughes Tool Company – Aircraft Division Two-Place, Single Engine, Three Bladed Helicopter Model 269A
Jun 5 1957 Rev1 Jul 1 1957
11 US Naval Air Test Center Evaluation of Stability and Control Characteristics of Model HRP-1 Helicopter BuNo 111809 with Stabilizer Device
Dec 26 1950
12 Report No. 230 Model Study of Helicopter Dynamic Stability and Control Phase II Comparison of Theoretical and Experimental Results Near Hovering Flight Princeton University
May 1953
13 Report 204-099-903 Structural Comparison of Six Multi-Bladed Rotor Designs Contract# AF 33(600)30229 Bell
Apr 12 1957
14 Report 204-099-907 Evaluation of Five Semi-Rigid Multi-Blades Rotor Designs Contract# AF33(600)30229 Bell
Jul 25 1957
15 Report 204-099-701 The Dynamics of Semi-Rigid Multi-Blade Rotors Contract # 33(600)30229 Bell
Sep 3 1957
16 Report 204-099-706 Preliminary Studies on the Design of Blades for Semi-Rigid Rotors to Minimize Vertical Vibration Contract# 33(600)30229 Bell
Sep 3 1957
17 Report SER-383 Mechanical Instability Characteristics of the H-5G Helicopter Contract# AF 33(038)-2662
Apr 15 1949
18 American Helicopter Co. XA-6 and H26 Helicopter Brochures
Undated
19 Report No. 123-G1 Performance Analysis XA-5 Pulse Jet Powered helicopter Contract# AF 33(038)-6099 AHC.
May 1 1950 Rev May 26 1950
20 Summary Report 123-O-1 Pulse-Jet Engine Development Contract# AF 33(038)-6099 AHC
Sep 14 1950
21 Summary Report 123-O-2 Development of Pulse-Jet Helicopter Rotor Contract# AF 33(038)-6099 AHC
Sep 14 1950
22 Report 123-B1 Pulse Jet Rotor design Analysis Contract# AF 33(038)-6099 AHC
Oct 5 1949
23 Report 163-B-2 Altitude Performance and Operational Tests of Pulse-Jet Engines AHC
Dec 20 1950
58
24 Report 157-1 Model 157 Single-Place Pulse-Jet Propelled helicopter (Collapsible) AHC
Feb 22 1951
25 Report 157-3 Aerodynamics Analysis of a Single-Place, Jet-Propelled Helicopter Model 157 AHC
Feb 22 1951
26 Report 163-F-1 Analysis of the Dynamic Forces in the Control System of the XA-5 Pulse-Jet-Powered Helicopter 25 Report 157-3 Contract# AF 033(038)-6099 AHC
Apr 6 1951
27 Report 157-b Model Specification Model 157, Single Place Helicopter AHC
Jun 8 1951
28 Report 163-H-1 A Mathematical Analysis of the Response Characteristics of a Two-Bladed, Jet-Driven Rotor to Vertical Excitation Helicopter Contract# AF 033(038)6099 AHC
Jun 21 1951
29 Report 163-L Progress Report for Sep 1951 – Development of a Pulse-Jet-Powered Helicopter Rotor Contract# AF 33(038)-6099 AHC
Oct 20 1951
30 Report 163-I Progress Report for Jun 1951 – Development of a Pulse-Jet-Powered Helicopter Rotor Contract# AF 33(038)-6099 AHC
Jul 14 1951
31 XH-26 Single Place Helicopter (Collapsible) Mock Up Board Information AHC
1951
32 Report S-157-k Proposed Model Specification, Model XH26A Two-Place, Observation-Reconnaissance-Utility Helicopter Contract AF 33(038)-27961 AHC
Oct 31 1952
33 American Helicopter Co. Progress Notes Feb 8 1954 34 Report No. TCAR001 Model Specifications Model TCAH
1 Twin Coach Jun 9 1953
35 Report No. TCAR002 Preliminary Performance of the Twin Coach Model No. TCAH-1 Helicopter Twin Coach
Aug 19 1953
36 Report No. S-157-Q ERs Model XH-26 Contract# AF 33(038)-27961 ( 13 separate reports)
1953
37 Report No. S-157-C ERs Model XH-26 Contract# AF 33(600)-5860 ( 10 separate reports)
1953
38 Report No. S-157-EE ERs Model XH-26 Pulse-Jet Helicopter Contract# AF 33(038)-27961 ( 6 separate reports)
1953
HELICOPTER PERFORMANCE & THEORY 25 1 Report No. 48-923-001 Preliminary Flight Test of XR-12
Helicopter Bell Apr 28 1948
2 NASA TN D-1364 A Wind Tunnel Investigation of the Longitudinal Aerodynamic Characteristics of Two Full-Scale Helicopter Fuselage Models with Appendages
Jul 1962
3 Technical Note WCT-53-16 Cornell Rotor Stabilizer Mar 1953 4 Experimental Study of a Tandem Helicopter Employing
Cocked Vertical Blade Hinges Kellett Jan 25 1956
59
5 NASA TN D-1363 A Wind Tunnel Investigation of the Drag and Static Stability Characteristics of Four Helicopter Fuselage Models
Jul 1962
6 Report Number 62-73 Proposal to USAF for use of Model Ten99A as a Missile Site Support Helicopter Hiller
Aug 1962
7 FTC-TDR-62-15 Performance Evaluation of the H-13K Aug 1962 8 Report No. 373 An Economical Technique for the
Construction and Hovering Flight Evaluation of Dynamically Similar Helicopter Models Princeton
Nov 1956
9 Report No. F-IR-133-RE Helicopter Theory Interview with Dr. Kurt Hohenemser
Sep 1946
10 Report No. F-IR-1001-RE The Performance Characteristics of the Helicopter by Dr. Kurt Hohenemser
Sep 1946
11 Report No. 30-929-113 Stability of Helicopter Having Universal Joint Two Blade Rotor Bell
Nov 26 1942
12 SER-442 The Effect of Platform on Static Thrust Performance Sikorsky
Nov 7 1944
13 SER-459 Tilted Tail Rotor Aerodynamic Study of New tail Arrangement Sikorsky
Feb 7 1945
14 SER-3104 Substantiating Data for Standard Aircraft Characteristics and Performance Charts for H-34A Helicopter Sikorsky
Aug 16 1954 RevA Mar 15 1955
15 Report F-TS-5406-RE The Danger of the Side Drift Landing in the Operation of Rotary Wing Aircraft by S. Hoerner (Germany)
Apr 1948
16 Report F-TS-1045-RE The Power Required for the Ideal Helicopter by K. Hohenemser (Germany)
Jan 1947
17 Report No. 156 An Experimental Investigation of the Transition of a Helicopter from Hovering to Vertical Flight Contract# NAw-5619 Princeton University
Dec 1 1949
18 AHS Design Considerations in the Kaman Servo-Controlled Intermeshing-Rotor Helicopter by Charles H. Kaman
Feb 9 1953
19 Progress Report – Unsteady Induced Flow on Helicopter Rotors Contract# NAw-5619 Princeton
Jun 1 1949
20 Report No. AA-1-6 Loading Analysis Theory for a Four-Bladed Universally Mounted Rotor System Contract# AF33(600)-9053
Sep 30 1953
21 Proposed Rotorcraft Design, Inherently Stable in Pitch and Roll, with a Simplified Control System by J.C.Vogtle & H. E. Stewart
Nov 28 1953
22 Flight Testing Helicopters for Dynamic Stability (Cornell Aero Lab Utilizing YH-13 Helicopter) by John O’Dea
Undated
23 Report AD No. 16-727 Design and Development of an Automatic Hovering Control for Rotary Wing Aircraft
May 15 1953
60
Final Report Number 111 – Phase I Contract# AF 33(616)227
24 Report No. R50GL174 Biased Cyclic Control for H-5 Helicopter Contract# AF33(083)6146
Jun 1 1950
25 Report No. 58-19 Damped Bar Stabilized Control Rotor System Hiller Helicopters
Jan 6 1958
26 Report GER-3005 (Photocopy) Theoretical Stability and Control Study for H-5 Helicopter Goodyear
Feb 1949
27 Report EP-247-0958-12 Proposal for Flight Test and Evaluation of Hydromechanical Stability Augmentation System Vertol t
Sep 22 1958
28 Report 1430.17 An Approximate Analysis of the Static Longitudinal Stability of a Tandem-Type Helicopter, with Applications to Kellett Model KH-3 Skycrane Kellett
Jan 1946
29 Report PTR AD-3096 Navy Evaluation of the Modified Model HSL-1 Helicopter, Report No. 1, Final Report
Jan 15 1960
30 Report YA-1533 Stability and Control Analysis of the M30 Quadrotor Transport Helicopter Convertawings
Jul 9 1958
31 File No. 565-PH-56-91(5004) Final Report on Study of Helicopter Stabilization Systems Contract# DA-36-039 SC-72412
Jun 1 1956 to 31 Jul 1957
32 AFFTC-TR-58-4 ARDC H-19 Stability with a Stabilizing Bar
Mar 1958
33 AHS 30th Annual National Forum – Doc# 800 – Laser Velocimeter measurements of the Helicopter Rotor-Induced Flow Field by James C. Biggers & Kenneth L. Orloff Ames research
May 1974
34 AHS 30th Annual National Forum – Doc# 801- The Prediction of Rotor Rotational Noise Using Measured Fluctuating Blade Loads by R.N. Hosier, R. Ramakrishnan & R.J. Pegg NASA Langley
May 1974
35 AHS 30th Annual National Forum – Doc# 802- Tail-Rotor Thrust on a 5.5-Foot Helicopter Model in Ground Effect by R. Wayne Empey & Robert A. Ormison Ames Directorate, Moffitt Field
May 1974
36 AHS 30th Annual National Forum – Doc# 803- Can Helicopter Rotors be Designed for Low Noise and High Performance? By David R. Clark Sikorsky
May 1974
37 AHS 30th Annual National Forum – Doc# 804- A Systematic Study of Helicopter Rotor Stall Using Model Rotors by Anton J. Landgrebe & E. Dean Bellinger United Aircraft
May 1974
38 AHS 30th Annual National Forum – Doc# 810- Design to Cost at Work for Helicopter Systems by Leonard J. Marchinski Boeing Vertol
May 1974
61
39 AHS 30th Annual National Forum – Doc# 811- Improved Cost Effectiveness of Helicopters Through a Two-Point Design Criterion by Arved Plaks & Richard C. Meier Kaman and Herman I. MacDonald USAAMRDL
May 1974
40 AHS 30th Annual National Forum – Doc# 812- The Scissors Rotor by Walter G.O. Sonneborn & Jan M. Drees Bell Helicopter
May 1974
41 AHS 30th Annual National Forum – Doc# 821- Visual and Manual Workload of the Helicopter Pilot by Dr. Dora Dougherty Strother Bell Helicopter
May 1974
42 AHS 30th Annual National Forum – Doc# 822- Helicopter Command Instrument Systems by James F. Hatcher US Army ASC
May 1974
43 AHS 30th Annual National Forum – Doc# 824- Avionic and Fire Control Equipment Complement to Enhance Attack Helicopter Survivability by Edward Stepans Lockheed-California
May 1974
44 AHS 30th Annual National Forum – Doc# 825- Controls and Displays for Helicopter IFR Operation – Pilot Factor Considerations by F.J. Winter, Jr. WPAFB Flight Dynamics Lab
May 1974
45 AHS 30th Annual National Forum – Doc# 831- On the Use of First Order Rotor Dynamics in Multiblade Coordinates by K.H. Hohenemser & S.K. Yin Washington Univ (St.Louis)
May 1974
46 AHS 30th Annual National Forum – Doc# 832- Effect of Hub Impedence on the Inplane Oscillatory Blade Loads of a Two-Bladed Rotor System by J.A. White & C.D. Lee Bell
May 1974
47 AHS 30th Annual National Forum – Doc# 833- Effect of Blade Design Parameters on Helicopter Stall by R.H. Blackwell Sikorsky & P.H. Mirick USAAMRDL
May 1974
48 AHS 30th Annual National Forum – Doc# 834- AH-56A (AMCS) Compound Helicopter Vibration Reduction by W.D. Anderson & E.R. Wood Lockheed-California
May 1974
49 AHS 30th Annual National Forum – Doc# 842- Rotor Moment Control with Flap-Moment Feedback by A.J. Potthast & A.W. Kerr Lockheed-California
May 1974
50 AHS 30th Annual National Forum – Doc# 843- Analysis, Simulation, and Piloted Performance of Advanced Tandem-Rotor Helicopters in Hover by Robert P. Smith USAAMRDL & Roman T. Lytwyn & F. White Boeing Vertol
May 1974
51 AHS 30th Annual National Forum – Doc# 844- Helicopter Icing Handling Qualities by LTC Warren E. Griffith II &
May 1974
62
CPT Larry K. Brewer US Army Avn Systems Test Activity (Edwards AFB)
52 AHS 30th Annual National Forum – Doc# 850- Fabrication of Boron-Hybrid Swashplates by Joseph Jakubowski & Alexander Yankovoy Boeing Vertol
May 1974
53 AHS 30th Annual National Forum – Doc# 852- Heat Transfer Modeling for Curing Process of Composite Rotor Blades by Tai Lang Huang & Andrew A. Peterson Boeing Vertol
May 1974
54 AHS 30th Annual National Forum – Doc# 853- Processing of Titanium Tubes – An Approach to Helicopter Blade Spar Manufacturing by Stanley M. Silverstein Sikorsky
May 1974
55 AHS 30th Annual National Forum – Doc# 860- Helicopter Reliability Testing by Thomas L. House USAAMRDL
May 1974
56 AHS 30th Annual National Forum – Doc# 861- RAPID – A Data Acquisition and Processing System for Flight Test Cost and Schedule Improvement by Victor G. Berecz Sikorsky
May 1974
57 AHS 30th Annual National Forum – Doc# 862- Helicopter Flight Investigation to Determine the Effects of a Closed-Circuit TV on Performance of a Precision Sling-Load Handling Task by Danial J. DiCarlo NASA Langley, Henry L. Kelley USAAMRDL & David L. Spivey CWO, US Army
May 1974
58 AHS 30th Annual National Forum – Doc# 863- Effect of Nap-Of-The-Earth Requirements on Aircrew Performance During Night Attack Helicopter Operations by COL Billy L. Odneal US Army Comcat Developments Experimentation Cmd.
May 1974
59 AHS 30th Annual National Forum – Doc# 864- UTTAS Flight Test: Real-Time Data Analysis by Donald L. Marshall & Herbert H. Steinmann Boeing Vertol
May 1974
60 AHS 30th Annual National Forum – Doc# 870- Heavy-Lift Helicopter Engine Control System by J. Roger Alwang Boeing Vertol & Richard D. McLain Detroit Deisel Allison
May 1974
61 AHS 30th Annual National Forum – Doc# 871- The Impact of Advanced Turboshaft Technology on T700-Powered Helicopter Systems by L.B. Veno GE
May 1974
62 AHS 30th Annual National Forum – Doc# 872- Small Turbine Advanced Gas Generators for Future Engine Requirements by Edwaed T. Johnson & Graydon A. Elloitt USAAMRDL
May 1974
63 AHS 30th Annual National Forum – Doc# 873- Balancing of High Speed Interconnect Shafting for operation Above Multiple Bending Critical Speeds by Robert H. Badgley &
May 1974
63
Jeurgen M. Tessarzik Mechanical Technology Inc. 64 AHS 30th Annual National Forum – Doc# 874- Digital
Computer Techniques for Engine/Airframe Simulation by David V. Lewis Boeing Vertol
May 1974
65 AHS 30th Annual National Forum – Doc# 883- Design, Testing and Performance of Elastometric Bearings by Warren E. Schmidt Lord Kinematics
May 1974
66 AHS 30th Annual National Forum – Doc# 884- Composite Material Geodesic Structures – A Structural-Concept for Increased Helicopter Rotor Blade Survivability by S. Pociluyko & I.E. Figge USAAMRDL and C.F. Griffin & L. Blad Lockheed-California
May 1974
67 Verti-Flite Volume 10, No. 8 August 1964 68 Aerodynamic Considerations of Rotors in Hovering and
Vertical Climb Conditions by Charles H. Kaman United Aircraft from Journal of the Aeronautical Sciences Vol 10 No 7
Jul 1943
69 AHS Meeting – A Note on the Short-Haul Commercial Transport Helicopter by Edward F. Katzenberger
Dec 21 1953
70 State of the Art Advancement in Helicopter Design Lockheed Aerogyro
Oct 1963
71 Aeroproducts Division, GM, Dayton ERs 162, 312, 315, 322, 323, 324, 327, 338, 356, 362, 370
1943
72 SBD Report No. TR 59-41 Aerial Utility Vehicle, Monthly Progress Report for May 1959 Contract# DA-44-177-TC397
Jun 5 1959
73 AHS 28th Annual Meeting Subcommittee Chairman’s Report to Membership on Aerodynamic Sources of Rotor Noise by C.R. Cox Bell
May 1972
74 AIAA Paper No. 71-580 Hingeless Rotor characteristic at High Advance Ratios by W.A. Kuczynski Lockheed-California & D.L. Sharpe US Army Aero Research Lab (Moffitt Field)
Jun 21-23 1971
75 Lockheed 1026 Turbo-Compound Interurban Transport Undated 76 TRECOM TR 63-42 Summary Report High-Performance-
Helicopter Program Contract# DA44-177-TC-711 Sep 1963
77 TRECOM TR 64-61 High-Performance-Helicopter Program Summary Report, Phase II Contract# DA44-177TC-711
Oct 1964
78 USAAVLABS TR 66-17 High-Performance UH-1 Compound Helicopter Maneuver Flight Test Program
Feb 1966
79 Items of Interest and Suggestions for Research by Robert R. Lynn Bell Helicopter
May 15 1968
80 AHS 30th Annual National Forum – Doc# 830- Helicopter Vibration Reduction with Pendulum Absorbers by Robert B. Taylor & Paul A. Teare Boeing Vertol
May 1974
64
81 Honeywell Document 8D-F-6 R&D Program for Fluidic Control of the Variable Deflection Thruster for Helicopter Applications
May 24 1967
82 AHS Advanced Paper Second Annual Technical Symposium – Tactical Uses of Vertical Lift Aircraft
Nov 14-16 1967
83 The Helicopter Comes of Age Boeing Helicopters Apr 3 1967 84 Utility Tactical Transport Aircraft System (UTTAS)
Boeing Mar 31 1972
85 Identification of Structural Parameters for Helicopter Dynamic Test Data Kaman
Feb 13-15 1974
86 Rotary Wing Design Methodology Kamam Mar 30-Apr6 1973
87 Test and Evaluation of a Quiet Helicopter Configuration HH-43B from Journal of the Acoustic Society of America Vol. 54, No. 5
Nov 1973
88 Report No. 24 Helicopter Stability Tests Model H-2A Landgraf Helicopter Co.
Jun 1948
89 TR ATI No. 20283 Evaluation and Tests of the Flettner282 German Helicopter
Sep 1948
90 NASA TN D-633 An Analysis of the Flapwise Frequencies and Mode Shaped of Rotor B;\lades Having Two Flapping Hinges to Reduce Vibration Levels
Dec 1960
91 NACA TN 2309 Charts for Estimation of Longitudinal Stability Derivatives for a Helicopter Rotor In Forward Flight
Jan 22 1951
92 NACA TN 3156 Charts for Estimating Tail-Rotor Contribution to Helicopter Directional Stability and Control in Low-Speed Flight
May 1954
93 NACA TN 3236 Wind-Tunnel Studies of the Performance of Multirotor Configurations
Aug 1954
94 MIT TR 123-3 An Extended Lift Line theory for the Loads on a Rotor Blade in the Vicinity of a Vortex Contract# Now 64-0188-d
Dec 1965
95 MIT TR 133-1 An Actuator Disc theory for the Shed Wake at Low Tip Speed Ratois Contract# Now 65-139-d
Undated
96 Report No. R-585-2 The Aeroelastic Behavior of Rotary Wings in Forward Flight Contract# Now 66-0629f Kaman
Jul 1968
97 MIT TR 123-2 Approximate Solutions for Computing Helicopter Harmonic Airloads Contract# Now 64-0188-d
Dec 1965
98 USAAVLABS TR 68-22A In Flight Measurement and Correlation with Theory of Blade Airloads and Responses on the XH-51A Compound Helicopter Rotor Volume I – Measurement and Data reduction of Airloads and Structural Loads Contract# DA 44-177-AMC-357(T)
May 1968
99 USAAVLABS TR 68-22C In Flight Measurement and Correlation with Theory of Blade Airloads and Responses
May 1968
65
on the XH-51A Compound Helicopter Rotor Volume III Theoretical Prediction of Airloads and Structural Loads and Correlation with Flight test Measurements Contract# DA 44-177-AMC-357(T)
100 The TRW Approach to Complete Assessment of the Cheyenne by John F. Mosher TRW
C.A. 1967
101 Operating Problems and Experience with the Sikorsky Skycrane by Miller A. Wachs Sikorsky
1967
102 Operational Problems and Experience with Vertical-Lift Aircraft Light and Utility Helicopters by John W. Oswalt Bell
Nov 15 1967
103 Operational History and Experience with Boeing Helicopters by Howard N. Stuverude Boeing-Vertol
Nov 14-16 1967
104 AHS 27th Annual National V/STOL Forum Number 573 Army/Navy Operational Evaluation of Offshore Discharge of Containerships by LTC L. J. McConnell USArmy
May 1971
105 Technical Data Digest – Helicopter Development 14731943 by Thomas M. Wood
C.A. 1943
106 Institute of Aeronautical Sciences Number 109 Chordwise and Beamwise Bending Frequencies of Rotor Blades by Gabriel Horvay
Undated
107 New Markets for the S-64 Skycrane Helicopter by E.E. Gustafsson
Jan 24 1968
108 AD 627-898 An Empirical Method for Calculating the Power Required Due to Compressibility on a Single Rotor Helicopter
July 1965
HELICOPTER AIRFOILS (ROTOR BLADES) 26 1 Report R-107-4 Part II Stress Analysis of Rotor Blades by
a Tabular-Dynamic Method Goodyear Aircraft Corp. Feb 28 1946
2 Report R-107-4 Part IV Helicopter Airload Calculations Goodyear Aircraft Corp.
Mar 5 1946
3 Report R-107-4 Part II-A Stress Analysis of Rotor Blades by a Tabular-Dynamic Method (Expansion of Part II) Contract# W33-038 ac-11439 Goodyear.
Apr 24 1946
4 Report R-107-4 Part III Effects of Second-Harmonic Flapping on the Stresses of a Hinged Rotor Blade Contract# W33-038 ac-11439 Goodyear
May 2 1946
5 Report R-107-4 Part V Stress-Model Method of Determining Bending Moments in R-6 Helicopter Blades Contract# W33-038 ac-11439 Goodyear
Jun 22 1946
6 Report 230.49 Analysis of Low Frequency Rotor Blade Flutter Coupled with Vertical Pylon Motion, for a Rotor Blade Having Flapping and Lag Hinges Kellett
Jun 1947
7 Cornelius Helicopter Rotor Principles Apr 28 1946
66
8 NACA Report No. 293 Two Practical Methods for the Calculation of the Horizontal Tail Area Necessary for a Statistically Stable Airplane
Jan 1929
9 NACA Report No. 349 A Proof of the Theorem Regarding the Distribution of Lift Over the Span for Minimum Induced Drag
C.A. 1930
10 NACA Report No. 362 An Extended Theory of Thin Airfoils and its Application to the Biplane Problem
1930
11 NACA Report No. 383 On the Theory of Wing Sections with Particular Reference to the Lift Distribution
1931
12 NACA Report No. 497 Computation of the Two-Dimensional Flow in a Laminar Boundary Layer
1934
13 NACA Report No. 527 Air Flow in a Separating Laminar Boundary Layer
1935
14 NACA Report No. 546 The Effect of Turbulence on the Drag of Flat Plates
1935
15 NACA Report No. 567 Propulsion of a Flapping and Oscillating Airfoil
1936
16 NACA Report No. 613 The Variation with Reynolds Number of Pressure Distribution Over an Airfoil Section
1938
17 NACA Report No. 684 Static Thrust and Power Characteristics of Six Full-Scale Propellers
1940
18 NACA Report No. 840 Stalling of Helicopter Blades 1946 19 NACA TM No. 921 Contribution to the Aerodynamics of
Rotating-Wing Aircraft Dec 1939
20 NACA TM 907 Dynamic Stability of a Helicopter with Hinged Rotor Blades
Sep 1939
21 NACA TM 929 Aerodynamics of Rotating-Wing Aircraft with Blade-Pitch Control
Feb 1940
22 NACA TM 990 Contribution to the Aerodynamics of Rotating-Wing Aircraft Part II
Oct 1941
23 NACA TM 1312 Calculation of the Bending Stresses in Helicopter Rotor Blades
Mar 1951
24 NACA Wartime Report ARR 3G29 Theory of Self-Exciting Mechanical Oscillations of Hinged Rotor Blades
Jul 1943
25 NACA Wartime Report ARR 3I13 Theory of Mechanical Oscillations of Rotors with Two Hinged Blades
Sep 1943
26 NACA Wartime Report L4H05 Effect on Helicopter Performance of Modifications in Profile-Drag Characteristics of Rotor-Blade Airfoil Sections
Aug 1944
27 NACA Wartime Report L5C12c High-Speed Photographs of a YR-4B Production Rotor Blade for Simulated Flight Conditions in the Langley Full-Scale Tunnel
Mar 1945
28 NACA Wartime Report 5A09 Response of Helicopter Mar 1945
67
Rotors to Periodic Forces 29 NACA Wartime Report L5E10 Evaluation of the Induced-
Velocity Field of an Idealized Helicopter Rotor Jun 1945
30 NACA Wartime Report L5E23 Comparisons of Methods of Computing Bending Moments in Helicopter Rotor Blades in the Plane of Flapping
Aug 1945
31 NACA Wartime Report L6D24 Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections
May 1946
31 NACA RM L54G02 Rapid Estimation of Bending Frequencies of Rotating Beams
Aug 18 1954
32 NACA TN 835 Analysis of Ground Effect on the Lifting Airscrew
Dec 1941
33 NACA TN 1083 Stalling of helicopter Blades Jun 1946 34 NACA TN 1184 Theory of Ground Vibrations of a Two-
Blade Rotor on Anisotropic Flexible Supports Jan 1947
35 NACA TN 1192 Charts Showing Relations Among Primary Aerodynamic Variables for Helicopter-Performance Estimation
Feb 1947
36 NACA TN 1812 The Application of Airfoil Studies to Helicopter Rotor Design
Feb 1949
37 NACA TN 1996 On Internal Damping of Rotating Blades Dec 1949 38 NACA TN 2226 Theoretical Analysis of Oscillations in
Hovering of Helicopter Blades with Inclined and Offset Flapping and Lagging Hinge Axes
Dec 1950
39 NACA TN 2648 Experimental Investigation of Transition of a Model Helicopter Rotor from Hovering to Vertical Autorotation
Mar 1952
40 NACA TN 2714 Normal Accelerations and Operating Conditions Encountered by a Helicopter in Air-Mail Operations
Jun 1952
41 NACA TN 2870 Power-Off Flare-Up Tests of a Model Helicopter Rotor in Vertical Autorotation
Jan 1953
42 NACA TN 2912 The Normal Component of the Induced velocity in the Vicinity of a Lifting Rotor and Some Examples of its Application
Mar 1953
43 NACA TN 3182 Manual of the ICAO Standard Atmosphere
May 1954
44 NACA TN 3376 The Effects of Control Stiffness and Forward Speed on the Flutter of a 1/10-scale Dynamic Model of a Two-Blade Jet-Driven Helicopter Rotor
Apr 1955
45 NACA TN 3844 Theory of Self-Excited Mechanical Oscillations of Helicopter Rotors with Hinged Blades
Feb 1957
46 NACA TN 3849 Analytical Determination of the Natural Coupled Frequencies and Mode Shapes and the Response
Dec 1956
68
to Oscillating Forces Functions of Tandem Helicopters 47 NACA TN 3850 Experimental Investigation of the
Langley Helicopter Test Tower of Compressibility Effects on a Rotor Having NACA 632-015 Airfoil Sections
Aug 1956
48 NACA TN 3852 Flight Measurements of the Vibrations Encountered by a Tandem Helicopter and a Method for Measuring the Coupled Response in Flight
Dec 1956
49 NACA TN 3228 Aerodynamic Investigation of a Four-Blade Propeller Operating Through an Angle of Attack Range from 0o to 180o
Jun 1954
50 NACA TN 3982 Exploratory Study of Ground Proximity Effects on Thrust of Annular and Circular Nozzles
Apr 1957
51 NACA TN 4356 Effects of Compressibility on Rotor Hovering Performance and Synthesized Blade-Section Characteristics Derived from Measured Rotor Performance of Blades Having NACA 0015 Aiorfoil Tip Sections
Sep 1958
52 NASA TN D-43 An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering In and Out of Ground Effect
Sep 1959
53 NASA TN D-73 Comparison of Calculated and Measured Stall Boundaries of a Helicopter Rotor at Advance Ratios from 0.3 to 0.4
Sep 1959
54 NASA TN D-88 Wind-Tunnel Tests of a Semispan Wing with a Fan Rotating in the Plane of the Wing
Oct 1959
55 NASA TN D-89 Wind-Tunnel and Piloted Flight Simulator Investigation of a Deflected-Slipstream VTOL Airplane, the Ryan VZ-3RY
Nov 1959
56 NASA TN D-97 A Note on the Calculation of Helicopter Performance at High Tip-Speed Ratios
Sep 1959
57 NASA TN D-112 Experimental Investigation of the Pressure Fluctuations on a Flat Plate and a Cylinder in the Slipstream of a Hovering Rotor
Aug 1959
58 NASA TN D-123 Investigation of the Effects of a GuideVane-Rotor Combination on Inlet Total-Pressure Distortions in a Compressible Fluid
Dec 1959
59 NASA TN D-124 Static tests of an External-Flow Jet-Augmented Flap Test Bed with a Turbojet Engine
Dec 1959
60 NASA TN D-153 A Flight Study of the Conversion Maneuver of a Tilt-Wing VTOL Aircraft
Dec 1959
61 NASA TN D-175 Dynamic-Model Investigation of the Damping of Flapwise Bending Modes of Two-Blade Rotors in Hovering and a Comparison with Quasi-Static and Unsteady Aerodynamic Theories
Dec 1959
61 NASA TN D-234 Ground Effect for Lifting Rotors in Forward Flight
May 1960
69
62 NASA TN D-240 A Note on the Mean Value of Induced Velocity for a Helicopter Rotor
May 1960
63 NASA TN D-371 Natural Frequencies in bending of Twisted Rotating and Nonrotating Blades
Mar 1960
64 NASA TN D-382 Effect of Blade Cutout on Power Required by Helicopters Operating at High Tip-Speed ratios
Sep 1960
65 NASA TN D-394 Equations for the Induced Velocities Near a Lifting Rotor with Nonuniform Azimuthwise Vorticity Distribution
Aug 1960
66 NASA TN D-624 A Preliminary Study of V/STOL Transport Aircraft and Bibliography of NASA Research in the VTOL-STOL Field
Jan 1961
67 NASA TN D-789 Aerodynamics of a Fan-In-Fuselage Model
May 1961
68 NASA TN D-1548 Wind-Tunnel Tests of two Full-Scale Helicopter Fuselages
Oct 1962
69 NASA TN D-4364 Flight Investigation to determine the Effect of Longitudinal Characteristics on Low-Speed Instrument Operations
Mar 1968
70 NASA MEMO 1-31-59L Parasite Drag Measurements of Five Helicopter Rotor Hubs
Feb 1959
71 NASA MEMO 2-28-59L Comparison of Measured Flapwise Structural Bending Moments in a Teetering Rotor Blade with Results Calculated from the Measured Pressure Distribution
Mar 1959
72 NASA TT F-519 Helicopters – Calculation and Design Volume II. Vibrations and Dynamic Stability (Russian)
May 1968
73 AF TR No. 6352 Longitudinal Stability Characteristics of a Gyroscopically Stabilized Helicopter in Forward Flight
Mar 1951
74 Report CGD 443 Air and Mass Forces in the Case of Helicopter Rotors with Oblique Hinge (Supplemental Report) United Aircraft Corp.
Jul 10 1946
75 Report CGD 444 A Method for the Direct Determination of Flapping in Flight Condition with High Blade Loading
Jul 11 1946
76 Young Two-Bladed Rotor C.A. 1945 77 Basic Helicopter Design Principles Part One: Drive
Mechanisms Dec 1945
78 Analytical Comparison of Helicopter and Airplane in Level Flight by Montgomery Knight Georgia School of Technology
Jan 25 1938
79 AAF Translation No. 510 Air and Mass Forces on Helicopter Propellers with Inclined Hinge by Gerhard Sissingh (German)
Mar 30 1946
80 Report F-TS-643-RE FA-223 Helicopter Interview with Prof. Focke and Inspection of Machine (German)
Jul 3 1946
70
81 Report F-TS-687-RE Stability in Hovering of the Helicopter with Central Rotor Location by K. Hohenemer (German)
Aug 1946
82 Report F-TS-689-RE Investigation of the Influence of Rotor-Diameter, Blade Solidity, and Blade setting on the Thrust of a Rotor with Jet Propulsion by Sissingh (German)
Aug 1946
83 Report F-TS-690-RE Contributions to the Dynamic Stability of Rotary-Wing Aircraft with Articulated Blades by Sissingh (German)
Aug 1946
84 Report F-TS-1001-RE The Performance Characteristics of the Helicopter by K. Hohenemer (German)
Sep 1946
85 Report F-TS-1003-RE Static Thrust Tests of the Model Helicopter Rotor and Preliminary Research of the Model Helicopter Rotor by G. Schoppe (German)
Sep 1946
86 Report F-TS-1007-RE Investigation of the Influence of High Subsonic Velocities on the L/D of Rotary Wing Aircraft by G. Sissingh (German)
Sep 1946
87 Report F-TS-1045-RE The Power Required of the Ideal Helicopter by K. Hohenemer (German)
Jan 1947
88 Report ATI No. 19597 Stress Analysis of a Helicopter Rotor by G. von Sissingh (German)
Jun 1948
89 The Induced Drag of Any Biplane by L.V. Kerber Nov 1 1927 90 MIT – 3 Papers on Helicopter Stability and Notes May 5 1952 91 Cornell University – 2 Articles by Harold Hirsch C.A. 1949 92 Miscellaneous Articles(11) 1943-1956
HELICOPTER AERODYNAMICS/STABILITY 27 1 Report 187 Wind Tunnel Test – Model 37 Beech Aircraft Jun 24 1947
2 Some Opportunities for Progress in Aircraft Performance by George S. Schairer Boeing
Jan 20 1964
3 Advanced Transport Technology Economic Report Task IV – Summary Report Contract# NAS1-10705 and 11238 McDonnell Douglas
Undated
4 A Theory of Identification of the Parameters in the Equations of Motion of a Structure Through Dynamic Testing by William G. Flannelly & Alex Berman Kaman and Joseph H. McGarvey USAAMRDL
Mar 23-25 1970
5 Report E.S.29813 Comparison of Experimental Pressure Distributions with Those Calculated by the Neumann Program Douglas
May 16 1960
6 AF TR No. 6590 Landing Gear Vibration Oct 1951 7 Report 43209A Heavy Logistics Support Aircraft System
Optimization Study Douglas Mar 4 1963
8 Report RAC 1236 The Case for Variable Geometry by A. Wadkovsky Republic
Apr 16 1963
71
9 RASA Report 71-01 An Experimental Study of Tip Vortex Modification by Mass Flow Injection Contract# N0001469-C-0169
C.A. Feb 1971
10 Report ASRL TR 133-2 A Routine Method for the Calculation of Aerodynamic Loads on a Wing in the Vicinity of Infinite Vortices Contract# Now 65-0139-d MIT
May 1966
11 USAAVLABS TR 65-52 A Main Power System for Shaft-Driven Heavy Lift Helicopters Contract# DA 44-177AMC-212(T)
Oct 1965
12 Report FT-125R-69 Limited Flying Qualities and Performance of the PS-1 Seaplane
Nov 20 1969
13 Report FTD-HT-23-710-68 Short Takeoffs for Jet Aircraft by N.K. Liseytsev (USSR)
Jan 31` 1969
14 NACA RM L57E24a Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations
Jul 12 1957
15 NACA RM L58B06 Preliminary Study of Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips
Mar 24 1958
16 NASA Memo 6-11-59L Low-Speed Investigation of the Effects of Horizontal-Tail Area and Wing Sweep on the Static Longitudinal Stability and Control Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips
Jun 1959
17 Report No. D3-71019 A Power Spectral Gust Response Study of Low Level Attack Airplanes
Jan 28 1963
18 Report No. TB-969-F-1 WADC TR 56-223 Flight Evaluation of the Effect of Variable Phugoid Damping in a JTB-26B Airplane Contract# AF 33(616)-2736
Oct 1956
19 Report No. TB-757-F-9 WADC TR 54-441 Artificial Stability Installations in B-26 and F-94 Aircraft
Sep 1954
20 Report No. TB-757-F-10 WADC TR 54-442 Evaluations of Elevator Force Gradients and Types of Force Feel in a B-26
Nov 1954
21 Report No. TB-757-F-12 WADC TR 55-299 Flight Evaluations of Various Longitudinal Handling Qualities in a Variable-Stability Jet Fighter Contract# AF 33(038)20659
Jul 1955
22 Non-Dimensional Power Curves for Aircraft in Level Flight by K. Korsak Piasecki
Undated
23 NASA TN D-217 Low-Speed Investigation of Static Longitudinal and Lateral Stability Characteristics of an
Jan 1960
72
Airplane Configuration with a Highly Tapered Wing and with Several Body and Tail Arrangements
24 NASA TN D-760 Skid Landings of Airplanes on Rocker-Type Fuselages
May 1961
25 Analysis of Thrust Due to the COANDA Phenomenon Contract# AF 61(052)-382
Oct 29 1960
26 Vertical-Gust-Alleviation System for a High-Speed Fighter Aircraft at Low Altitudes
Mar 1961
27 Report No. 133 Theoretical Aerodynamics of Flexible Wings at Low Speeds II-Two-Lobed Parawings Contract# Nonr-3728(00)
May 1 1964
28 Report No. 172 Theoretical Aerodynamics of Flexible Wings at Low Speeds IV-Experimental Program and Comparison with Theory Contract# Nonr-3728(00)
Feb 15 1965
29 Aircraft Preliminary Design Considerations of Range-Payload by Ken Coward General Dynamics/Convair
Undated
30 Pilatus Turbo Porter Model PC-6/A Aircraft Parts Catalog Undated 31 Analytical Study of a Sailwing STOL Lift System for
Limited War Aircraft VRC Sep 10 1965
32 Beechcraft MS 760 Brochure Undated 33 Pilatus Turbo Porter Model PC-6/A Specification Feb 1960 34 Pilatus Turbo Porter Model PC-6/A Aircraft Parts Catalog
(Temporary Edition) C.A. 1960
35 Pilatus Turbo Porter Model PC-6/A Aircraft Service Manual
Dec 1960 Rev Jul 1962
36 Pilatus Turbo Porter Model PC-6/A Airplane Flight Manual
Nov 26 1962
37 ASE 680646 Design and Tests of Inverting Flaps and Wing Span Flaps by Alberto Alvarez-Calderon
Oct 7-11 1968
38 ASE 730898 Propulsion Technology Advances Neede for a Quiet Supersonic transport by Richard L. Foss & Ellwood L. Bragdon Lockheed-California
Oct 16-18 1973
39 AFFTC-TR-59-38 ARDC L-28A Air Force Flight Evaluation
Jan 1960
40 Schulflugzeug Fantrainer AWI 2 VFW-Fokker (in German)
Aug 1972
41 Report LR 25180 Boxplane Configuration – Conceptual Analysis and Initial Experimental Verification Lockheed-California
Mar 30 1972
42 Report 93 Model 26 Aerodynamic Flight Test of AT-10 with 40o V Tail Beech
Aug 20 1944
43 Report 109 Model 33 Aerodynamic Wind Tunnel Test of Model 33 Beech
Aug 8 1947
44 Report 210 Model 35C Aerodynamic Rolling Jan 31 1947
73
Characteristics of Beech Model 35C with Conventional and Differential Ailerons Beech
45 Report No. T-463 UH-2 Stall Warning Flight Test Evaluation Contract# Now 65-0241-f Kaman
Apr 21 1966
46 APGS-TR-64-93 Simulated V/STOL Aircraft Operation Utilizing F-100D Aircraft
Dec 1964
47 Report ER 4223 New Transport Aircraft Lockheed Feb 1 1960 48 Report SM 10233 Study of a High-Altitude; Long
Endurance RPV Wing Structure Concept Goodyear Oct 30 1973
49 Report D180-17477-1 Liquid-Hydrogen-Fueled Aircraft May 15-16 1973 50 Report R-581/4 Airframe Structural Materials for Drone
Applications Rand Jul 1971
51 Overview of RPV Activities of the Boeing Company Apr 19 1973 52 Report SM-14025 Dimensionless Parameters for Airplane
Model Testing Douglas Mar 27 1951
53 Report 808-72-96 A Simplified Example Relating Air Transport Requirements to Aircraft Evaluation Douglas
Jan 1972
54 TAPV 60035E Fiat G95/2 Oct 1 1960 55 Report No. 209 Theoretical Aerodynamics of Flexible
Wings at Low Speeds V-Engineering Method for Estimating Parawing Performance Contract# Nonr3728(00)
Dec 1 1965
56 SK-3287-0 Helio model U-10E Brochure Nov 1 1966
HELO AERODYNAMICS AND KAMAN K-190 28 1 Report No. 3.3 Stress Analysis of Flap Bracket and Hinge
Contract# NOa(s) 9124 Section C Item 1(a) Part 2 Kaman Oct 6 1947
2 Report No. 1.0 Structural Loads Criteria Report Contract# NOa(s) 9124 Item 1(a) Kaman
Oct 24 1947
3 Report No. 2.2 General Performance of the Model K-190A Helicopter by the Kaman Representative Method Contract# NOa(s) 9124 Section C Item 1(a) Part 1(d) Kaman
Nov 5 1947
4 Report No. 2.3 Kaman Method of Detail Aerodynamic Rotor Performance Calculation Contract NOa(s) 9124 Item 1(a) Section C Part 1(d) Kaman
Nov 14 1947
5 Stress Analysis of Hub Assembly, Blade End Assembly and Dampers Contract# NOa(s) 9124 Item 1(a) Section C Part 2 Kaman
Nov 15 1947
6 Report No. 2.4 Kaman Representative Station Method of Helicopter Performance Calculation Contract# NOa(s) 9124 Item 1(a) Section C Part 1(d) Kaman
Nov 18 1947
7 Report No. 3.2 Load Determination and Stress Analysis of Flap Contract# NOa(s) 9124 Item 1(a) Section C Part 2
Nov 22 1947
74
Kaman 8 Report No. 2.1 Hovering Detail Analysis Contract# NOa(s)
9124 Section C Item 1(a) Part 1(d) Kaman Nov 26 1947
9 Report No. 3.1 Blade Stress at Hovering with 135 Percent Maximum Rotative Speed Contract# NOa(s) 9124 Section C Item 1(a) Part 2 Kaman
Nov 29 1947
10 Report No. 6.0 Structural Description of the Kaman Rotor Contract# NOa(s) 9124 Section C Item 1(a) Part 1(b) Kaman
Dec 1 1947
11 Report No. 3.4 Load and Stress Analysis of Rotor Controls Contract# NOa(s) 9124 Section C Item 1(a) Part 2 Kaman
Dec 8 1947
12 Report No. 7.0 Strength Summary and Operating Restrictions Contract# NOa(s) 9124 Section C Item 1(a) Part 1(f) Kaman
Dec 11 1947
13 Report No. 8.0 Loads report Contract# NOa(s) 9124 Section C Item 1(a) Part 1(c) Kaman
Dec 11 1947
14 Development of the Kinematic Focal Isolation System for Helicopter Rotors by Rodney W. Blake Bell
May 1968
15 USAAVLABS TR 68-57 Installation of a High-Reduction-Ratio Transmission in the UH-1 Helicopter Contract# DA 44-177-AMC-411(T)
May 1969
16 Bell Helicopter Military Products Reference Data May 1 1967 17 NASA TM X-3185 Wind-Tunnel Investigation of
Helicopter-Rotor Wake Effects on Three Helicopter Fuselage Models
Mar 1975
18 USAAVLABS TR 67-23 Cost Effectiveness Study of Heavy Lift Aerial Vehicles Contract# DA 44-177-AMC205(T)
Oct 1967
19 Report No. 190V-902 Analysis of Blade C.G. and/or A.C. Offset Stabilizing System (with Viscous and Elastic Restraint) Applied to the XH-26, Pulse-Jet Helicopter Contract# AF 33(600) 15220
Feb 18 1955
20 Report No. 190V-901 Analysis of Displacement Bar Stabilizing System Applied to the XH-26 Pulse-Jet Helicopter Contract# AF 33(600) 15220
Feb 18 1955
21 WADC TR 55-407 Investigation of helicopter Stability and Control in Hovering and Forward Flight
Dec 1956
22 Progress in Dynamic Analysis and Automatic Control of Helicopters by R.P. Walton & L.G. Campbell, Jr. J.B. Rea Company Contract# AF 33(616)-108
Undated
23 Report No. 190-H-1 Investigation of Stability and Control of Small Helicopters with and Without Various Stabilizing Systems Contract# AF 33(600)-15220
Dec 31 1952
24 Unsteady Aerodynamic and Stall Effects on Helicopter Rotor Blade Airfoil Sections by Jaan Liiva Boeing Vertol
Jan 1968
75
25 Blade Tip Aerodynamics – Profile and Planform Effects by Richard F. Spivey Bell
May 1968
26 Dynamic Stall of Airfoil Sections for High-Speed Rotors by Jaan Liiva & Franklyn J. Davenport Boeing-Vertol
May 1968
27 The Effect of Advanced Propulsion on Future Rotary-Wing-type Aircraft by L.M. Graham, A.W. Schulz & H.C. Smith Bell
Jun 10-14 1968
28 Helicopter Instrument Operations in Terminal Areas by Alder P. Betti Flight Standards Service
May 14 1965
29 Present and Future Roles of the Helicopter by L.L. Douglas & J.J. Schneider Boeing-Vertol
Oct 1965
30 Control and Maneuver Requirements for Armed Helicopters by H.K. Edenborough & K.G. Wernicke Bell Helicopter (with attached sketches and photos)
May 13-15 1964
31 AHS 24th Annual National Forum – Articles # 200, 205, 207, 208, 214, 215, 217, 221, 223, 224, 225, 226, 227, 228, 229, 230, 231, 232
May 8-10 1968
32 Helicopter Propulsion Trends by C.W. Ellis, J. Acurio & J.J. Schneider Boeing-Vertol
Undated
33 Experimental Boundary Layer Study on Hovering Helicopters by W.H. Tanner Bell Helicopter & P.F. Yaggy Ames Research Center
May 11-13 1966
34 Operating History and Experience with Boeing Helicopters by Howard N. Stuverude Boeing-Vertol
Nov 14-16 1967
35 The Boundary Layer of the Hovering Helicopter by W.H. Tanner Bell Helicopter & P. Buettiker Arlington State College
C.A. 1967
36 SAE 680672 Structural Fatigue Considerations in the Design of Rotary-Wing Vehicles by H.G. Smith Hughes Tool
Oct 7-11 1968
37 SAE 680673 Vulnerability and Crashworthiness in the Design of Rotary Wing Vehicle Structures by Melvin J. Rich Sikorsky
Oct 7-11 1968
38 Stowed Rotor Assault Transport Parametric Study Boeing-Vertol
Undated
39 Field Repairable-Expendable Main Rotor Blade by A.S. Falcone & J.E. Miller Kaman
1977
40 Report No. R-442 10-Ton Intra-Theater Transport Kaman Oct 24 1962 41 The Pressure-Jet Helicopter Propulsion System by J.B.
Nichols The Aerospace Corp. Sep 1972
42 An Evaluation of Some Important Stability Parameters that Influence Helicopter Flying Qualities by Alfred Gessow & Kenneth B. Amer Langley
Undated
43 WADC TR 58-54 Part I A Study of the Frasibility of Using a Semi-Rigid or Articulated Rotor System on a Tilt-Wing VTOL Aitcraft
Oct 1957
76
44 AGARD-CP-121 Advanced Rotorcraft Volume I Sep 20-23 1971 45 AGARD CP No. 31 Helicopter Propulsion Systems Jun 1968
ROTORS 29 1 Report No. 204-099-702 Aerodynamic Data for Use in the
Selection of Design Parameters for Semi-Rigid Multi-Blade Rotors Contract# AF33(600)-30299 Bell
Mar 8 1957
2 Report no. 47-980-113 Initial Flight test evaluation of X47-120-400 Three-Bladed Rotor Contract# AF33(600)30299 Bell
Apr 1 1957
3 Report No. 299-099-072 Proposal for the Construction and Test of an Experimental Rotor Blade Suitable for Operation at High Tip Mach Number Bell
Nov 6 1957
4 Report No. 299-099-086 A Proposal for an Applied Research Program in the Field of Helicopter Aerodynamics Bell
Apr 7 1958
5 Report No. 8011-099-002 The Weights of Very Large Rotors for Nuclear Powered Helicopters Bell
Apr 23 1959
6 Report No. 299-010-051 Proposal for Extended Studies of the Three-Bladed Semi-Rigid Rotor System on the HU-1 Helicopter Bell
Jun 15 1959
7 Report No. 299-010-050 Proposal for Developing a Means of Measuring Rotor Loads Bell
Feb 14 1958
8 Report No. 6751 Proposal for Forward Flight-Tests of High Speed Rotor Blades McDonnell
Apr 15 1959
9 Report No. 1078 Charts for Estimating Blade Stall for Jet Rotors Contract# AF33(038)-937 McDonnell
Mar 18 1948
10 Report No. SM-18310 Preliminary Report on Some Aerodynamic Problems of Vertical Capability Transport Douglas
Apr 4 1954
11 Report No. SM-18294 Vertical Capability Transport – Model 1845 Douglas
Mar 24 1954 Rev. Apr 9 1954
12 WADC Report 52-256 Low-Range Air-Speed Indicator for Helicopters Contract# AF33(038)-22265
Oct 1952
13 NACA TN 2062 Dynamic Similitude Between a Model and a Full-Scale Body for Investigation at Full-Scale Mach Number
Mar 1950
14 Report No. C-266 Wind-Tunnel Tests of a 0.10-Scale Model of the HRP-2 Helicopter Without Rotors Part II – Longitudinal and Lateral Characteristics with Revised Afterbody
Oct 1949
15 Research Report #23 An Application of Boundary Layer Control to Rotating Blades Mississippi State Univ.
May 30 1959
16 Report No. 240 On the Design of Models for Helicopter Research and Development Princeton Univ.
Oct 1953
77
17 Report No. 338 Instrumentation of a Tandem Helicopter for Static and Dynamic Stability and Control Flight Tests Princeton Univ.
Mar 1956
18 Report No. SER-2187 Analytical Solution of Static Longitudinal Trim in Hovering and Forward Flight Contract# AF33(038)-14807 Sikorsky
Apr 8 1953
19 Proposal for Developing Optimum Rotor Blades Prewitt Apr 27 1959 20 Report No. 16-X-2 PiAC-16 Helicopter with Shrouded
Propeller for Torque Correction Mar 25 1957 rev. Apr 11 1957
21 Report No. PR-198 Proposal for a Flight Test Program to Determine the Effect of Pulsating Aerodynamic Pressures on Tandem Rotor Helicopter Vibrations Vertol
Dec 6 1957
22 Report No. 121X90-5 Proposal to Determine a Method for Specifying Design Loads Associated with Flight Maneuver and Skid Landing Maneuver Criteria Kellett
Jan 1959
23 Report No. F-TS-1003-RE Static Thrust Tests of the Model Helicopter Rotor and Preliminary Research of the Model Helicopter Rotor by G. Schoppe (from German)
Sep 1946
24 An Investigation of the Experimental Aerodynamic Loading on a Model Helicopter Rotor Blade Contract# NAw-5983 MIT
Feb 1951
25 Report No. 510 Air and Mass Forces on Helicopter Propellers with Inclined Hinge by Gerhard Sissingh (from German)
Mar 30 1946
26 Report No. F-TS-689-RE Investigation of the Influence of Rotor-Diameter, Blade Solidity, and Blade Setting on the Thrust of a Rotor with Jet Propulsion by Sissingh (From German)
Aug 1946
27 WADC TR 58-124 A Design Investigation of a Propeller Air Flow Measurement System
Apr 1958
28 Report No. 30—929-111 Model Tests on Underslung Rotor Bell
Nov 8 1944
29 Application of Boundary Layer Control to Rotor Blades Progress Reports for Sep 1953, Nov 1953, Mar 1954
Oct 17 1953
30 Business Proposal for a One Man Ultra-Light Helicopter United Technical Industries
Apr 1983
31 Development of Air Mobility by Helicopter Second Edition Boeing-Vertol
Aug 1 1968
32 Helicopter Range & Speed Extension by Aerial Towing with Fixed-Wing Aircraft
May 29 1969
33 The “Heliocoupe” A New Light Helicopter Design Helicopter Research Lab. Dayton, OH
Feb 1946 Rev. Mar 4 1946
34 Report No. AN 01-230HB-2 Pilot’s Flight Operating Instructions for Army R-5A/Navy HO2S-1 Helicopters
Feb 25 1945
35 Report No. AN 01-230HB-1 Erection and Maintenance Instructions for Army R-5A/Navy HO2S-1 Helicopters
Apr 25 1945
78
36 Report No. AN 01-230HB-4 Pilot’s Parts Catalog for Army R-6A/Navy HOS-1 Helicopters
Feb 20 1945
37 Summary of Rotary Wing Projects of Aircraft Projects Section ( by Models) TSEOA-5 AMC
Jan 1945 rev. Feb 1947
38 R 420-71-LC-14b Helicopter Propulsion System Study Contract#AF33(038)-22185 Thermal Research& Engineering Corp.
Sep 1952
39 The Impact of technology on Payloads of Very Large Helicopters by Lewis G. Knapp, Wilfried Meier & David Unsworth Sikorsky
Sep 23-25 1969
40 WADC TR 57-583 Part I Helicopter Configuration and Propulsion Systems Study Part I. Statistical Weight Analysis
Nov 1957
41 Cost Effectiveness Comparison of Heavy Lift Helicopter Systems HTC
C.A. 1970
42 The STORC Approach to the Helicopter Ferry Problem by J.B. Nichols Hiller
Undated
43 Hughes Hot Cycle Presentation Undated 44 The Hot Cycle Propulsion System Research Program by
K.B. Amer HTC Undated
45 The Hot Cycle Flying Crane Helicopter by Harvey O. Nay & Robert J. Sullivan HTC
Jan 1963
46 Jet Propelled Rotor for Helicopters Undated 47 ER No. 63-24 Tip Turbojet Powered Heavy-Lift Rotor
System Hiller Undated
48 ER No. 62-66 1962 Flying Crane Design Study Hiller Jun 1962 49 Report No. 58-142 Proposal for the Development of Large
Transport and Crane Helicopters Powered by Rotor Tip Mounted Turbojets Hiller
Nov 1958 rev.1 Jul 1959
50 The Application of Tip Turbojets to the Solution of Design and Operating Problems of Large Helicopters by John B. Nichols Hiller
May 12 1960
51 Summary Report on New family of V.T.O.L. Vehicles Mar 1963 52 Report No. 29472-7 Proposal for Development of
Aerocrane (A Lightweight, Very High Payload Flying Crane) Ryan
Jul 15 1966
53 Environmental Effects on Rotor Tipjet Propulsion by E.R. Sargent, R.M. Lockwood & M.F. Gates Hiller
Oct 1956
54 Tip Turbojet Powered Heavy Lift Aerial Vehicle Hiller & Continental
Mar 1962
55 Report No. 62-39 Tip Turbojet Powered Heavy Lift Aerial Vehicle Part I: Airframe Program Hiller
Mar 1962
56 Report No. 62-12 Proposal for Flight Demonstration of Rotor Tip Mounted Turbojets Hiller
Jan 1962
57 Report AMCA-70-001 Aerial Very Heavy Lift Concepts for the 1990 Army Volume I – Basic Report
Nov 1969
79
58 A Flying Crane Readily Convertible to a High Speed VTOL Transport – Slide Presentation
Undated
59 Paper No. 20 Research and Development on Rotors with Tip Jet Drive in Germany by Christoph Fischer Dornier
Sep 1971
60 AHS 27th Annual V/STOL Forum Paper 552 Size Effects on the Design of Large Rotor Systems by Henry G. Smith HTC
May 1971
61 AHS 27th Annual V/STOL Forum Paper 561 Turbofan Engine Considerations for Reaction Drive Rotors by R.J. Sullivan HTC
May 1971
62 Optimization of Design Data for Reaction Drive Helicopters by Werner Goller Dornier
Jan 1970
HELICOPTER/ROTOR AERODYNAMICS 30 1 Helicopter Development 1939-1950 Volume 3 (original
Manuscript) 1954
2 The Domain of the Helicopter by Raoul Hafner, F.R.Ae.S Bristol Aeroplane Co., Ltd.
Oct 1954
3 Proposal to Develop a Small VTOL Remotely Piloted Vehicle (original) probably by Lindenbaum
Undated
4 Miscellaneous Articles – Early Helicopters Various 5 Hover Tests of a Model H-Force Rotor by H.R. Velkoff
Ohio State Univ. Sep 8-11 1981
6 A Note on Rotary Wing Hovering and Takeoff Performance, Data Acquisition and Analysis by John C. Kidwell USArmy Test & Eval. Command
Undated
7 Preliminary Study of the H-Force Rotor by Henry R. Velkoff & Thomas W. Parker Ohio State Univ.
Oct 22-24 1980
8 FAA-P-8100.1 Rotorcraft Master Plan Sep 1987 9 Air-Jet Helicopter Air-Jet Development Corp. Undated 10 Piasecki – Miscellaneous Information 1956-1959 11 The Boeing Fiberglass Blade Manufacturing Story
Brochure Undated
12 Helicopter Research & Development Conference Bell May 16-17 1961 13 DH_2011 Experimental Helicopter Undated 14 Report No. 150-FT-1004P Proposal for a Variable Sweep,
Oscillating Pitch Rotor Blade Airfoil Test Program HTC Apr 1972
15 Report No. 150-A-1005P Optimum Pitch Rotor System Wind Tunnel Model Test HTC
Mar 1972
16 Report 150-A-1006P Aerodynamic Testing of Bidirectional Airfoil Sections
C.A. 1972
17 Current Status of the helicopter by Henry R. Verkoff Ohio State Univ.
Sep 21 1967
18 Selected Data from HTC-AD OPR Computer Studies Undated 19 Optimum Pitch Rotor (OPR) Presentation Handout HTC Undated
80
20 A Nonlinear Aeroelastic Loads Analysis of Rotary Wings by A.Z. Lemios Kaman
Undated
21` Calculated and Measured Thrust, Torque and Performance of a Helicopter Rotor by P.E. Hemke, Louis Levoy & Wm. E. Wayman
Undated
22 Report No. 1-001-003 Theoretical Background for the Vaughen Helicopter Rotor System
C.A. 1958
23 Report No. 2-000-001 Technical Proposal Phase I Development Program for the Vaughen Rotor System
C.A. 1958
24 Report No. 2-000-001R Revised Proposal Phase I Development Program for the Vaughen Rotor System
C.A. 1958
25 Vaughen Aircraft Corp. Correspondence Concerning Their Rotor System
1958
26 Instrument Flight Investigation in Helicopters by Owen Q. Niehaus Bell
Undated
27 The Hiller “L” Rotor Control and Stability Augmentation System
May 1963
28 Report No. R-309 Advanced Rotor Configuration Research Boeing-Vertol
Feb 15 1963
29 Report No. 659 Aerodynamic Characteristics of Helicopter Rotors Princeton Univ.
Dec 1963
30 Reports and Translations No. 1021 Survey on German Research and development of Rotary Wing Aircraft by G. Sissingh (from German)
Aug 1 1948
31 FSTC-HT-23-1472-72 Helicopter Design by V.N. Dalin (from USSR)
1971
32 F-TS-9747/V The Aerodynamic Design of Helicopters by B.N. Yur’yev Part I of II
Apr 1960
33 F-TS-9747/V The Aerodynamic Design of Helicopters by B.N. Yur’yev Part II of II
Apr 1960
34 Report No. G-71 Interim ER on Internal Combustion Engines and Hose-Cable Assemblies for a Tethered Antenna Supporting Helicopter Contract# AF 30(602)-675 Kaman
Aug 1 1954
35 USAAMRDL-TR-74-56 Analysis of Unmanned, Tethered, Rotary-Wing Platforms
Jul 1974
36 Report No. A.A.E.E./Res/264 Aeroplane and Armament Experimental Establishment The Low Speed Performance of a Helicopter UK Min. of Supply
May 15 1952
37 R & M No. 1730 The Flight of a Helicopter Nov 28 1935 38 Tech. Note AERO.2131 Helicopter Behavior in the Vortex
Ring Conditions UK Royal Aircraft Estab. Nov 1951
39 AHS SW Regional Meeting Turning a Rotor into Profit by Harry W. Mitchell Bell
Oct 22 1954
81
40 AHS 21st Annual Forum A Study of the Turbine Integrated Geared Rotor for the Heavy-Lift Helicopter by Robert B. Bossler, Jr. Kaman
May 12-14 1965
41 AHS 25th Annual Forum Paper No. 341 A Comparison of Dynamically Scaled Model Rotor Test Data with Discrete Azimuth Aeroelastic Stability theory by Charles F. Niebanck Sikorsky
May 14-16 1969
42 AHS 33rd Annual Forum Paper 77.33.12 The Army’s Improved Main Rotor Blade for the AH-1 Helicopter by Paul F. Maloney Kaman, Larry G. Dite Army Avn Syscom, & Robert D. Powell USAAMRDL
May 1977
43 AHS 34th Annual Forum Paper 78-36 Filament Wound Main Rotor Blade – The Army’s New Production Blade for the AH-1 by Mark L. White Kaman Aerospace
May 1978
44 AHS 35th Annual Forum Paper 79-38 Rotorshaft Torquemeter by Robert B. Bossler, Jr. Kaman
May 1979
45 AHS 35th Annual Forum Paper 79-40 Ground Test Vehicle Testing by H.D. Jones USAA R&D Command
May 1979
46 AHS 35th Annual Forum Paper 79-43 Certification of Composites in Civil Aircraft by R. Allen & J.R. Soderquist FAA
May 1979
47 AHS 35th Annual Forum Paper 79-49 Helicopter Component Environmental Vibration Testing by Dr. Sam T. Crews USAA R&D Command
May 1979
48 NASA TN D-2628 Wind-Tunnel Investigation of a Lifting Rotor Operating at Tip-Speed Ratios from 0.65 to 1.45
Feb 1965
49 Rigid Rotors vs. Hinged Rotors for Helicopters by Bertram Kelley
Mar 25 1963
50 AIAA Paper No. 64-784 Technology Contributions of the CH-53A Weapons System Development Program by Edward S. Carter, Jr. Sikorsky
Sep 21-23 1964
51 Lockheed Rigid Rotor Helicopter Article and 2 Blueprints 1963-1965 52 Fiat 7002 Helicopter – Letter and Notes Jan-Feb 1960 53 Helicopter Articles and Other Papers Various
HELICOPTER VIBRATION, MISC. HELICOPTERS 31 1 Alouette Helicopter Brochures (6) Various
2 Helicopter Brochures (13) Various 3 FT-58R-67 Navy Evaluation of the Fairchild-Hiller Model
FH-1100 Light Turbine-Powered Helicopter NATC Sep 22 1967
4 Advanced Commercial Helicopter Presentation Summary Boeing-Vertol
May 1967
5 AHS 23rd Annual Forum Paper No. 113 The US Army Hueycobra - Configuration and Design Considerations by Charles M. Seibel Bell
May 11-13 1967
6 AHS 23rd Annual Forum Paper No. 112 The Dollar Value May 11-13 1967
82
of Empty-Weight Control in Helicopters by Kenneth B. Amer & Robert J. Sullivan HTC
7 AHS 23rd Annual Forum Paper No. 111 Methods for Improving Flying Qualities of Compound Helicopters by W.E. Blackburn Kaman
May 11-13 1967
8 Report SER-50174 Sikorsky High Performance Helicopter Oct 1961 9 USAAMRDL TR 71-23 Advanced Anti-Torque Concepts
Study Jul 1971
10 USAAMRDL TR 71-44 Advanced Anti-Torque Concepts Study
Aug 1971
11 Report No. R-140A KAMAN Model K-600 Local Crash Rescue Helicopter for the USAF
Dec 1 1956
12 Report No. AD872906 AH-56 Cheyenne Control Augmentation System Study
Jul 1970
13 WADC TR 55-437 An Investigation of the Handling Characteristics of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers – Part I Analytical Evaluation of Stabilizers
May 1957
14 Report No. R-140C Detail Specification KAMAN Model K-600 Crash rescue Helicopter for the USAF
Sep 5 1957
15 Practical Instrument Flying in the Helicopter by Joseph A. Cannon & Owen A. Niehaus Bell helicopter
Undated
16 Report No. SER-3309 Model Specification – Model H-19B (MDAP) Helicopter 12-Place, Single-Engine Contract# AF33(600)-22310 Sikorsky
Nov 17 1953
17 AHS (23rd) National Forum The US Army Hueycobra Configuration and Design Considerations by Charles M. Seibel Bell
May 10-12 1967
18 Report No. 56-66 Proposal to the USAF – Local Crash Rescue Helicopter Hiller
Jun 1956
19 Report No. SER-2556 Summary Report – Long Range Helicopter Design Study Contract# AF33(616)-2628
May 27 1955
20 Report No. 80X-80-1 Proposal for a Study to Investigate the Possibility of Obtaining Substantial Improvement in Range and Cruise Speed Performance for Helicopters Contract# USAF PR 383905
Apr 1954
21 Report No. 1081 Calcul Des Forces Aerodynamiques Instationnaires Sur Les Pales D’un Rotor D’Helicoptere (in French)
1972
22 DOD Contract DA 44-177-TC-420 with Bell helicopter for a Preliminary Design Study for a Two-Place Helicopter
Mar 29 1957
23 AIAA Paper No. 71-994 The Heavy Lift Helicopter Program – An Advanced Technology Solution to Transportation Problems by Ben Tencer & J.P. Cosgrove Boeing
Oct 25-28 1971
83
24 Paper No. 3 The Developing Technology and Economics of Large Helicopters by John J. Schneider Boeing-Vertol
Sep 16-19 1980
25 Report No. RD46-310000-1 Final Report on Preliminary Design Study of Optimum Army Two-Place Observation Helicopter Contract# DA 44-177-TC-419
Aug 30 1957
26 Acoustic Effects of Rotor-Wake Interaction During Low-Power Descent by Bruce D. Charles
May 6-7 1975
27 The Bert Kelley Award Technical Presentations for 1968 1968 28 Report No. 190-F-1 Preliminary Design Study – Army
Two-Place Helicopter – Final Summary Report Nagler Helicopter Co.
Sep 6 1957
29 USAAVLABS TR 68-42 An Analytical and Model Test Research Study on the Kaman Dynamic Antiresonant Vibration Isolator (DAVI) Contract DA 44-177-AMC391(T)
Nov 1968
30 USAAVLABS TR 68-60 Studies of Helicopter Rotor Noise Contract# DAAJ02-67-C-0023
Jan 1969
31 USAAVLABS TR 70-30 The Exploratory Development of the Three-Dimensional Dynamic Antiresonant Vibration Isolator for Rotary-Wing Application Contract# DAAJ0269-C-0003
Aug 1970
32 Assorted Blueprints Various
ROTORS, AERIAL UTILITY VEHICLE 32 1 Report No. 299-099-086 A Proposal for an Applied
Research Program in the Field of Helicopter Aerodynamics Bell
Apr 7 1958
2 Report No. 299-099-110 A Proposal to Experimentally Determine High Speed Rotor Performance, Including Effects of Stall and Compressibility, and Comparisons with Theory
Apr 14 1959
3 Report No. 299-099-113 An Analytical Study of the Longitudinal Stability of Tandem Rotor Helicopters Contract# BuAer NOa(s) 58-534-c Bell
Jul 13 1959
4 Report No. 299-099-137 Final Report – Analytical and Experimental Studies of the Flying Qualities of Tandem Rotor Helicopters Contract NOa(s) 58-534-c Bell
May 25 1960
5 Report No. 204-099-928 Model XH-40 Revised Design Three Bladed Rotor Ground and Flight Tests Contract# AF 33(600)30299 Bell.
Apr 16 1959
6 Report No. 204-099-929 Investigation of Rotor Behavior Following Throttle Chop – YH-40 Helicopter Bell
Jul 10 1959
7 Report No. PR-191 A Study of Boundary Layer Control to Reduce Helicopter Download Vertol
Sep 4 1957
8 Report No. PR-225 Program for the Improvement of the Static Longitudinal Stick Position vs. Forward Speed
Feb 19 1958
84
Characteristics of Tandem Rotor Helicopters Vertol 9 Report No. PR-267 Proposal for Flight Test and Evaluation
of Hydromechanical Stability Augmentation System Vertol
Sep 22 1958
10 Wind Tunnel Tests on Four Model Helicopter Rotors in Vertical Descent by Walter Castles, Jr. & Robin B. Gray Georgia Institute of Technology Contract# NAw 5527
May 1960
11 Report No. PR-106 Proposal for the Advancement of Techniques for V/STOL Lift and Propulsion Systems Vanguard Air & Marine Corp.
Aug 31 1961
12 SBD Report No. TR 59-77 Aerial Platform Monthly Progress Report for Sep 1959 Contract# DA-44-177-TC397 Curtiss
Oct 1 1959
13 SBD Report No. TR 59-87 Aerial Platform Monthly Progress Report for Oct 1959 Contract# DA-44-177-TC397 Curtiss
Nov 6 1959
14 Report No. SM-18311 Helicopter Vibration Model 1845 Douglas
Apr 9 1954
15 Report No. ARD-213 Static Lift Characteristics of Jet Slots – A Clarifying Study of the External Ejector –Final Report Contract# Nonr 2428(00) Hiller
Oct 15 1958
16 ER No. 59-25 21 Ton Payload Flying Crane Helicopter for Army Missions Hiller
Mar 1959
17 ADC Report No. 520-2/R34/46 Monthly Progress Report on the Aerial Utility Vehicle Apr 1 – Apr 30 Contract# DA-44-177-TC-397 Aerophysics
May 5 1958
18 ADC Report No. 520-2/R35/46 Monthly Progress Report on the Aerial Utility Vehicle May 1 – May 31 Contract# DA-44-177-TC-397 Aerophysics
Jun 5 1958
19 ADC Report No. 520-2/R36/46 Monthly Progress Report on the Aerial Utility Vehicle Jun 1 – Jun 30 Contract# DA44-177-TC-397 Aerophysics
Jul 8 1958
20 ADC Report No. 520-2/R37/46 Monthly Progress Report on the Aerial Utility Vehicle Jul 1 – Jul 31 Contract# DA44-177-TC-397 Aerophysics
Aug 7 1958
21 ADC Report No. 520-2/R38/46 Monthly Progress Report on the Aerial Utility Vehicle Aug 1 – Aug 31 Contract# DA-44-177-TC-397 Aerophysics
Sep 9 1959
22 ADC Report No. 520-2/R31/46 Monthly Progress Report on the Aerial Utility Vehicle Feb 1 – Feb 28 Contract# DA-44-177-TC-397 Aerophysics
Mar 5 1958
23 TREC TR 60-70 Study of the VTOL Downwash Impingement Problem Contract# DA-44-177-TC-689
Nov 1960
24 WADC Technical Note 58-98 AD-151146 Investigations Jan 1958
85
Toward the Development of an Aerodynamic Strip Analysis for Single Rotation Propellers Operating at Low Airspeeds and/or Low Advance Ratios
25 Preliminary Report – Phase II Evaluation of XV-1 Convertiplane
Jun 1956
26 Report No. 230.58 Model XR-17 A determination of the Rotor Horsepower Required for Hovering Flight Including the Effects of Varying the Pitch, Chord and Airfoil Section Along the Span Kellett
Apr 1947 Rev. Apr 30 1948
27 Report No. 124X90-3 Proposal for Low-Cost Fuselage Construction Using Reinforced Plastics Kellett
Apr 1958
28 Preliminary Presentation of Results on VTOL Operational Limitations Due to Downwash Effects Contract# Now 600450-f
May 1 1961
29 Report No. H-123-3 Stability of Rotor Blade Flapping Motion Contract# NOa(s)-3703 McDonnell
Jan 23 1946
30 ER 1079 Charts for Estimating the Autorotative Performance of Jet Rotors Contract# AF 33(038)-937 McDonnell
Mar 18 1949
31 ER 1100 An Autorotative Performance Study of the Model 38 Flyable Test Stand Contract# AF 33(038)-937 McDonnell
Mar 18 1949
32 Report No. SER-74 Induced Velocity in Level Flight Contract# W535 ac-29005 Sikorsky
Dec 22 1944
33 Report No. SER-1524 A Comparison Between Modified Tandem and Full Tandem Type Helicopters Sikorsky
Mar 17 1947
34 Report No. 22-A-05 Report on Methods and Computations Used in Selecting Rotor Physical Characteristics and Efficiencies for the H-21 Helicopter Contract# AF 33(038)-12881 Piasecki
Apr 1951
35 Report No. RP-42 Helicopter Stability Criteria Cessna Jan 9 1959 36 Report No. DR-306 Engineering Flight Test Evaluation of
Doman Rotor System Contract# NOas58-679-c Doman Mar 30 1959
37 Limited Flight Evaluation of the English Fairey Rotodyne by Charles C. Crawford & Maj. Walter J. Hodgson
Undated
HELICOPTER TOWING & RANGE EXTENSION 33 1 Helicopter Towing Presentation Including Slides, Notes
Photos, Vugraphs & Background Data 1998
2 Report No. M-E109 Mid Air Cargo Transfer to Rotary Wing Aircraft All American Engineering Co.
Jan 1967
3 AHS 5th Annual Western Forum A Study of the Attainable Range of Helicopters by Abraham C. Adler & Helen S. Holm Cornell
Sep 25-26 1958
4 Report No. 2-809 Analysis of Rotary Wing Gliders as a Jan 1949
86
Type Eastern Rotorcraft 5 Memorandum RM-3809-PR Parasiting Versus Aerial
Refueling for Support of Combat Aircraft Rand Corp. Mar 1964
6 UH-2C Brochure Kaman 1967 7 Report NO. SER-1906 Aerodynamic Analysis of a
Helicopter Towed as a Glider Contract# M 6549-2 Sikorsky
Jan 19 1949
8 Helicopter Range Extension by Means of Aerial Towing and Hock-On by B.T. Wolfson & B. Lindenbaum ARDC WPAFB
Undated
9 Proposed Helicopter Towing Arrangements Various 10 Report No. P-149 Stress Analysis – Helicopter-In-Flight
Pick-Up Kit Contract# AF 33(600)-18639 All American Engineering
Apr 1953
11 Report No. TR 11-100 Study of “Pick-A-Back” Operation of an H-5H Helicopter on a C-119B Airplane Part I: Theory and Design Contract# AF 33(616)-239 Thieblot Aircraft Co.
Oct 10 1957
12 Report No. TR 11-100 Study of “Pick-A-Back” Operation of an H-5H Helicopter on a C-119B Airplane Part II: Wind Tunnel Tests Contract# AF 33(616)-239 Thieblot Aircraft Co.
Oct 10 1957
13 A V/STOL Cargo/Transport Glider System by B. Lindenbaum
Mar 1972
14 A V/STOL System for Light & Medium Intratheater Transport (LIT/MIT) by B. Lindenbaum
Mar 1972
15 Vertical Take-Off and Landing “Glider” Concept Weekly Activity Report
Jul 26-30 1971
16 “Mother-Daughter” Operation of Helicopter with Airplane to Improve Rescue Capability Proposal Paperwork by B. Lindenbaum
1967-1968
17 Helicopter Towing Notes Lindenbaum/Kaman/Lockheed 1981 18 LIT (Light Intratheater Transport) Tilt Wing and “Glider” 1971 19 V/STOL Towed Glider notes from AHS Meeting Jun 13 1975 20 VTOL Glider – Miscellaneous Notes Various
21 Report No. ER 9736 “Project Dock” A Self-Contained System for Launch, Control and Recovery of Drones Lockheed-Georgia (2 copies plus notes)
Jan 1968
22 Canadair CX-84 VTOL Glider Concept Jul 20 1971 23 B36/F84E Photos & Negatives Undated 24 Miscellaneous Articles and Photos Various
HUGHES HOT CYCLE ROTOR/WING COMPOSITE AIRCRAFT
87
34 1 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 2 Performance Data HTC
May 1966
2 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 3 Propulsion System HTC
May 1966
3 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 4 Weight and Balance HTC
May 1966
4 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 6 Structures Part I HTC
May 1966
5 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 6 Structures Part II HTC
May 1966
6 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft section 11 Results of Model Testing HTC
May 1966
7 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 16 Preliminary Model Specification HTC
May 1966
8 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 16 Parametric Studies and Alternate Configurations HTC
May 1966
9 Report No. HTC-66-10 TR Hot Cycle Rotor/Wing Composite Research Aircraft Program Summary HTC
May 1966
10 Report No. HTC 65-15 Volume III Appendices G and H Summary TR Rotor/Wing Concept Study HTC
Sep 1965
HELICOPTERS 35 1 WADC TR No. 55-437 Part II An Investigation of the
Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Contract# AF 33(616)-2780
Jan 1958
2 Report No. 102X90-4 An Investigation of the Handling Qualities of a Tandem Rotor Helicopter (H-21) Equipped with a Gyroscopic Stabilizing System Contract# NOas 56796-c Kellett
Aug 1 1958
3 AFFTC-TN-57-13 Effect of Gross Weight and Center of gravity Location on Dynamic Stability of a Tandem Rotor Helicopter in Forward Flight
Jun 1957
4 Wing-Rotor Interaction by Robert R. Lynn Bell 1966 5 Investigation of Helicopter Stability and Control in Feb 28 1956
88
Hovering and Forward Flight Final Report Contract# AF 33(616)-108
6 Convertawings Inc. “Quadrotor” Concept Paper Jan 9 1958 7 The Influence of Blade Flapping Restraint on Dynamic
Stability of Low Disk Loading Prepeller-Rotors by Maurice I. Young & Roman T. Lytwyn Boeing-Vertol
May 10-12 1967
8 AFFTC-TN-58-1 Flight Evaluation of Directional Stability and Control of Kaman K-600 with Various Empennage Configurations and Stability Augmentation
Feb 1958
9 Report No. NRL 4621 Velocity Tests of NRL Valve Pulsejet and Whirling Loss Evaluation
Nov 4 1955
10 Report No. R-585 The Aeroelastic Behavior of Rotary Wings in Forward Flight Final Report Volume I-Analysis Contract# Now 64-0488f Kaman
Undated
11 Chinook Crane – The Boeing Model 297 Heavy Lift Helicopter Brochure
Undated
12 New Control Criteria for VTOL Aircraft by Robert R. Lynn Bell
Aug 1962
13 Fuselage Vibration Prediction Boeing 1965 14 Performance Potential of Rotor Blade Inboard
Aerodynamic Devices by Maurice I. Young & Jaan Liiva Boeing
Jun 22-24 1966
15 Report No. 395 Stability and Control of Tandem Helicopters Phase III & IV Static and Dynamic Lateral Stability and Control Contract# Nonr-27024 Princeton Univ.
Jul 1957
16 Heavy Lift Helicopter Technology Assessment 1968 Lockheed-California
1968
17 Report No. FT23-4R-64 Military Research Evaluation of the Lockheed XH-51A Rigid Rotor Helicopter Final Report
Jan 7 1964
18 The Coming Revolution in Aeronautics with VTOL/RLS Presentation Bell
May 18 1966
19 FanJet Drive Systems for Heavy Lift Helicopters HTC Undated 20 Technology Background Fanjet Drive HLH Presentation May 8 1969 21 Proposed Areas for Rotorcraft Development Aircraft
Laboratory C.A. 1956
22 Summary of Parametric Studies for Flying Crane Helicopters
Aug 1957
23 Development of the Helicopter Brochure Lockheed-California
1966
24 Extending Helicopter Speed Performance Brochure Lockheed-California
C.A. 1967
25 Paper No. 782 Heavy Lift VTOL – Effect of Weight and Size on Productivity by J.E. Fuller & M.L. Marquis Sikorsky
May 5-8 1969
89
26 Garrett RPV Presentation Undated 27 Air Force Long Range R&D Program for Rotary Wing
Aircraft Presentation Apr 1954
28 Report on Helicopter Developments in Germany by R.H. Prewitt
May 1945
29 NAVWEPS 00-80T-88 (ATC Manual 51-2) Helicopter History and Aerodynamics Manual
1961
30 DAVI (Dynamic Antiresonant Vibrator Isolator) Brochure Kaman
Undated
31 Proposal No. 35-4 Unsolicited Proposal for the development of the Helicycle Vehicle by Peter R. Payne
Apr 12 1968
32 AFFTC-TR-60-2 Appendix III YHO-2HU Air Force Flight Evaluation
May 1960
33 Summary Report on New Family of VTOL Vehicles Brochure L.C. McCarty
Mar 1963
34 PB 121097 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Vol. 5 Weight and Balance
1954
35 PB 111390 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 6 Aerodynamics and Performance of Helicopters
1954
36 PB 111289 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 7 Vibrations Handbook for Helicopters
1954
37 PB 111521 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Vol. 10 Stability and Control of Rotary Wing Aircraft
1954
38 PB 111288 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 13 Convertible Aircraft
1954
39 PB 111391 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 14 The Rotary Wing Industry
1954
40 ASD TR No. 61-660 Investigation of Flexible Rotor Systems – Results of Phase I & II Contract# AF 33(616)7613
Sep 1961
41 WADC TR 55-408 Utilization of Helicopters as Army Fuel Tankers
Dec 1955
42 AHS Paper No. AHS-1 Helicopter Flight Research at NACA, Langley by Jack P. Reeder NACA
Dec 1951
43 AHS Paper Preliminary Development of a Trailing Rotor System by J.A. DeTore Bell
Nov 3-4 1965
44 AHS Paper No. 102 The helicopter Rotor at High Mach Speeds by W.H. Tanner & J.F. Van Wychhouse Bell and Patrick Cancro USAAMlabs and John McCloud, III NASA
May 10-12 1967
45 AHS Paper US Army Hueycobra Configuration and May 10-12 1967
90
Design Considerations by Charles M. Seibel Bell 46 AHS Paper No. 201 Status Report on Design Development
of the AH-56A Cheyenne by P.W. Theriault Lockheed-California
May 8-10 1968
47 AHS Paper No. 233 Experimental Flight Tests of the 300 MPH XH-51A Compound Helicopter by W.E. Spencer Lockheed-California
May 8-10 1968
48 AHS Paper No. 210 A Special Gas Turbine Cycle for the Compound Helicopter by J.B. Nichols United Technologies
May 8-10 1968
49 AHS Paper No. 216 Flight Investigation of the Wing-Rotor Lift-Sharing Characteristics of a Hingeless Rotor Compound Helicopter by Perry L. Deal & Julian L. Jenkins NASA Langley
May 8-10 1968
50 AHS Paper Flying Qualities Considerations in the Design and Development of the Hueycobra by C.L. Livingston & M.R. Murphy Bell
May 1968
51 Full Scale Wind Tunnel Test of a High Performance Helicopter Rotor Bell
Undated
52 SAE Paper No. 923C Aerodynamic Development of the OH-6A Helicopter for the Army by Kenneth B. Amer HTC
Oct 5-9 1964
53 AIAA Paper No. 93-4819 International Research in Rotorcraft Technologies by Alfred Gessow Univ. of Maryland
Dec 1-3 1993
54 Report No. R&M No. 1157 On the Horizontal Flight of a Helicopter
Mar 1928
55 Report No. F-IR-133-RE Helicopter Theory Interview with Dr. Kurt Hohenemser Concerning His Recent Contributions
Sep 1946
56 USAAVLABS TR 68-26 Preliminary Design Study of Convertible Fan/Shaft Engines Contract# DAAJ02-67-C0070
Apr 1968
57 USAAVLABS TR 69-50 Exploratory Study of the Nature of Helicopter Rotor Blade Boundary Layers Contract# DAAJ02-67-C-0001
Jul 1969
58 NACA TN 3238 Review of Information on Induced Flow of a Lifting Rotor
Jun 1954
59 NACA TN 3690 Normal Component of Induced Velocity in the Vicinity of a Lifting Rotor with a Nonuniform Dick Loading
Apr 1956
60 NACA TN 3691 Analysis and Comparison with Theory of Flow-Field Measurements Near a Lifting Rotor in the Langley Full-Scale Tunnel
Apr 1956
61 NACA TN 3900 Investigation of Vertical Drag and Periodic Airloads Acting on Flat Panels in a Rotor
Dec 1956
91
Slipstream 62 NASA TN D-43 An Evaluation of Linearized Vortex
Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect
Sep 1959
63 NASA TN D-112 Experimental Investigation of the Pressure Fluctuations on a Flat Plate and a Cylinder in the Slipstream of a Hovering Rotor
Sep 1959
64 Report No. FTD-MT-24-449-68 Aerodynamics of the MI4 Helicopter
1967
65 Rotor Blueprints SE 3000 Undated 66 Helicopters – Miscellaneous Articles, Photos and
Brochures Various
ROTORS, HOT CYCLE ROTORS, STABILITY 36 1 Report No. FDM No. 267 Results of Data Flights on the
XHO3S-2 – Helicopter Stability Investigation Contract# AF33(616)-2773 Cornell
Apr 8 1957
2 Report No. FDM No. 271 The Determination of Helicopter Longitudinal Stability Derivatives from Phase II Flight Test Data Contract#AF33(616)-3772 Cornell
Jul 3 1957
3 Simulation of the Heavily Damped Mode (Short Period Mode) of the XHO3S-2 Helicopter on the EASE Analog Computer Using Linearized Equations of Motion Contract# AF33(616)-5361 Cornell
Oct 24 1957
4 Report No. FDM No. 280 Analyses of a 30 MPH Helicopter Flight Transient on the EASE Analog Computer Cornell
Feb 27 1958
5 Report No. FDM No. 292 A Preliminary Study of Helicopter Lateral Stability and Control Contract# AF33(616)-6049 Cornell
Jan 5 1959
6 Report No. FDM No. 294 Methods for Extracting Helicopter Lateral Stability Derivatives from Transient and Steady-State Flight Data Cornell
Apr 20 1959
7 Report No. R-217 A Review of Theoretical and Experimental Investigations of the Rotor Aerodynamic Problem Contract NONR 2811 (00) Boeing-Vertol
Oct 1960
8 Report No. PR-508 Advanced Flight Research Program Boeing-Vertol
1964
9 Report No. HTC-AD-65-15 Volume II Summary TR – Rotor/Wing Concept Study Contract# Nonr-4588(00) HTC
Sep 1965
10 Report No. HTC-AD-65-15 Volume I Appendixes A, B, C, D, E, and F to Summary TR – Rotor/Wing Concept Study Contract# Nonr-4588(00) HTC.
Sep 1965
11 Reporty No. HTC-AD-66-9 Rotor/Wing Series V Wind Tunnel Test – 1/15-Scale Transonic Model HTC
Sep 1966
92
12 Hot Cycle Rotor/Wing Concept HTC Feb 15 1968 13 PB 111632 Rotary Wing Aircraft Handbooks and History
Volume 8 Mechanical Design and Description Contract# W33038-ac-21804 (20695)
C.A. 1954
14 PB 111632 Rotary Wing Aircraft Handbooks and History Volume 11 Special Types of Rotary Wing Aircraft Contract# W33038-ac-21804 (20695)
C.A. 1954
15 Dynamic Antiresonant Vibration Isolator Kaman Undated 16 Report No. R-145 A Study of Aerodynamic Interaction
Between Lifting Rotors and Components in the Rotor Wash Contract# AF33(616)-2981 Kaman
Jul 23 1956
17 Report No. MTI-67RD627 Proposal for Hybrid Boost Bearing Development Sikorsky
Aug 11 1967
18 Report No. MTI 68RD670 Proposal for WPAFB – Hydrostatic Boost Spherical Ball Bearing for Helicopter Rotor Blade Joint Application, Design, Development and Testing Mechanical Technology
Apr 8 1968
19 Report No. HF 68-1 Injury Experience in Army Helicopter Accidents by Kenneth L. Mattox, CPT, MC
C.A. 1968
20 Report No. WAC 103 Proposal for a Preliminary Design Study of a Squad Carrying Combat Utility Transport Wilford
Apr 1970
21 TRW Systems Evaluation of Helicopter Evacuation Rescue Outfit (HERO) Presentation
Undated
22 Report No. 55McC103R Full Scale Investigation of Rotor Hub Fairing for a Sikorsky H-5 Rotor Hub Contract# AF 18(600)-176
Apr 1955
23 Helicopter Research & Development Conference Papers Bell
May 16-17 1961
24 Items of Interest and Suggestions for Research by Robert R. Lynn Bell
May 15 1968
25 Bibliography of Rotary Wing Aircraft C.A. 1940 26 Report No. 1-64 US Army Helicopter Accidents Involving
Fire C.A. 1964
27 TCREC TR 62-103 Hot Cycle Rotor Duct Closure Valve System Contract# DA 44-177-TC-832
Mar 1963
28 USAAVLABS TR 65-29 Aircraft Design XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44-177-AMC-877(T)
Aug 1965
29 USAAVLABS TR 65-68 Component Testing XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44-177-AMC-877(T)
Nov 1965
30 USAAVLABS TR 65-68 Ground and XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44177-AMC-877(T)
Mar 1966
93
37 1 USAAVLABS TR 66-10 XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44-177-AMC877(T)
Jun 1966
2 USAAVLABS TR 66-81 20-Hour Follow-On Flight Test Program, XV-9A Hot Cycle Research Aircraft Contract# DA 44-177-AMC-225(T)
Dec 1966
3 USAAVLABS TR 67-1 Preliminary Design of a Rotor System for a Hot Cycle Heavy-Lift Helicopter Contract# DA 44-177-AMC-225(T) Task II
Mar 1967
4 USAAVLABS TR 67-9A In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume I Instrumentation and In-Flight Recording System Contract DA 44-177-AMC-124(T)
May 1967
5 USAAVLABS TR 67-9B In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume II Calibrations and Instrumented Component Testing
May 1967
6 USAAVLABS TR 67-9C In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume III Data Processing and Analysis System
Nov 1967
7 USAAVLABS TR 67-9D In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume IV Summary and Evaluation of Results
Nov 1967
8 USAAVLABS TR 67-9E In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume V Investigation of Blade Stall Conditions
Apr 1968
SERIES VI: Convertiplane, Autogiro, Composite Research Vehicle and Stowed Rotor, 1923-1999
Box File Description Date
CONVERTIPLANE 38 1 Report 3371 The Development of a V-Tab Controlled
Floating Horizontal Tail For Rotary Wing Aircraft Contract # AF33(600)-22222 McDonnell
Jan 8 1954
2 Report 3379 Full Scale Rotor Tests of the AF Feb 4 1954
94
Convertiplane Model XV-1 NACA Wind Tunnel, Moffett Field, CA Contract# AF33(616)-487 McDonnell
3 Report 3359 Characteristics of the Model XV-1 Convertiplane in Airplane and Autogiro Flight Conditions NACA Wind Tunnel, Moffett Field, CA Contract# AF33(600)-9392 McDonnell
Nov 1 1954
4 Report 2347 Model 82 Preliminary Performance Data Report Contract# AF33(038)-28075 McDonnell
Nov 12 1951
5 Model 82 Mockup Design and Specifications McDonnell Oct 17 1956 6 Report 3652 Model XV-1 Performance Data Report
Contract# AF33(600)-9392 McDonnell Mar 1 1955
7 Data Book For Helicopter Phase Tests on Model 82 Convertiplane
Sep 25 1952
8 Report 3652 Model XV-1 Performance Data Report Contract# AF33(600)-9392 McDonnell
Mar 1 1955
9 Report 3377 Design, Fabrication and Test of a Tail System Design of Model 82 Convertiplane Contract# AF33(600)22222 McDonnell
Dec 1 1953
10 Wind Tunnel Data Notebook 8/31 Scale Model 82 Convertiplane Massie Wind Tunnel Wright ADC
Dec. 1952-Jan. 1953
11 Report 1923 Aerodynamics Report Model 82 Dec 8 1950 12 Report 4459 XV-1 Drag Reduction Wind Tunnel Results
Contract# AF33(600)-9392 McDonnell Oct 31 1955
13 Wind Tunnel Investigation of the Aerodynamic Characteristics of an 8/31 Scale McDonnell Model 82 Convertiplane
Jan1954
14 Report 3386 Revision Dated 1 March 1956 Stability and Control Analysis of the McDonnell XV-1 Convertiplane Contract# AF33(600)-9392 McDonnell
Apr 6 1954
15 TN 54-2 Wind Tunnel Investigation of an 8/31 Scale McDonnell Model 82 Convertiplane in the Helicopter Flight Range
Jan1954
STOPPABLE/STOWED ROTOR/ CONVERTIPLANE
39 1 Ryan Stowed Rotor Aircraft Concept Article and drawings Jun 13 1968 2 LR 19755 VTOL Advanced Transport Aircraft Lockheed May 19 1966 3 Ryan VTOL Transport Potential 1975-1985 Undated 4 LTV The Promise of VTOL 1975-1985 Undated 5 Stoppable Rotor Aircraft Unidentified Appendices Undated 6 Hughes VTOL Briefing 1975-1985 Undated 7 Hughes Hot Cycle Rotor/Wing Undated 8 Performance of Advanced Heavy Lift Helicopters with Hot
Cycle Propulsion May 11-13 1966
9 Report SER-2600-23 Engineering Progress Report 23 Phase I of Development of Convertiplane Contract#
May 13 1953
95
AF33(038)-28076 Sikorsky 10 Report SER-2618 Aerodynamics Report S-57
Convertiplane Contract# AF33(038)-28076 Sikorsky Apr 21 1952
11 Report SER-2638 Substantiating Data for Standard Aircraft Characteristics and Performance Charts Contract# AF33(038)-28076 Sikorsky
Jul 2 1954
12 Report SER-2633 Detail Specification Model S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky
Jun 2 1954
13 Report SER-2634 Preliminary Analysis of Airloads for Sikorsky S-57 Airplane Configuration Contract# AF33(038)-28076 Sikorsky
Jun 24 1954
14 Report SER-2639 Preliminary Load Report S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky
Jul 2 1954
15 Sikorsky S-57 Convertiplane Engineering Drawings Contract# AF33(038)-28076 Sikorsky
1954
16 Report SER-2622 Estimated Weight and Performance Alternative Phase II Aircraft Contract# AF33(038)-28076 Sikorsky
Jun 20 1952
17 Report SER-2608 Detailed Calculation of Rotor-Wing Interference of S-57 for Vertical Climb and Hovering Contract# AF33(038)-28076 Sikorsky
Oct 11 1951
18 Report SER-2637 Preliminary Analytical Study of the Stability & Control of the Sikorsky S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky
Jul 2 1954
19 Report SER_2609 Performance of the S-57 Powered by a T-38 Allison Turbo-Prop Powerplant Contract# AF33(038)-28076 Sikorsky
Oct 9 1951
20 Report SER-2636 Preliminary Group Weight and Balance Statement Contract# AF(33)-028076 Sikorsky
Jun 8 1954
21 Report SER-2642 History of a Non-Retractable Rotor & a Retractable Landing Gear for the Model S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky
Jul 8 1954
22 HTC-AD 66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 2 – Performance Data HTC
May 1966
23 Report SER-50631 (Volume II) Stoppable Rotor Study – Wind Tunnel Plan Contract# F33615-69-C-1579 Sikorsky
Oct 15 1969
24 Wind Tunnel Investigations of a High Speed Stowed Rotor Aircraft
1968
25 Code Ident. No 81205 Stowed Rotor Aircraft Transport Parametric Study by Boeing-Vertol
1965
26 USAAVLABS TR 69-7 The Aerodynamic and Aeroelastic Characteristics of a Full-Scale Rotor Blade Stopped in Flight Contract# DA 44-177-AMC-366(T)
Apr 1969
27 Report R-598 Kaman Aircraft Model K-120 Composite Aircraft Kaman
Jul 30 1965 Rev Feb 7 1966
28 WSDS 68-18 Preliminary Weight and Performance May 1968
96
Analysis of AFFDL Transition Wing, Stopped Rotor Aircraft Concept
29 HTC-AD 65-15 Volume II Appendixes A, B, C, D, E, and F to Summary TR Rotor/Wing Concept Study Contract# Nonr-4588(00) HTC
Sep 1965
30 HTC-AD 65-15 Volume I Summary TR Rotor/Wing Concept Study HTC
Sep 1965
31 HTC-AD 66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 3 Propulsion System HTC
May 1966
STOWED ROTOR (LOCKHEED COMPOSITE RESEARCH VEHICLE)
40 1 LR 19539 Composite Research Aircraft Lockheed May 1966 2 LR 19534 Review Draft Preliminary Design Study and
Proposal For Full Scale Follow-On Program Volume 1 – Technical M-Statement of Work For Follow On Phase Contract# DA-44-177-AMC-372(T) Lockheed
May 1966
3 Report 16661 Wind Tunnel Investigation of a Hybrid Helicopter Dynamic Model Lockheed
Mar 25 1963
4 Report 17865 Experimental Investigation of Rotor Model Stop/Start in Forward Flight Lockheed
Jun 2 1964
5 USAAVLABS TR 68-40 Stopped-Stowed Rotor Composite Research Aircraft
Jan 1969
6 LR 19538 Trade-Off Analysis for Stowed Rotor Concept Lockheed
May 1966
7 LR 19535 Review Draft Preliminary Design Study and Proposal for Full-Scale Follow-On Program Volume 1 – Technical N-Plan of Performance for Full Scale Follow-On Contract# DA-44-177-AMC-372(T) Lockheed
May 1966
8 LR 21793 Selected Bibliography Lockheed Undated 9 LR 19522 Review Draft Preliminary Design Study and
Proposal For Full-Scale Follow-On Program Volume 1Technical A- Design Concept Contract# DA-44-177AMC-372(T) Lockheed
May 1966
10 LR 19523 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical B-Performance Data Contract# DA 44-177AMC-372(T) Lockheed
May 1966
11 LR 19540 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume II Management Contract# DA 44-177-AMC-372(T) Lockheed
May 1966
12 LR 19541 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume III
May 1966
97
Cost Contract# DA-44-177-AMC-372(T) Lockheed 13 LR 19524 Review Draft Preliminary Design Study and
Proposal For Full-Scale Follow-On Program Volume 1Technical C Propulsion Data Contract# DA 44-177-AMC372(T) Lockheed
May 1966
14 LR 19525 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical D-Weight and Balance Contract# DA 44-177AMC-273(T) Lockheed
May 1966
15 LR 19526 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical E-Stability, Control and Flying Qualities Contract# DA 44-177-AMC-372(T) Lockheed
May 1966
16 LR 19528 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical G-Electrical, Hydraulic and Mechanical Systems Contract# DA 44-177-AMC-372(T) Lockheed
May 1966
17 LR 19536 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical O-Test Plans for Full-Scale Follow-On Contract# DA 44-177-AMC-372(T) Lockheed
May 1966
18 LR 19537 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical P-Draft Specification Contract# DA 44-177AMC-372(T) Lockheed
May 1966
19 LR 19529 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical H-Emergency Systems and Procedures Contract# DA 44-177-AMC-372(T) Lockheed
May 1966
20 LR 19530 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical I-Cockpit Arrangement Contract# DA 44-177AMC-372(T) Lockheed
May 1966
21 LR 19531 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1Technical J-Drawings Contract# DA 44-177-AMC-372(T)
May 1966
CONVERTIPLANE / COMPOSITE RESEARCH AIRCRAFT
41 1 RDM Convertiplane and Engine Jun 1951 2 Report 2R90-10 Quarterly Report Contract# AF33(616)
3647 Transcendental Aircraft Corp. Task 449L Project R56-662-TC
Sep 15 1956
3 Bell XV-3 Articles, Pictures and Summary Feb 10 1955 4 Report 301-199-001 V/STOL Tilt Rotor Research Aircraft
Volume 1 Performance and Noise Analysis Contract# Jan 1973
98
NAS2-7260 Bell 5 Report 200-094-233 Determination of Stability Derivatives
for Two Center of Gravity Locations from Wind Tunnel Tests of Bell Model 200 (XH-33) Bell Convertiplane
May 23 1955
6 Report200-099-703 Dynamic Stability Analysis for the XV-3 Convertiplane Bell
Sep 1 1955
7 Bell Helicopter Brochure Model 301 Tilt Rotor Aircraft Bell
Dec 1973
8 Report 200-102-100 Aerodynamic and Performance Data for the XV-3 Convertiplane Bell
Mar 11 1954
9 Report 200-094-232 Wind Tunnel Investigation of Airplane Flight Characteristics of the Bell Model 200 Convertiplane Volume 1 Analysis and Discussion of Results Bell
Oct 12 1953
10 Report 200-094-238 Wind Tunnel Investigation of Lateral – Directional Stability of the XV-3 Convertiplane Bell
Feb 1 1955
11 Bell XV-3 Convertiplane Photos and Articles for Contract# AF33(600) 20777
1954
12 Report AR-B103 Preliminary Stability and Control Analysis of the Model B Convertiplane Convertawings, Inc.
Dec 7 1950
13 Quarterly Progress Report (15 Sept. 56 – 15 Dec. 56) Transcendental Aircraft Corp. Task No. 449L, Project No. R-56-662-TC Contract# AF33(616)-3647
Jan 15 1957
14 Transcendental Aircraft Corp. Interim Progress Report Contract# AF33(616)-3647
Oct 31 1956
15 Report D26-099-101 Composite Research Aircraft Design Study – Design Concept- Contract# DA 44-177-AMC373(T) Bell
May 1966
16 Report D26-099-102 Composite Research Aircraft Design Study – Performance Data- Contract# DA 44-177-AMC373(T) Bell
Undated (probably May 1966)
17 Report D26-099-103 Composite Research Aircraft Design Study – Stability, Control and Flying Qualities - Contract# DA 44-177-AMC-373(T) Bell
May 1966
18 Report D26-099-105 Composite Research Aircraft Design Study – Propulsion Data- Contract# DA 44-177-AMC373(T)
May 1966
19 Report D26-099-107 Composite Research Aircraft Design Study – Emergency Systems and Procedures- Contract# DA 44-177-AMC-373(T) Bell
May 1966
20 Report D26-099-111 Composite Research Aircraft Design Study – Detail Specification (Draft) - Contract# DA 44177-AMC-373(T) Bell
May 1966
21 Report D26-266-101 Composite Research Aircraft Design May 1966
99
Study – Results of Model Test- Contract# DA 44-177AMC-373(T) Bell
22 Tilt Rotor Composite Aircraft Articles May 1971 23 Bell Helicopter Proprotor VTOL Technology Program Mar 16 1970 24 Bell TiltRotor Photos and Vugraphs 1966 25 The Rheem-Platt Vertical Take-Off Airplane Aerodynamic
Analysis Sep 16 1947
26 Northrup Norair Division Article – About the Application of Low Drag Boundary Layer Suction to Tilt Rotor Propeller Blades During Cruising
Apr 1967
27 Bell Article – An Analysis of Low-Disc-Loading VTOL Aircraft Types
Jan 10-13 1966
STOPPABLE/STOWED ROTOR/ CONVERTIPLANE 42 1 Report SER-50621 Stoppable Rotor Study Phase I – Final
Report Sikorsky Oct 1 1969
2 AFFDL-TR-71-62 Volume 1 Design Studies and Model Tests of the Stowed Tilt Rotor Concept
Jul 1971
3 AFFDL-TR-72-81 Summary of Design Studies and Results of Model Tests of the Folding-Prorotor Aircraft Concept
Jul 1972
4 USAAVLABS TN 70-28 Convertible Fan/Shaft Engine Variable Fan Geometry Investigation Contract# DAAJO269-C-0002
Apr 1970
5 Summary of Mission Design Studies for Folding Tilt Rotor Aircraft Boeing-Vertol
Jun 3 1969
6 Horizontal/Stoppable Rotor Articles and Concept Photos 1969 7 AHS 27th Annual National V/STOL Forum– Horizontal
Stoppable Rotor Conversion by George A. Watts & James C. Biggers Lockheed & NASA Ames
May 1971
8 Report D270-099-001 Design Studies of Folding-Prorotor VTOL Aircraft Bell
Oct 1969
9 R&D Interim Report of Phase I – Design Studies and Model tests of the Stowed Tilt Rotor Concept – Volume I. Parametric Design Studies
Sep 1969
10 Report 2D-3210-1 Summary Report Helicopter Model 2D Gyrodyne
Jul 1953
11 Report 2C-3336-2 Performance Demonstration Report Model 2C Contract# NOas 51-1217-f Gyrodyne.
Sep 26 1952
12 Report 2C-3336-3 Flying Qualities Demonstration Report Model 2C Contract# NOas 51-1217-f Gyrodyne
Oct 15 1952
13 Report 2C-3336-5 Spoiler Evaluation Report Model 2C Contract# NOas 51-1217-f Gyrodyne
Dec 12 1952
14 Report 2C-3336-6 Supplementary Flying Qualities Report Model 2C Contract# NOas 51-1217-f Gyrodyne.
Dec 26 1952
15 Report 2C-3336-7 Directional Control Tests with Blade Tip Air Brakes Contract# NOas 51-1217-f Gyrodyne
Apr 14 1953
100
16 Report 2C-3336-8 Summary Report Model 2C Flight test Results Contract# NOas 51-1217-f Gyrodyne
May 11 1953
17 Report 102X90-4 An Investigation of the Handling Qualities of a Tandem Rotor Helicopter (H-21) Equipped with a Gyroscopic Stabilizing System Contract# NOas 56796-c Kellett
Aug 1 1958
18 US Army TRC Preliminary Flight Test Data UH-1B High Performance Helicopter with Auxiliary Propulsion
Feb 1964
19 US Army TRC Preliminary Flight Test Data XH-51A Rigid Rotor High Speed Flight Program Interim Report No. 4
Oct 1964
20 Operational History and Experience with Boeing Helicopters by Howard N. Stuverude
Nov 14-16 1967
21 NASA TN D-4195 A Numerical Method for Studying the Transient Blade Motions of a Rotor with Flapping and Lead-Lag Degrees of Freedom
Oct 1967
22 Report FT-13R-66 Monitor of the Development of Helicopter and VTOL Research Programs; Third Interim Report
Dec 13-17 1965
23 Development of a Piloted, Real Time, Hybrid Simulation of the X-22A V/STOL Aircraft by William G. Cockayne Bell
Undated
24 Report 2127-950006 Flight Test Summary Report X-22 Aircraft No. 1 (BuNo 151520)
Sep 19 1966
43 1 KELLETT DRAWINGS
STOPPABLE & STOWED ROTOR 44 1 Stoppable Rotor Program – Briefings and Slides Nov 1969
2 Stoppable Rotor Program – Reports and Analysis with Handwritten Notes
C.A. 1969
3 Stoppable Rotor Program – Phase I Briefing Contract#F33615-69-C-1578 (6 sections and photo) Bell
Oct 30 1969
4 Folding Proprotor Program Briefing Contract# NAS 25461 Bell
Jan 15 1970
5 Proprotor Landing Gear Memo Bell Jan 7 1970 6 Design Criteria for Folding Tilt Rotor Aircraft Contract#
F-33625-69-C-1577 Boeing Vertol Oct 1969
7 Report DRC-268 Downwash Environment for the Boeing Model 160 V/STOL Aircraft Dynasciences
Jan 1968
8 Stoppable Rotor Program – 1) Feb 1968 Calender; 2) VTOL Aircraft Chart; 3) Operational and Summary Evaluation Matrixes; 4) Lindenbaum Notebook
Feb 1968
9 Proposal For Analytical and Experimental Study of a New VTOL Concept VRC.
Jul 5 1960
10 Convertible Aircraft – Article, Sketches and Photo Jan 1953
101
11 Wing Rotor Configuration Research Plan Oct 23 1967 12 Stoppable Rotor Program – Concept Assessment Report Jan 2 1968 13 Stoppable Rotor Program – NAA Meeting Report Jan 22 1968 14 Report D-213-100000-2 R&D Interim Report of Phase I –
Design Studies and Model Tests of the Stowed Tilt Rotor Concept Volume III Appendixes Contract#F33615-69-C1577 Boeing
Sep 1969
15 Report D-213-100000-3 R&D Interim Report of Phase I – Design Studies and Model Tests of the Stowed Tilt Rotor Concept Volume II Component Design Studies Contract#F33615-69-C-1577 Boeing
Sep 1969
16 Report D-213-100001-1 R&D Interim Report of Phase II – Design Studies and Model Tests of the Stowed Tilt Rotor Concept Contract#F33615-69-C-1577 Boeing
Sep 1969
17 The Helijet Lateral Twin Folding Rotor V/STOL Aircraft Boeing Vertol
Feb 15 1968
STOWED/STOPPABLE ROTOR 45 1 Report SEP 6229 Stowed Rotor V/STOL Program
Planning Proposal SPB 64-AF9063-US Sikorsky Mar 23 1964
2 Report SEP-6260 Stowed Rotor V/STOL Flight Program Proposal SPB 64-AF1854-US Sikorsky
Oct 30 1964
3 Circulation Control Rotor Program for Advanced Technology Navy/Marine Helicopters
Undated
4 Stowed Rotor Helicopter Program Blueprint and Partial Document Sikorsky
C.A. 1964
5 Stoppable Rotor – Miscellaneous C.A. 1964-1965 6 Stoppable Rotor – Study Plan & Briefings Oct 10 1967 7 NASA Literature Search No. 5331 Stoppable Rotor
Aircraft Dec 1 1967
8 IAS Paper No. 62-62 The Hot Cycle Jet Rotor for Economical VTOL Aircraft by Malcolm Harned HTC
Jan 22-24 1962
9 Bell Stoppable Rotor Nov 3-4 1965 10 Stowable Rotor V/STOL Sikorsky Jan 20 1964 11 Application of Circulation Control Rotor Technology to a
Stopped Rotor Aircraft Design by Robert M. Williams Sep 22-24 1975
12 Proposal for the Development of a Vertical Take-Off and Landing Aircraft Prewitt Plastics Co.
Apr 4 1961
13 Report D2064-953001 Tri Service VTOL Transport – Proposal Summary Vol I Part I Bell/Lockheed
Apr 1961
14 Vertol Stoppable Rotor C.A. 1967 15 Berguet 941 VTOL Transport – Detail Specification
Summary Report for Tri-Service VTOL Prototype Aircraft Apr 9 1961
16 Sikorsky Stowed Rotor – Blueprints and Sketches C.A. 1964 17 Conversion of Berguet’s STOLs to VTOLs by Harlan D.
Fowler with Additional Calculations Oct 10 1960
102
18 Report ARD-211 VTOL Amphibious Assault Transport Systems 1962-1967 Phase III Summary report Hiller
Apr 15 1959
19 59RDZ-34581 Grumman Report to the Perkins Committee 1959 20 Stoppable Rotor Program – Pictures, Negatives and
Overhead Projection Slides Various
21 The Future of Vertical Take-Off and Landing Aircraft by Philip L. Michel Sikorsky
Oct 1967
22 Research and Development by Philip L. Michel Sikorsky Jan 1963 23 Stoppable Rotor Concepts and Descriptions Used in
CARA Evaluation Undated
24 Photos Undated 25 V/STOL Photographs
(See also Location 50, File 3 for drawings/prints of various V/STOL Aircraft & Helicopters – mounted on cardboard)
Undated
26 Legal Aspects of Planning for Urban Heliports by L. Welch Pogue & George C. Neal Virginia Law Review Vol. 46, No. 1
1960
27 NASA TN D-814 Nomographic Solution of the Momentum Equation for VTOL-STOL Aircraft
Apr 1961
28 NASA TN D-5819 Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floors
Jun 1970
29 AERO Report 954 Comparison of Experimental and Theoretical Design Parameters of a 6 Inch Diameter Annular Jet Model with a Jet Angle of -45o Hovering in Proximity to the Ground: and Experimental Results for Forward Flight at Zero Angle of Attack
May 1959
30 NACA RM L53A09 Langley Full Scale Tunnel Tests of the Custer Channel Wing Airplane (Cover missing)
Undated
31 Report 16-A-3 The Ring Tail as a Stabilizer and Control Device Piasecki
Aug 26 1960
32 Report 2-Y-4 Ring-Wing V/STOL Logistics Aircraft Piasecki
Feb 25 1960
33 V/STOL Logistic Aircraft Blueprints by Harlan D. Fowler C. A. 1960
34 SAE 266G Mass Transportation by High-Speed VTOL by H.V. Borst & J.M. Mergen Curtiss
Jan 9-13 1961
35 V/STOL Logistics Aircraft ARDC SR. No. 175 by Harlan D. Fowler
Jan 28 1960
36 Report 60-6 New Transport Aircraft 1965-1970 Time period Hiller
Feb 1960
37 Report 59RDZ-15303 Program Planning Report Pre-Phase 1 Part 1 and Part 2 – Development Program VTOL Supersonic Aircraft Contract# AF33(600)-39722 AVRO
Jun 1959
38 Report ZP-258 Preliminary Study Comparative Characteristics of Tilt-Wing, Ducted Propeller & G.E. Lift-
May 20 1959
103
Fan Military transport Type Aircraft With Combined VTOL & STOL Capability Convair
39 AIAA Paper 69-198 The Outlook for Future Commercial VTOL Transportation by Robert W. Simpson MIT
Feb 17-19 1969
40 Report D8-2357-8 Light Tactical Transport Aircraft System (LTTAS) Final Report Volume VIII Boeing
Jul 1969
41 SAE 650807 V/STOL Transport Aircraft for Air Cargo Operations by G.B. Pearson LTV
Oct 4-8 1965
SAE 660335 Vertical Flight in Common Carrier Transportation by Robert L. Cummings NYAirways
Apr 25-28 1966
42 SAE 700809 Planning the Evolution of V/STOL Powerplants by A.G. Newton & S.C. Miller Rolls-Royce Ltd.
Oct 5-9 1970
43 AIAA Paper 71-1015 STOL, VTOL, and V/STOL – Where Do They Fit In?
Oct 25-28 1971
44 NASC Report 3032-72-02 A Suggested Way for Comparing VTOL Configurations
May 1972
45 FDV 10-7-34 V/STOL Low Disc Loading Technology Oct 11 1967 46 Survey Paper on the Application of Technology to the
Flight Mechanics of Aircraft Development by Lawrence P. Green, Clem C. Weissman & Jack D. Brewer
Sep 13 1967
47 AIAA Paper 67-711 Study of Aircraft in Short-Haul Transportation Systems for 1985 by Donald W. Hayward Boeing
Oct 23-27 1967
48 Study of Aircraft in Short-Haul Transportation Systems Contract# NAS2-3862
1967
49 VTOL Aircraft Concepts and Development by B. Lindenbaum
Apr 8 1965
50 Observations on Subsonic V/STOL Aircraft Designs for USAF by Bernard Lindenbaum
Jun 30 1960
51 SOR-210 Mar 1964 52 AGARD Flight Mechanics Panel Symposium on “Military
Applications of V/STOL Aircraft” TRIP REPORT by Major Robert M. Bowman USAF
Dec 27 1972
53 SAWE Paper 842 A Merit Factor Suitable for Evaluation of a Variety of Aircraft Types and Missions by Gavid F. Gebhard Grumman
May 4-6 1970
54 Evaluation of V/STOL Vehicles for Flight Control Research Flight Testing USAF Flight Dynamics Lab
Aug 1965
55 The Economics of VTOL Systems Apr 29 1966 56 FSTC-HT-23-1062-70 Battle Zone Transports of the
Future (Germany) Jan 1970
57 VTOL Negatives and Articles 1967 58 Sikorsky Stowed Rotor Fighter Undated 59 Stoppable Rotor – Photos, Slides, Miscellaneous Undated
104
XF5U AIRCRAFT 46 1 XF5U-1 Illustrated Assembly Breakdown Undated
2 References for Information on Sikorsky V-173 and Vought XF5U-1 Aircraft
Various
3 The Development of the Chance Vought Model XF5U-1 Airplane Contract NOa(s)270
May 11 1948
4 Air Classics Magazine with Article on ZF5U-1 (pg 16) Aug 1975 5 Recommended Circular Wing Design Study Jan 10 1973 6 Articles Concerning Circular Wing Model Aircraft Various 7 XF5U-1 Pilot’s Handbook Undated 8 Log of Flights & Pilot’s Daily Flight Progress(unreadable) Undated 9 NACA Research Memorandum RM L9C29 Preliminary
Full-Scale Investigation of a 1/3 Scale Model of a Convertible-Type Airplane
Jun 7 1949
10 Report 4876 (unreadable) Undated 11 XF5U-1 Handwritten notes and memos 1972-1973 12 Report 5711 (unreadable) Mar 28 1945 13 AFFDL TM 72-3-PTB Conceptual Study of a Low Aspect
Ratio Wing Design for a Close Air Support Mission Nov 2 1972
14 NACA Research Memorandum RM L9C24 Static Longitudinal Stability and Control of a Convertible-Type Airplane as Affected by Articulated and Rigid-Propeller Operation
Nov 7 1949
15 XF5U-1 Photos Undated 16 XF5U-1 Articles and Diagrams 1972
AUTOGIRO/CONVERTIPLANE 47 1 Rotorcraft/Contractor/Contract# Cross Reference Aug 28 1951
2 Roadable Autogiro by B. Lindenbaum and Supporting Documents
Nov 1971
3 Illustrations for Roadable Autogiro Report Nov 1971 4 Elementary Aerodynamics of Compound Rotorcraft by
W.Z. Stepniewski & R. Bumstead Piasecki Undated
5 Report No. SER-2000 Determination of Parasite Drag from Wind Tunnel and Flight Test Data Sikorsky
Sep 9 1949
6 Turbine Powered Aircraft (Alouette II) General description Advanced Copy Republic Aviation Corp.
Mar 2 1959
7 Rotodyne Brochure Kaman Aircraft Undated 8 Compound Helicopters – Clippings and Photos Various 9 Sikorsky S-65-200 Compound V/STOL Brochure Undated 10 Sikorsky S-61 Brochure Undated 11 Sikorsky H-39 Experimental Brochure Undated 12 Report No. 1921 Model Specification for McDonnell
Model 82 Convertiplane Stripped Version Contract# Dec 8 1950
105
AF33(600)-9392 13 Piasecki Aircraft Corp. Brochure Undated 14 Towing with the Vertol 44 Brochure Undated 15 The Case for the Tandem Helicpoter by Z.M. Ciokosz &
W.Z. Stepniewski Piasecki Helicopter Corp. Dec 17 1954
16 Report No. 255-X-3 Proposal for Air to Air Launch and Retrieval System Piasecki Aircraft Corp.
May 13 1972
17 Helicopter Photos (Early Years) Undated 18 AIAA 1999-01-5644 Advanced Flying Automobile LS1
Engine by Mike Czajkowski Oct 19-21 1999
19 AIAA 1999-01-5625 Starcar on the Road by Steven C. Crow
Oct 19-21 1999
20 Roadable Aircraft From Wheels to Wings by Palmer Stiles Copyrighted
1994
21 Report No. R-550 HH-43F “Huskie” Brochure Aug 1964 22 AN 01-260HBA-1 Flight Handbook for Navy Model
HOK-1 Helicopters Apr 15 1955 Rev. Feb 1 1956
23 Report No. 47-980-004 Model 47 tail Rotor Test Technical Data Bell
Aug 13 1947
24 Sikorsky Current Production Models Brochure Mar 1971 25 Report No. SD-466-2 Detail Specification for Model
HO4S-2 Helicopter Class HO Single Engine Contract NOas 51-220
Feb 13 1951
26 ER No. 62-73 Model Ten99A as a Missile Site Support Helicopter Hiller Aircraft Corp.
Aug 1962
27 AFFTC-TN-60-8 Performance Evaluation of the Djinn Helicopter
Feb 12 1960
28 Hiller Camel (Civil Version) Brochure Undated 29 WADC TR 55-437 Part II An Investigation of the
Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Part II. Flight Test Evaluation of the Optimum Stabilization System
Mar 1959
30 WADC TR 55-438 Part II The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part II. Analyses of Flight Data and Extraction of Basic Stability Derivatives
Mar 1959
31 WADC TR 55-438 Part III The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part III. An Analog Computer Study of Flight Measured Longitudinally Transient Motion of a Single Rotor Helicopter
Sep 1959
32 WADC TR 57-583 Part III Helicopter Configuration and Propulsion Systems Study Part III. Aerodynamic Analysis
Nov 1957
106
33 WADC TR 57-583 Part IV Helicopter Configuration and Propulsion Systems Study Part IV. Analytical Procedure for Predicting Rotor Weight
Nov 1957
34 Report No. 48-980-003 YH-12B High Tip Speed Flight Test Evaluation Contract# AF 33(600)-6473
Nov 17 1954
35 Report No. SER-126 Flight Test measurements of the Stresses and Relative Motions of the Main Rotor Blades Contract# DA W535 ac-2514 and ac-29845 Sikorsky
Dec 15 1944
36 WADC TR 55-438 Part I The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part I. Development of Flight Test Instrumentation, Techniques and Analysis Methods
Feb 1958
37 Report No. ARD 134 Quick Starting of Ramjet Powered Helicopter Rotor Hiller Helicopters
Feb 20 1957
38 Report No. SER-538 Performance – Tail Rotor Sikorsky Oct 9 1944 39 ER No. J1-040-1 Discussion of Proposal and General
Description of Model 38 Jet Powered Helicopter McDonnell
Feb 13 1946
40 Report No. 1572 Progress Report No. 41 – Month of January 1950 – Rotor-Helicopter, Jet-Propelled, with Flyable test stand Contract# AF33(038)-9845 McDonnell
Feb 15 1950
41 Report No. 1576 Preliminary Design Data – High Tip Speed Ram Jet Rotor Contract# AF33(038)-9845 McDonnell
Feb 22 1950
42 Report No. ATD-TTH-Y24 The Gates Twinjet Helicopter Technical Information Bulletin Gates Learjet
Jul 1 1970
43 USAAMRDL TR 72-44 Fan-In-Fin Antitorque Concept Study Contract# DAAJ02-71-C-0060
Jul 1972
44 Huey Tug Brochure Bell Undated 45 ER No. 60-5 A Parametric Study of the USArmy New
Light Observation Aircraft 1965-1970 Time Frame. Hiller Feb 1960
46 Report No. 46-947-001 Proposed Model Specification for Single Engine-Two Bladed Helicopter Bell
Aug 10 1945 Rev Sep 10 1945
47 Report No. 47-947-015 Specification for Helicopter – Two Place – Single Engine – Two Bladed Contract# AF 33(038)15940
Sep 15 1951
48 Miscellaneous Papers and Articles Various
CONVERTIPLANE/COMPOUND HELICOPTER 48 1 Report No. 16-X-12 Model 16H Helicopter Overview
Piasecki C.A. 1962
2 Report 16-X-12D Military Applications of 16H V/STOL Aircraft Piasecki
May 28 1962
3 Report 16-X-12DE Piasecki 16H Compound V/STOL Jun 15 1962
107
Aircraft Piasecki. 4 Report 16-X-15a Fiscal Proposal 16H-1 Test and
Evaluation Program Piasecki May 12 1962
5 Report 16-X-17 Cost Effectiveness and Comparisons Piasecki
May 1 1962
6 Report 16-X-18 Proposal For Test Evaluation of a Compound Helicopter Configuration Piasecki
May 15 1962
7 Report 16-X-13 Proposal For Test Evaluation of a Compound Helicopter Configuration Piasecki
Mar 14 1962
8 Report SER-2551 Long Range Helicopter Method of Analysis – Compound Helicopter Configuration Sikorsky
Feb 18 1955
9 Report SER-2555 Long Range Helicopter Design Study Contract# AF33(616)-2628 Sikorsky
May 23 1955
10 Report SER-2556 Summary Report Long Range Helicopter Method of Analysis – Pure Helicopter Configuration Contract# AF33(616)-2628 Sikorsky
May 27 1955
11 Report SER-611344 Final Report NH-3A (Sikorsky S-61F) Flight Test Program Contract# Now-64-0528-f
Mar 20 1969
12 FSTC-HT-23-1554-72 New Technology of Fast Italian Helicopters
Mar 14 1973
13 USAAVLABS TR 71-2 High Mach Number/High Advance Ratio Flight Test Program with the High-Performance UH-1 Compound Helicopter Contract# DA 44-177-AMC-364(T)
Feb 1971
14 USAAVLABS TR 67-18 Rotor Blade Loads, Blade Motion, and Stress Caused by Transient Inputs of Shaft Torque as Related to Stoppable Rotor Operations Contract# DA-44-177-AMC-77(T)
May 1967
15 USAAVLABS TR 67-58 16H-1A Flight Test Research Program Contract# DA-44-177-AMC-154(T)
Aug 1968
16 WADC TR 53-125 Wind-Tunnel Investigation to Determine the Critical Advance Ratio of the 8/31-Scale McDonnell Model 82 Convertiplane Rotor
Apr 1953
17 WCLS TN 54-29 Tests on a 1/6-Scale Jacobs 104 Convertiplane Model in WADC Five-Foot Wind Tunnel
Apr 1954
18 The Generalized Actuator Disk by G.R. Hough & D.E. Ordway
Mar 5-6 1964
19 The Promise of Compounding by Jan M. Drees & Robert R. Lynn Bell
Jan 13-16 1966
20 Report No. 3447 Airplane Tow of the XV-1 for Long Range Rescue Missions Contract# AF33(600)-9392
Feb 24 1954
21 Tables for Computing the Instantaneous Velocities Induced at the Blade Axes of a Lifting Rotor in Forward Flight by the Skewed Wake Helical Wake Vortices and a Method for Calculating the Resultant Blade Air Loads Contract# Nonr 991(05) Georgia Tech
Jun 1962
108
22 AFFTC-TR-56-35 ARDC XV-1 Phase II Flight Evaluation Feb 1957 23 TR 107-1 Programs for Machine Computation of Rotor
Blade Downwash Contract# Now 62-0100-d MIT Aug 1964
24 Report No. R 242 Fundamentals of Helicopter Stability and Control Contract# Now 60-0469-f Boeing Vertol
Feb 1961
25 Report No. 8011-099-002 The Weight of Very Large Rotors for Nuclear Powered Helicopters Bell
Apr 23 1959
26 Report No. BB-1187-H-1 Improvement of Ferrying Range of Army Helicopters Contact# DA-44-177-TC-441 Cornell
Jan 1958
27 Report No. R-240 General Management Proposal for a Medium Transport Helicopter 58MCXS-13805
Aug 15 1958
28 Army Study Requirement 3-60 The Kaman Rotodyne Undated 29 Report 104-A-01 Performance Analysis of Jacobs 104
Helicopter Undated
30 Report D-114 A Review of the Convertiplane Development Program Jacobs Aircraft Engine Co.
Apr 22 1955
31 Report 3294 McDonnell V-1 Convertiplane Contract# AF33(038)-28075
Oct 26 1953
32 Report No. 1901 McDonnell Model 78 Assault Transport Helicopter
Dec 20 1950
33 Report No. 6248 Model 113P Medium Transport Compound Helicopter 58MCXS- 13806
Aug 18 1958
34 Report No. 3371 The Development of a V-Tab Controlled Floating Horizontal Tail for Rotary-Fixed Wing Aircraft Contract# AF33(600)-22222
Jan 8 1954
35 Report No. 2230 An Estimate of Propeller Effects on Static Longitudinal Stability of Model 82 Convertiplane Contract# AF33(038)-28075
Aug 21 1951
36 Miscellaneous Articles Various
AUTOGIROS – PRE WWII 49 1 Autogiros, Pre-World War II – Photos and Clippings Pre 1941
2 Aurogyio Photos Various
3 R&M No. 885 Some Experiments on Airscrews at Zero Torque, with Applications to a Helicopter Descending with Engine “Off”, and to the Design of Windmills by C.N.H. Lock
Sep 1923
4 R&M No. 1162 A Summary of the Experimental and Theoretical Investigations of the Characteristics of an Autogiro by H. Glauett & C.N.H. Lock
Apr 1928
5 Autogiro – Articles Various 6 Model 18-A Gyroplane – Weldon F. Stump and Co. Undated 7 Report No. ER-200 & ER-201 Report on Tests to
Determine Friction in Jump-Off Mechanism(ER200) and Feb 26 1938 Mar 10 1938
109
PA-36(ER201) Autogiro Co. of America 8 Report No. ER-130.4 Possibilities of “Jump-Off” Giro
Utilizing Optimum Blade Incidence Angles Kellett Feb 1935
9 Hafner AR-3 Gyroplane 1937 10 Cievra C-30 Autogiro 1928 11 Air Ministry reports and Memoranda Concerning
Autogiros No. 1108(Aug 1926); No. 1111(Nov 1926); No. 1127(Mar 1927): No. 1131(Jul 1927); No. 239.Vol.XXXIV(Nov 1930)
1926-1930
12 The Direct Control Autogiro Autogiro Co. of America Undated 13 Journal of The Franklin Institute Feb 1939
Mar 1939 14 The Aircraft Yearbook by Aeronautical Chamber of
Commerce – Volume 16, 17 and 24 1934, 1935, 1942
15 The Autogiro – Second Complete Authoritative Presentation Autogiro Co. of America
Undated
16 Copy of Brochure “What the Autogiro Co. of America Offers”
Undated
17 NACA No. 205 The Hafner A.R. III Gyroplane (British) Apr 1937 18 Testimony Before the Committee on Military Affairs of the
House of Representatives by Harold F. Pitcairn Autogiro Co. of America
Apr 26 1938
19 Recent Air Corps Developments in Rotating Wing Aircraft by H.F. Gregory
Jan 29 1941
20 Comparison of Flying machines by Juan de la Cievra Feb 1934 21 Kellett YG-1 Autogiro 1935 22 Kellett YG-1/KD-1 Autogiro Correspondence Various 23 Kellett XO-60 Autogiro 1943 24 TCTC 2175 Meeting 112 Military Characteristics for
Airplane, Observation, Light Oct 17 1957
25 Autogiro Mail Service, Philadelphia, PA Oct 2 1940 26 Serial No. 3445 Air Corps TR on Performance Estimates
of Autogiro Equivalents of the XO-27A Observation Airplane
Apr 29 1931
27 No. 98-800 Autogiro, Observation Type Specification for Jul 10 1935 28 Report No. 150.1 Resonance in Rotating Wing Aircraft and
Associated Article Aug 19 1942
29 Report No. 541 Service Test Requirements for Kellett YG1 Autogiro
May 6 1936
30 Kellett YG-1 Autogiro – Additional Documents Various 31 Report ER-060.2 Comparative Performance of Airplane,
Aurigiro and Theoretical Helicopter Kellett Mar 1940
32 Possibilities of the Jump-Off Autogiro by R.H. Prewitt Kellett
Jan 25 1938
33 NACA AR257 Photographic Observations of Blade Motion of the YG-1B Autogiro Equipped with Tapered
May 9 1940
110
Rotor Blades 34 PA-36 Blueprints 1938 35 Report ER-192 Study of Effects of using3 Tilt in Hub of
PA-36 Autogiro Autogiro Co. of America Nov 1 1937
36 Report ER-194 Best Combination of Angles on Centralized Hubs Autogiro Co. of America
Nov 10 1937
37 Report ER-195 Study of Effect of Fairing Autogiro Rotor Hubs and Tapering Blades in Plan-Form Autogiro Co. of America
Nov 11 1937
38 Report ER-202 Study of Probable Performance of Modified PA-33 Autogiro Autogiro Co. of America
Jun 28 1938
39 AF Flight Dynamics Lab Reply to Chief, Patents Division, HQUSAF (AF/JACP) and Associated Documentation
Nov 21 1972
40 Copies of Patents Related to Autigiros Various
CONVERTIPLANES 50 1 Report 67-050161 AFFDL-TR-195 The X-19 V/STOL
Technology – A Critical Review May 1967
2 Miscellaneous Tilt-Rotor Papers 1967 3 Report No. 200-947-003 Model Specification for Two
Place, Single-Engine Convertiplane Bell Sep 3 1952
4 Army Air Mobility Study – Advanced Concepts Supplement
Jun 1962
5 Report 200-099-932 Proposal for a Modernized Version of the XV-3 Convertiplane Bell
Sep 26 1960
6 SAE Report 650193 Helicopters and Propeller-Type VTOL Aircraft in the Light of Technologies by W.Z. Stepniewski & M.I. Young Boeing-Vertol
Apr 12-16 1965
7 FW 860 Seitenleitwerk Photos and Technical Data Sep 1979 8 VC-400 Symposium Info (in German) Nov 1967 9 AHS 50th Annual Forum – Aerodynamic Evaluation of the
V-22 Osprey Wing Section by J.C. Narramore & M.K. Farrell Bell & W.K. Grauer Boeing
May 11-13 1994
10 Report No. CER 897 ER on The Results of the Wind Tunnel Testing for the 1/10 Scale Aerodyne Model Contract# Nonr 2566(00)
Jan 30 1959
11 The Domain of the Convertible Rotor by R. Hafner Westland Aircraft Ltd.
Undated
12 AHS 28th Annual Forum #615 Parametric Studies of Instabilities Associated with Large, Flexible Rotor Propellers by Dr. Robert A. Johnson Sikorsky
May 1972
13 AHS 24th Annual Forum Tilt-Proprotor Composite Aircraft, Design State of the Art by K.G. Wernicke Bell
May 1968
14 Planicopter Project II, IIIA, IIIB Undated 15 VC-400 VTOL-Kipp-Rotor (in German) Aug 14 1964
111
16 Report No. 200-094-270 Results of the Wind Tunnel Tests of the Quarter-Scale Semi-Span Model of the XV-3 Tilting-Rotor Convertiplane Contract# AF 33(600)20777
Aug 18 1958
17 NACA TN 3917 Effects of Propeller Location and Flap Deflection on the Aerodynamic Characteristics of a Wing-Propeller Combination for Angles of Attack from 0o to 80o
Jan 1957
18 NASA TN D-318 A Wind Tunnel Investigation of Three Propellers Through an Angle of Attack Range from 0o to 85o
May 1960
19 NASA TN D-730 Aerodynamic Characteristics of Propeller-Driven VTOL Aircraft
Mar 1961
20 Report No. 200-099-201 Calculated Weight and Balance XV-3 Convertiplane Contract# AF 33(600) 20777
Nov 1 1954
21 VTOL Articles Various 22 NASA CR 177452 Civil Tiltrotor Missions and
Applications: A Research Study Contract# NAS2-12393 Jul 1987
23 JVX “What an Opportunity” Presentation Slide Printouts Apr 20 1982 24 Technology Assessment of Capability for Advanced Joint
Vertical Aircraft (JVX) Industry Debriefing Jun 28 1982
25 XV-15 Articles and Photos Various 26 XV-3 Articles and Photos Various 27 Model 732 Variants Conceptual Diagrams Undated 28 V-22 Photos, Articles Various 29 V22/MV22 5 Theses 1988-1989 30 AHS 40th Annual Forum JVX Design Update by Stanley
Martin, Jr. & William B. Peck Boeing-Vertol May 16-18 1984
31 NASA TM 84293 Dynamic Structural Aeroelastic Stability Testing of the XV-15 Tilt Rotor research Aircraft
Dec 1982
32 Report AD-B102 592 Evaluation of XV-15 Tilt Rotor Aircraft Concept for JVX Missions
May 12 1986
33 Report AD-A134 642 Airloads on Bluff Bodies, with Application to the Rotor-Induced Downloads on Tilt-Rotor Aircraft
Sep 1983
34 AIAA-83-2695 Frequency-Domain Identification of XV15 Tilt-Rotor Aircraft dynamics
Nov 16-18 1983
35 Report AD920906 Low-Disc-Loading Helicopter and Tilt-Rotor Aircraft Study Bell
Apr 1974
36 An Analysis of Low-Disc-Loading VTOL Aircraft Types by Robert L. Lichten Bell
Jan 10-13 1966
37 Expanding Tilt Rotor Capabilities by J.M. Drees Bell 1988 38 Advanced Helicopter Technology Seminar Jul 18 1967 39 Prop-Rotor Info Various 40 AFFDL-TR-70-44 Configuration Design Analysis of a
Prop/Rotor Aircraft Apr 1970
41 General Considerations for Response of Tilting Rotors to Sharp Edge Gusts by R.F. Klingloff Sikorsky
Nov 4 1969
112
42 VTOL Transportation Briefing May 18 1966 43 NASA TM 81280 Historical Overview of V/STOL
Aircraft Technology by Seth B. Anderson Mar 1981
44 Report D266-099-104 Composite Research Aircraft Design Study – Weight and Balance Contract# DA-44177-AMC-373(T)
May 1966
AUTOGIROS 51 1 Report No. 146X90-2 A Proposal to Appraise the Modern
Usefulness of Autogiros Kellett Aircraft Dec 12 1958
2 Rotary Wing Kite (partial) Lt. R.N. Gottfried (from German)
Undated
3 Report No. UDSE-TR-74-03 Autogiro Feasibility Study Design and Cost Analysis by F. Gerard Albers Univ. of Dayton
Aug 1974
4 McCulloch Autogiro Pamphlets 1966-1968 5 The Police Autogiro – Plan For Development Sep 1972 6 McCullogh Autogiro Papers 1968 7 Report No. WSDS 69-61 Hanson Autogiro Study Dec 1969 8 FA-330 German Submarine (U-Boat) Kite Oct 12 1948 9 Report No. 158X90-1 The 1960 Autogiro A New
Observation and Liaison Aircraft Kellett Feb 1959
10 Kinedyne 2 Autogiro Cessna C.A. 1958 11 Report No. 3 Super-STOL A Proposal For general
Aviation by Thomas F. Hanson May 1969
12 Autogiro – Miscellaneous Papers Undated 13 Report No. USDE-TR-75-09 Simulation of Autogiro
Performance by F. Gerard Albers & David L. Moorman Univ. of Dayton
Oct 1975
14 NACA Confidential Memorandum Report Control-Force and General Performance Tests of Kellett YG-1 Autogiro
Mar 27 1936
15 The Hafner Gyroplane by Raoul Hafner Feb 1938 16 Kellett YG-1 Wind-Tunnel and Flight Tests C.A. 1937 17 Reports and Memoranda No. 1859 General Investigation
into the Characteristics of the C.30 Autogiro Mar 1939
18 Report No. Z-812 Apparent Aerodynamic Limitations of Rotary Wing Aircraft in Towed Flight Eastern Rotorcraft
Jul 15 1948
19 Reports and Memoranda No. 1154 Wind Tunnel Experiments on a Model Autogiro at Small Angles of Incidence
Mar 1928
20 Reports and Memoranda No. 1116 Wind Tunnel and Dropping Tests of Autogiro Models
Nov 1926
21 Report No. 160.37Flight Performance Tests of the XR-3 Autogiro Kellett Aircraft
May 26 1944
22 Report No. ASTDN FTR 70-6 Rotorglider Discretionary Descent Concept by Robert W. Markland
Feb 1970
113
23 Aircraft Carrier by Jerry O’Rourke Feb 19 1975 24 Report No. LR 24151 STOL/Autogiro Vehicle Study for
Mass Urban Transportation Lockheed-California Dec 1970
25 Report No. R-70-0-3061-A Proposal for the Kaman Model K-15 Utility and Liaison Gyroplane Kaman
Apr 6 1955
26 NACA Memorandum Report Full-Scale Wind-Tunnel and Flight Tests of a YG-1 Autogiro
Aug 26 1937
27 Report No. G-101 Analysis of Giro-Glider AGA Aviation Corp.
Jan 20 1943
28 The Autogiro – Tomorrow’s Aircraft Today by Robert K. Clark
1975
29 Cyclogiro Information C.A. 1967 30 The Roadable Autogiro by B. Lindenbaum Nov 1971 31 Drone Autogiro –AISA GU-100 Jun 14 1973 32 FA223 Equipment Test Photos Undated 33 Comparative Evaluation of the Kinedyne Cessna Undated 34 Report No. 12-170.1 Design Study for KD-2X Giro
Incorporating Direct Take-Off and Direct Landing Kellett Sep 24 1937
35 The Autogiro – A Business Opportunity Undated 36 Testimony Before the Committee on Military Affairs of the
House of Representatives Apr 26 1938
37 Report No. R-80 Aerodynamic Performance Characteristics – Kaman Model K-15
Apr 6 1955
38 Autogiro Transparencies C.A. 1965 39 Autogiro Proposal to Aerospace Corp. by Nichols Jan 1973 40 Extra Figures and Tables for Police Autogiro Report C.A. 1972 41 Schluter ROBBE Autogiro 1990 42 Autogiro – Miscellaneous Post WWII Various 43 Engine Off Landings Nov 13 1947 44 NACA TN No. 741 Observations in Flight of the Region
of Stalled Flow Over the Blades of an Autogiro Rotor Dec 1939
45 NACA TN No. 1267 Flight Tests of a Helicopter in Autorotation, Including a Comparison with Theory
Apr 1947
46 R. & M. No. 1727 The Effect of Blade Twist on the Characteristics of the C.30 Autogiro
1936
47 R. & M. No. 1802 A Rough Estimate of the Twist of Autogiro Blades in Flight
1937
48 Technique of Handling the Direct-Control Autogiro by Lou Levy Kellett
Undated
AUTOGIROS & AUTOGIRO GLIDERS/KITES 52 1 Report No. 01954-2-T Autorotating Wings: An
Experimental Investigation Contract# DAHCO-4-68C0027 Univ. of Michigan
Jun 1970
2 AISA Autogiro Sketch and Specifications Undated 3 NACA TN 209 Tests of Rotating Cylinders Dec 1924
114
5
10
15
20
25
4 NACA TM 367 Application of the “Magnus Effect” to the Wind Propulsion of Ships
Nov 17 1924
Report No. R&M, No. 1009 Experiments on the Flow Behind a Rotating Cylinder in a Water Channel
May 1925
6 Report No. R&M, No. 1018 Experiments on the Air Forces on Rotating Cylinders
Jun 1926
7 Report No. R&M, No.1410 Experiments on the Flow Past a Rotating Cylinder
Mar 1931
8 Report No. R&M, No. 1623 On the Effect of Discs on the Air Forces on a Rotating Cylinder
Jan 5 1934
9 Aerodynamics of Flight Mechanics of Magnus-Rotor Bomblets Volume I. Literature Search by James E. Brunk Contract# F08635-67-C-0135
1968
Report No. 1430.7 Wind Tunnel Test No. 1009 Test of Kellet XR-Fuselage
May 1944
11 Performance Substantiation for Kinedyne Proposal Cessna Feb 5 1958 12 Proposal – Model CH-3 Kinedyne Design – Engineer – 2
Prototypes Flight Test Cessna Apr 21 1958
13 The Kinedyne Concept Cessna Aircraft Co. C.A. 1958 14 Report No. 146X90-1 A Proposal to Appraise the Modern
Usefulness of Autogiros Kellett Sep 29 1958
Report No. 146X90-2 A Proposal to Appraise the Modern Usefulness of Autogiros Kellett
Dec 12 1958
16 Handbook of Service Instructions for the Model YO-60 Liaison Observation Autogiro Kellett
Undated
17 Report No. 56-115 Proposal for the Construction and Test of a Power Compounded Vertical Take-Off Autogiro Hiller
Dec 1956
18 Report No. 158X90-1 The 1960 Autogiro – A New Observation and Liaison Aircraft Kellett
Feb 1959
19 Report No. 420-1-23 XR-1 Aircraft Contract# W535 ac15375 Platt-LePage
C.A. 1945
Autogiro Description Material Letter Garrett Airesearch Dec 3 1973 21 Engineering Theory of the Autogiro by Juan de la Cierva
(with handwritten corrections) (probably late 1920’s) Undated
22 Report No. ER-111 Proposed Additions to “The Theory of the Autogiro” Autogiro Co. of America, Inc.
Apr 1933
23 NACA Report No. 523 The Influence of Wing Setting on the Wing Load and Rotor Speed of a PCA-2 Aurogiro as Determined in Flight
1935
24 NACA TN 581 A Study of Autogiro Rotor-Blade Oscillations in the Plane of the Rotor Disk
Sep 1936
NACA TM No. 879 Static Longitudinal Stability and Longitudinal Control of Autogiro Rotors
Oct 1938
26 TR No. 330-45 Focke-Achgelis Autogiro Type Fa 330 Sep 1945 27 Item No. 12 File No. XXVIII-21 CIOS German Submarine C.A. 1945
115
Rotary Wink Kite 28 Report No. 33200 “Rotochute” Rotary Wing Glider-Kite
General Electric Co. Oct 25 1946
29 Report No. DCR-292 Concept Description of Autogiro Air-Train System (AATS) Dynasciences Corp.
Nov 1968
30 Report No. AU-112 Model Specification – Rotary Wing Glider G&A Aircraft, Inc.
Sep 1 1944
31 Autogiro Drone Papers, Charts and Photos Northrop/Radioplane
Various
32 Autogiro Project – ARPA’s Visit to Spain May 2-4 1973 33 Alternate RPV Configuration Garrett Dec 3 1973 34 An Autogiro RPV Presentation Garrett Undated 35 Report No. R&M No. 1116 Wind Tunnel and Dropping
Tests of Autogiro Models Nov 1926
36 Report No. R&M No. 1131 Lift and Torque on an Autogiro on the Ground
Jul 1927
37 Report No. R&M No. 1802 A Rough Estimate of the Twist of Autogiro Blades in Flight
1937
38 NACA TN 741 Observations in Flight of the Region of Stalled Flow Over the Blades of an Autogiro Rotor
Dec 1939
39 Report No. R&M No. 1859 General Investigation into the Characteristics of the C.30 Autogiro
Mar 1939
40 Report No. R&M No. 1727 The Effect of Blade Twist on the Characteristics of the C.30 Autogiro
1933
41 Farrington Aircraft Co. Autogiro Information 1993 42 Extension of Compound Helicopter Performance by Means
of the Telescoping Rotor by Evan A. Fradenburgh Sikorsky
1969
43 Special Report on VFW Compound Aircraft Jan 17 1968 44 Tests of the German Submarine Rotary Wing Kite, Fa-330 1948 45 A Study of Design and Economics of Rotary Wing Gliders
by Igor B. Bensen Kaman Apr 26 1951
46 NACA Report No. 434 Lift and Drag Characteristics and Gliding Performance of an Autogiro as Determined in Flight
1932
47 NACA Report No.523 The Influence of Wing Setting on the Wing Load and Rotor Speed of a PCA-2 Autogiro as Determined in Flight
1935
48 NACA Report No.536 Wind-Tunnel Tests of a 10-Foot-Diameter Gyroplane Rotor
1935
49 NACA Report No.552 Wind-Tunnel Tests of a 10-Foot-Diameter Gyroplane Rotor
1936
50 NACA Report No. 600 An Analysis of the Factors That Determine the Periodic Twist of an Autogiro Rotor Blade, with a Comparison of Predicted and Measured Results
1937
51 NACA Report No. 623 A Study of the Torque Equilibrium 1938
116
on an Autogiro Rotor 52 Testimony before the Military Affairs Committee of the
House of Representatives by Harold F. Pitcairn Autogiro Co. of America
Apr 26 1938
53 McCullouch Aircraft Corp Status Summary Jul 1 1971 54 The Autogiro – A Business Opportunity by Bell Sep 15 1975 55 Tomorrow’s Aircraft Today by R.K. Clark 1976 56 McCulloch Aircraft Articles, Pamphlets and Brochures Various 57 United Technical Industries Business Plan Volume 1-Intro
and Executive Summary Jul 1983
58 United Technical Industries Business Plan Volume 2 & 3 – Detailed Business Plan Appendices
Jul 1983
59 Autogiro Miscellaneous Articles and Photos Various
COMPOUND HELICOPTERS, CONVERTIPLANES, TIP-MOUNTED POWER
53 1 Proposal for Engineering Study of Medium Transport Convertible Aircraft No. 3A
Nov 11 1957
2 Report No. R-527A UH-2 Helicopter High-Speed Flight Research Program Utilizing Jet Thrust Augmentation Final Report (Draft) Contract# DA 44-177-AMC-105(T) Kaman
Nov 1964
3 Report No. PR-564 Preliminary Design Study of VTOL Rotary Wing Composite Aircraft – Technical Proposal Contract# RFP AMC-177-65 Neg. 91 Boeing-Vertol
Jul 16 1965
4 Report No. 58-139 A Design Study of Helicopters Powered by Rotor Tip Mounted Turbojet Engines Contract# Nonr 1814(00) Hiller
Oct 1958
5 VTOL Boundaries by R.B. Lightfoot Sikorsky Feb 14 1962 6 A VTOL Progress Report for the Four-Ton Payload
Sikorsky Jan 17 1964
7 Notes on Studies of VTOL and V/STOL Aircraft by R.G. Stutz Sikorsky
Jun 1963
8 Report No. ES 40495 A RVX Study – A Comparison of Mother/Daughter and Single Aircraft Concepts Douglas
Sep 9 1961
9 Report No. UP-42 Study of Proprietary Ideas Concerning the Aerodynamics of Retractable Rigid Rotors with Circulation Control by Blowing Air Vehicle
Jun 1968
10 NASA Literature Search No. 5331 Stoppable Rotor Aircraft
Dec 1 1967
11 Convertiplane Interest Grows Fast by Robert McLarren AW&ST
Dec 26 1949
12 Model D2064 Propulsion System Blueprint Lockheed-Georgia
Mar 14 1961
13 AGARD Conference ( 2 papers on Fluid Controlled Stoppable Rotors)
Sep 20-23 1971
14 Report No. D181-945-008 Bell Aerosystem X-22 Proposal May 1956
117
with Photos 15 Aerodyne Brochure Dornier System (in German) Undated 16 Shrouded/Ducted Prop Illustrations Various 17 Report No. 84-X-5 Vectored Thrust Take-Off and Landing
Recoverable Strike RPV: Design Study Piasecki Nov 22 1973
18 Ducted Prop and Ring Wing Various 19 Report No. 7064 VTOL Unloaded Rotor Compound
Helicopter Contract# DA 44-177-TC-588 McDonnell Feb 1 1960
20 “MODUS” High Speed VTOL Reconnaissance Aircraft VMAX
Jan 1995
21 Report No. 8125 Model 177 VTOL Technical Proposal Tri-Service Transport McDonnell
Apr 3 1961
22 Report No. 7223-953001 V/STOL Capability Bell March 1965 23 McCullouch J-2 Gyroplane Brochure Undated 24 The J-2 and How to Fly it. McCullouch 1970 25 Convair VTOL/STOL Handbook Undated 26 Report NO. NB 63-228 The Northrup All Mechanical
Flight Control System for VTOL Aircraft and Reentry Vehicles
Sep 1963
27 Report No. 1272 A Project Suggestion for a VTOL RPV Centro Corp.
Undated
28 Current Sikorsky Models Brochure Jun 1966 29 Statement by R. Hafner and Extracts from Patent
Applications Sep 1938
30 Kinedyne Concept Brochure Cessna Undated 31 Sikorsky S-65-300 Compound V/STOL Transport Volume
I Technical Undated
32 Report No. LR 21049 Advanced VTOL Naval Aircraft Study Final Report Contract# N00019-67-C-0261 Lockheed-California
Jun 10 1968
33 Report No. 4197 The V-1B Convertiplane McDonnell C.A. 1955
34 Report No. 7376 (Supplement to No. 7064) Substantiating Data on the Unloaded Rotor V/STOL Transport Aircraft McDonnell
Feb 1 1960
35 Miscellaneous Papers Undated
COMPOUND & RIGID ROTOR HELICOPTERS 54 1 Report No. 285-17 (62-17) Hot Cycle Design and
Development Program Technical Summary Report Contract# AF 33(600)-30271 HTC
Mar 1962
2 Report No. HTC-AD-65-15 Rotor/Wing Concept Study, Summary TR – Volume II – Appendices A, B, C, D, E, and F Contract# Nonr-4588(00) HTC
Sep 1965
3 Report No. HTC-AD-65-37 Rotor/Wing Concept Study, Supplementary Study Report Contract# Nonr-4588(00)
Feb 1966
118
HTC 4 Report No. HTC-AD-67-3 Rotor/Wing Series VI Wind
Tunnel Test 7-Foot Diameter Model in the NASA LRC 30by-60-Foot Wind Contract# Nonr-4588(00) HTC
Apr 1968
5 Report No. HTC-AD-69-12A Rotor/Wing Final TR Contract# Nonr-4588(00) HTC
Mar 1970
6 Stowed Rotor Assault Transport Parametric Study Boeing-Vertol
1965
7 NASA TN D-5232 Wind-Tunnel Investigation of Steady-State Aerodynamics of a Composite-Lift VTOL Aircraft Model
Jun 1969
8 NASA TN D-5256 A Wind-Tunnel and Analytical Study of the Conversion from Wing Lift to Rotor Lift on a Composite-Lift VTOL Aircraft
Jun 1969
9 NASA TN D-5945 Wind-Tunnel Investigation of Various Small-Scale Rotor/Wing Configurations for VTOL Composite Aircraft in the Cruise Mode
Oct 1970
10 WADC TR 55-410 WADC Rapid Performance Prediction Method for Compound Type Rotorcraft
Mar 1959
11 USAAVLABS TR 68-31 Hot Cycle Rotor/Wing Composite Research Aircraft Contract# DA 44-177-AMC338(T)
Aug 1968
12 USAAVLABS TR 68-32 Tilt Prop-Rotor Composite Research Aircraft Contract# DA 44-177-AMC-373(T)
Nov 1968
13 NASA CR 112152 Rotor System Research Aircraft Predesign Study Final Report Volume I Summary and Conclusions Contract# NAS1-11228
Oct 6 1972
14 NASA CR 112153 Rotor System Research Aircraft Predesign Study Final Report Volume II Conceptual Study Report Contract# NAS1-11228
Oct 6 1972
15 NASA CR 112154 Rotor System Research Aircraft Predesign Study Final Report Volume III Predesign Report Contract# NAS1-11228
Oct 6 1972
16 NASA CR 112155 Rotor System Research Aircraft Predesign Study Final Report Volume IV Preliminary Draft Detail Specification Contract# NAS1-11228
Oct 6 1972
17 Report No. FT23-4R-64 Military Research Evaluation of the Lockheed XH-51A Rigid Rotor Helicopter
Jan 7 1964
18 The Conversion of the Rotor/Wing Aircraft by R.J. Huston & J.P. Shivers NASA
Sep 11-13 1967
19 Composite Aircraft Design by LeRoy H. Ludi USAAVLABS
May 10-12 1967
20 Rotor Systems Research Aircraft Predesign Summary Review
Sep 22 1972
119
21 Report No. LR 26175 VTOL Strike RPV Study Contract# F 33657-74-C-0190 Lockheed-California
Dec 12 1973
22 Possibilities of Compound Helicopters – Status 1968 by Dr. Richard M. Carlson Lockheed-California
Mar 7 1968
23 Report No. D8-0554 Evaluation Report of the Rotafix Concept Boeing-Vertol
Jan 1968
24 BRL MR 1850 Composite V/STOL Utility/Logistics Aircraft, Speed Versus Payload and Productivity
Jun 1967
25 Report No. 2346 Preliminary Stability and Control Report Model 82 Contract# AF 33(038)-28075 McDonnell
Nov 12 1951
26 Report No. SER-2554 An Examination of the Stability and Control Problems of a Compound Helicopter Contract# AF33(616)2628 Sikorsky
May 12 1955
27 Report No. SER-2557 Proposed Work Statement Extended Investigation of Long Range Helicopter Contract# AF33(616)-2628
Jun 15 1955
28 Report No. SER-2569 Proposed Work Statement – Study Toward Compound Helicopter Performance Sikorsky
Jan 23 1956
29 Report No. LR 19533 Composite Research Aircraft – Preliminary Design Study and Proposal for Full-Scale Follow-On Program Volume I – Technical Contract# DA 44-177-AMC-372(T) Lockheed-California
May 1966
30 Report No. LR 19539 Composite Research Aircraft- Summary Report Lockheed-California
May 1966
31 Report No. LR 19755 Advanced Transport Aircraft – 1975-1985 Lockheed-California
May 19 1966
32 Report No. LR 21283 A Summary of Stopped Rotor Research and Development at the Lockheed-California Company
Jan 22 1968
33 XV-1 Photos and Clippings 1966 34 Miscellaneous Loose Pages Concerning V/STOL
Transport 1960-1961
35 Roles and Missions Documents 1956 36 Compound Helicopter Photos and Notes Various 37 Convertiplane Development Project Folder Contract AF
33(600) 22222 1952-1956
SERIES VII: SR-175, Tri-Service Transport and V/STOL Transports, 1938-1990
Box File Description Date
SR-175 + SYMPOSIUMS 55 1 AHS, Inc.: Proceedings of the Sixteenth Annual National
Forum May 11-14 1960
2 USAF AFSC: Report: Beyond the Horizon: Flight in the Atmosphere, 1975-1985 Volume III Annexes Vertical
Jan 1967
120
Takeoff and Landing 3 SR-175 V/STOL Logistic Aircraft Study Vol. I Appendix;
Contractor Report Summaries Jun 1960
4 Proceeding of Rotating Wing Aircraft Meeting at Franklin Institute
Oct 1938
5 Conference on V/STOL and STOL Aircraft Ames Research Center
Apr 4-5 1966
6 Report 7277 V/STOL Logistics Aircraft Study 1965-1970 Time Period McDonnell Aircraft Corp
Feb 12 1960
7 Second Convertible Aircraft Congress Proceedings Dec 12 1952 8 USAF AFSC Report: Beyond the Horizon: Flight in the
Atmosphere, 1975-1985 Volume III Vertical takeoff and Landing
Jan 1967
9 Avenues for Research 1966 US Army Aviation Material Laboratories
Jun 1966
10 Presentation to the Ad Hoc Group on Evaluation of V/STOL Aircraft, Princeton, NJ Lockheed
Nov 11 1959
11 Proceedings of 1st National V/STOL Aircraft Symposium Supplement
Nov 3-4 1965
12 USAF AFSC Report: Beyond the Horizon: Flight in the Atmosphere, 1975-1985 Volume III Vertical Takeoff and Landing
Jan 1967
13 Proceedings of 1st National V/STOL Aircraft Symposium Nov 3-4 1965 14 AIAA/NASA Ames V/STOL Conference: A Collection of
Technical Papers Jun 6-8, 1977
15 Proceeding of Rotating Wing Aircraft Meeting at Franklin Institute
Oct 1938
16 Proceeding, Third Cal/AVLabs Symposium: Aerodynamics of Rotary Wing and V/STOL Aircraft Volume I Rotor/Propeller Aerodynamics-Rotor Noise
Jun 18-20 1969
17 Proceeding, Third Cal/AVLabs Symposium: Aerodynamics of Rotary Wing and V/STOL Aircraft Volume II Wind Tunnel Testing-New Concepts in Rotor Control
Jun 18-20 1969
18 AHS, Inc.: Proceedings of the Fourteenth Annual National Forum
Apr 16-19 1958
19 3-Ring Binder – Data and Diagrams of Various Helicopter Projects Including Kellett Project 19, G. & A. Model 49, Bell Model D-41 and Sikorsky Model R-5D
Undated
20 USAF AFSC Report: Beyond the Horizon: Flight in the Atmosphere, 1975-1985 Volume III Vertical Takeoff and Landing
Jan 1967
TRI-SERVICE TRANSPORT
121
5
10
15
20
25
56 1 NA01H-101 Tri-Service VTOL Transport Aircraft – Proposal Summary North American Aviation, Inc.
Apr 3 1961
2 Tri-Service VTOL Transport Sketches and Blueprints North American Aviation, Inc.
1961
3 Report PDR-511A-11 Helicat Aerodynamic Model and Full Cyclic Prop/Rotor System Vol. 1 Technical Proposal Grumman
Oct 1970
4 Report PDR-511A-12 Helicat Aerodynamic Model and Full Cyclic Prop/Rotor System Vol. 1 Price Proposal Grumman
Oct 1970
Grumman Helicat Presentation c.a. 1970 6 NASA Memo 8-4-59A Full-Scale Wind-Tunnel
Investigation of the Longitudinal Characteristics of a Tilting-Rotor Convertiplane
c.a. 1959
7 Prop-Rotor Stability at High Advance Ratios – Article Undated 8 Design and Developmental Considerations of the X-19
VTOL Aircraft Curtiss-Wright Undated
9 Sikorsky Concept Photos VTOL Transport Undated Advanced VTOL Concepts Presentation Boeing Oct 1967
11 XV-15 Presentation Vugraphs Undated 12 Bell Helicopter Letter, Pamphlets XV-3/XV-15 Feb 23 1978 13 Report 299-099-128 Technical Considerations for Low-
Disc-Loading V/STOL Aircraft of the Fixed-Wing and Tilt-Wing Configurations
Dec 23 1959
14 JVX What an Opportunity Presentation Apr 20 1982 Tilt-Rotor Articles and Pamphlets Various
16 D246-099-020 V/STOL Transport Aircraft Study 19651970 Bell
Mar 1 1960
17 Bell Helicopter Cost and Engineering Proposals, Tri-Service VTOL Transport Aircraft
Mar-Apr 1961
18 D252-099-001 Summary Report D252 Tri-Service Transport Aircraft Bell
Mar 31 1961
19 D252-099-003 Stability and Control Analysis D252 Tri-Service Transport Aircraft Bell
Mar 30 1961
D252-099-004 Estimated Weight and Balance D252 Tri-Service Transport Aircraft Bell
Mar 30 1961
21 D252-099-005 Structural Description and Design Data D252 Tri-Service Transport Aircraft - Bell
Mar 30 1961
22 D252-099-006 Structural, Ground and Flight test Program D252 Tri-Service Transport Aircraft - Bell
Mar 30 1961
23 D252-099-007 Power Plant and Drive System Installation D252 Tri-Service Transport Aircraft - Bell
Mar 30 1961
24 D252-099-008 Maintenance and Support Data D252 Tri-Service Transport Aircraft - Bell
Mar 30 1961
D252-099-009 Dynamics Analysis D252 Tri-Service Transport Aircraft - Bell
Mar 30 1961
122
26 D252-947-001 Detail Specification D252 Tri-Service Transport Aircraft - Bell
Mar 30 1961
27 Report 300-099-003 Advancement of PropRotor Technology Task I-Design Study Summary Contract# NAS 2-5386 Bell
Sep 3 1969
28 Boeing Document D-215-10000-1 Determination of design Criteria and Demonstration of Technology of s Prop/Rotor Aircraft R&D Interim Report R&D-3-FDL
Aug 1969
29 Boeing Document D-215-10000-1 Detail Design of Critical Components for a Prop/Rotor Aircraft Phase II of Determination of Design Criteria and Demonstration of Technology of s Prop/Rotor Aircraft
Jul 1970
30 Helicat Aerodynamic Model and Full Cyclic Prop/Rotor System Volume 1 – Technical Proposal (Revision)
Undated
31 Sikorsky S-65-200 Compound Helicopter Brochure Undated 32 Report No. LR 21793 Proposal for Study of Propulsion
System Requirements for Advanced Rotary Wing Compound and Composite Aircraft Lockheed-California
Sep 1968
33 Report No. FT-66-1 Analysis of VSTOL Aircraft Configurations for Short Haul Air Transportation Systems Contract# C-85-65 (Dept. of Commerce)
Nov 1966
34 Report No. 535 Dynamic Stability Analysis of a VTOL Vectored Slipstream Vehicle During Transition Contract# Nonr 1858(01) and (14) Princeton Univ.
Apr 1961
TILT-WING/PROPELLOPLANE 57 1 Report 58-136 Remote Controlled Free Flight Test of a 1/8
Scale Model X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
Oct 31 1958
2 Grumman Tilt-Wing Design 242 – Miscellaneous Papers and Pictures
Undated
3 Boeing-Vertol Model 119F Proposal PR 394 Undated 4 Report 56-60 Tilt-Wing Propelloplanes for Transport-
Rescue Missions Hiller Jun 1956
5 ARD-207 VTOL Amphibious Assault Transport Systems 1962-1967 Hiller
Jan 30 1959
6 Product Analysis of Tilt Wing Propelloplane Type VTOL Aircraft by J. B. Nichols Hiller
Undated
7 VTOL/VSTOL Logistic Transport Tilt Wing Propelloplanes Contract AF SR 175 Hiller
Feb 1960
8 Report 461.3 A Simplified Theoretical Investigation of a Wing-Propeller Combination Through a Range of AngleOf-Attack from 0 to 90 Degrees and a Comparison with Experimental Results
Oct 15 1955
9 Report 461.31 A Simplified Theoretical Investigation of a Wing-Propeller Combination Through a Range of Angle-
Apr 6 1956
123
Of-Attack from 0 to 90 degrees II – Partial Wake Deflection
10 Propelloplane Transport Study Summary Report Contract# Nonr-1657(00) Hiller
May 15 1956
11 Tilt Wing Propelloplane Design Requirements by Joseph Stuart III Hiller Helicopters Plus Slides and Photos
Oct 7-9 1956
12 NASA Memorandum 11-3-58L Force-Test Investigation of the Stability and Control Characteristics of a 1/4 –Scale Model of a Tilt-Wing Vertical-Take-Off-and-Landing Aircraft
Nov 20 1958
13 NASA Memorandum 11-4-58L Flight Investigation of the Stability and Control Characteristics of a 1/4 –Scale Model of a Tilt-Wing Vertical-Take-Off-and-Landing Aircraft
Nov 20 1958
14 Report CS-1790 SER-50145 U.S.NAVY Tri-Service VTOL Prototype Transport Engineering Proposal Part I Sikorsky
Apr 3,1961
15 Report CS-1790 SER-50145 U.S.NAVY Tri-Service VTOL Prototype Transport Engineering Proposal Part II Sikorsky
Apr 3 1961
16 Report 59-34 Airplane Stability and Control X-18 Tilt-Wing Test Bed Contract# AF 33(600)32749 Hiller
May 15 1959
17 Report 57-9 Aerodynamic Data for Structural Analysis X18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)32749 System No. 607A Hiller
Feb 21 1958
18 HSER 2407 Blade for Sikorsky Tri-Service VTOL Sikorsky
Mar 28 1961
19 SER 50146 Tri-Service VTOL Prototype Transport Proposed Ground Test Program Sikorsky
Apr 3 1961
20 SER 50147 Tri-Service VTOL Prototype Transport Proposed Flight Test Program Sikorsky
Apr 3 1961
21 SER 50148 Tri-Service VTOL Prototype Transport Proposed Detail Specification Sikorsky
Mar 29 1961
22 SER 50149 Tri-Service VTOL Prototype Transport Supporting Research Report for Engineering Proposal Sikorsky
Apr 3 1961
23 Report 57-58-1 Estimated Flight test Performance X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 System No. 607A Hiller
May 31 1957
24 Report 57-58-2 Estimated Flight Test Performance X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 System No. 607A Hiller
May 31 1957
25 Breguet 941 VTOL Transport Detail Specification Summary Report for Tri-Service Prototype Aircraft by Harlan D. Fowler
Apr 9 1961
26 U.S.NAVY Tri-Service VTOL Prototype Transport Cost Proposal Refer to CS 1790 Sikorsky
Apr 14 1961
124
27 Report 58-74 An Analysis of the Variation of Pitching Moment in Transition Flight X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 System No. 607A Hiller
May 27 1958
28 Report 56-94 Stability and Control Analysis Aircraft, Tilt-Wing, VTOL Test Bed X-18 Contract# AF 33(600)-32749 System No.451L Hiller
Oct 5 1956
29 SR 175 VTOL/VSTOL Logistic Transport Tilt Wing Propelloplanes
Feb 12 1960
V/STOL TRANSPORT/LIFT FANS & FAN IN WING 58 1 Report G-18-35 VTOL/STOL Logistics Aircraft
Parametric Study – 1965-1970 Time Period Ryan Jan 23 1960
2 Report A 35-52-2 Preliminary Design Report Study of Submerged Fan Type VTOL Aircraft Contract# AF33(616)-6605 Ryan
Feb 15 1960
3 Lift Fan Miscellaneous – 1) Concept Photos (6); 2) VZ-11 Pamphlet; 3) Vertiflite Article Feb 1964 – Lift Fan Concept
1964
4 FTC-TR-66-30 Flight Evaluation of the XV-5A VSTOL Aircraft
Mar 1967
5 XV-5A Lift Fan VSTOL A/C Flight Test Accomplishments GE Flight Propulsion Div.
1967
6 Report 63B032A Operational V/STOL Aircraft Evaluation Program – Volume III – Aircraft Characteristics Ryan
Aug 13 1963
7 IAS Paper No. 63-27 Characteristics of Aircraft with Lifting-Fan Propulsion Systems for V/STOL by Robert H. Goldsmith and David H. Hickey
Jan 21-23 1963
8 AIAA Paper No. 69-200 Deaign Concept for V/STOL Intercity Jet by Peter G. Kappus GE Engines
Feb 17-19 1969
9 Convertible V/STOL Propulsion Systems – Large Engines GE Flight Propulsion Div.
Sep 1961
10 NASA TN D-5695 Wind-Tunnel Investigation of a V/STOL Transport Model with Six Wing-Mounted Lift Fans
Mar 1970
11 NASA TN D-4322 Static and Dynamic Longitudinal Stability Derivatives of a Powered 0.18 Scale Model of a Fan-In-Wing VTOL Aircraft
Feb 1968
12 NAS2-5499 Advanced Lift Fan Aircraft Study McDonnell Aircraft
Jun 2 1970
13 TSP-6415 Lift Fan Technology Undated 14 NA-66-1287 Fan and Inlet Performance from an
Experimental Investigation of a Multi Fan-In-Wing V/STOL Model North American
Jan 4 1966
15 R60FPD149 Volume III – Propulsion System Data Parametric Study SR-175 VTOL/STOL Logistics Aircraft
Mar 1960
125
1965-1970 Period GE Flight Propulsion 16 WADD TR 60-374 Volume I Study of Submerged Fan
Type VTOL Aircraft Ryan May 25 1960
17 Report G-29-42 Parametric Analysis Report Study of Submerged Fan Type VTOL Aircraft Ryan
Sep 8 1959
18 GE Propulsion Magazine Vol. I No. 11, 17(2copies),21,23 Undated 19 Technical Discussion on the Tip Turbine Driven Lift and
Lift/Cruise Fan Propulsion System GE Flight Propulsion Undated
20 Lift Fan data for V/STOL Medium Logistics Transports GE Flight Propulsion
Jan 27 1961
21 Report 22272-1 Strike Escort Rescue Aircraft Ryan Model 222 – Summary Aircraft Specification
Dec 7 1966
22 WADD TR 60-374 Volume II – Study of Submerged Fan Type VTOL Aircraft GE
Mar 1960
23 NASA TN D-4092 Aerodynamic Characteristics of a Large-Scale V/STOL Transport Model with Lift and Lift-Cruise Fans
Aug 1967
24 Report G-52-6 The feasibility of the VERTIFAN Concept Ryan
Feb 18 1958
25 Report A35-52-1 Aircraft Design Studies Report of Submerged Fan Type VTOL Aircraft Contract# AF33(616)-6605 Ryan
Nov 15 1959
26 Report 63B033 (Partial) untitled Ryan Undated 27 Report 64B002 Proposal for V/STOL Operational
Evaluation Aircraft Program Part I – Aircraft Preliminary Specification Ryan
Feb 10 1964
V/STOL SHORT HAUL TRANSPORT 59 1 Parametric Investigation on STOL Aircraft FIAT Jun 20 1960
2 Report 61B118 Proposal for a Flex Wing STOL Assist System for a USAF F-100D Aircraft Ryan
Dec 1 1961
3 Report AER-E1R-12759 V-451 Close Support STOL Chance Vought
C.A. 1961
4 Report DAC-56096 Preliminary Results – Advanced Tactical Transport Studies (with inserts) Douglas
Mar 23 1967
5 Report LB-30899 Proposal for an STOL to V/STOL 10-12 Ton Payload Assault Transport Douglas
Jun 8 1962
6 Soviet YAK Freehold and SU-7 Fighters – Negative Copy from AWST
Apr 14 1969
7 Report 9D-F-11 Research and Development Program for Low Airspeed Control Techniques as Applied to STOL Vehicles (Preliminary Draft) Honeywell
Oct 15 1969
8 Report D3-8514-2 Low-Wing-Loading STOL Transport Ride Smoothing Feasibility Study Boeing
Jan 1971
9 Report D6-8543 Design Considerations for a Ten Ton Tactical Transport Boeing
Jul 1962
126
10 Report D180-14413-1 STOL Tactical Aircraft Investigation – Final Program Review Contract#F3361571-C-1757 Boeing
Jan 24 1973
11 FTD-HC-23-179-69 Some Problems Concerning Airplanes with Short Start and Landing Distances by Z. Brodski Soviet
May 11 1970
12 “Compound Propulsion System” for Particular Application on Short Take-off and Landing Airplanes and Flying Boats (S.T.O.L.) FIAT
Sep 16 1959
13 Short Take-Off and Landing Jet Plane Fitted with a “Compound Propulsion System” FIAT
Sep 16 1959
14 AFFDL-TR-71-26-VOL I STOL High-Lift Design Study Volume I. State of the Art Review of STOL Aerodynamic Technology
Apr 1971
15 NASA CR 114612 Quiet Turbofan STOL Aircraft for Short Haul Transportation – Final Report Contract# NAS 2-6995 Lockheed
Jun 14 1973
16 NASA CR 114613 Quiet Turbofan STOL Aircraft for Short Haul Transportation – Final Report Contract# NAS 2-6995 Lockheed
Jun 14 1973
17 NASA CR-(?) Study of Quiet Turbofan Aircraft for Short Haul Transportation Lockheed
Jul 1973
18 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume I : Summary Contract# NAS2-6994 Lockheed
Jun 1973
19 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume II : Aircraft Contract# NAS2-6994 Lockheed
Jun 1973
20 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume III : Airports Contract# NAS2-6994 Lockheed
Jun 1973
21 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume IV : Markets Contract# NAS2-6994 Lockheed
Jun 1973
22 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume V : Economics Contract# NAS2-6994 Lockheed
Jun 1973
23 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume VI : Systems Analysis Contract# NAS2-6994 Lockheed
Jun 1973
TRI-SERVICE TRANSPORT- D-828 (DOUGLAS REPORT ES40292 )
60 1 Douglas Proposal Sketches and Loose Papers for ES 40292 Mar 31 1961 2 ES 40292 Features of the D-828 Concept Douglas Apr 12 1961 3 ES 40292 Book 1 Program General Summary (Lots I and Mar 31 1961
127
II) Douglas 4 ES 40292 Book 2 Summary Report (Technical) Douglas Mar 31 1961 5 ES 40292 Book 3 Operational Suitability Douglas Mar 31 1961 6 ES 40292 Book 4 Configuration Selection Douglas Mar 31 1961 7 ES 40292 Book 5 Effects of Dimensional Limitations
Douglas Mar 31 1961
8 ES 40292 Book 7 Part II Power Plant Analysis Douglas Mar 31 1961 9 ES 40292 Book 9 Aerodynamic Test Program Douglas Mar 31 1961 10 ES 40292 Book 10 Part I Weight and Balance Douglas Mar 31 1961 11 ES 40292 Book 10 Part II Weight and Balance Douglas Mar 31 1961 12 ES 40292 Book 11 Structural Description and Design Data
Douglas Mar 31 1961
13 ES 40292 Book 12 Structural Test Program Douglas Mar 31 1961 14 ES 40292 Book 13 Flight Control Systems Douglas Mar 31 1961 15 ES 40292 Book 14 Power Plant Installation and Fuel
System Douglas Mar 31 1961
16 ES 40292 Book 14 Appendix D Hamilton Standard Propellers Douglas
Mar 31 1961
17 ES 40292 Book 14 Appendix E Development Status of Variable Camber Propeller Douglas
Feb 15 1961
18 ES 40292 Book 14 Appendix F Propeller Fiberglass Blade Construction Douglas
Mar 31 1961
19 ES 40292 Book 14 Appendix G Power Plant Main Transmission Gearbox Douglas
Mar 31 1961
20 ES 40292 Book 15 Hydraulic and Landing Gear Systems Douglas
Mar 31 1961
21 ES 40292 Book 16 Electrical Systems Douglas Mar 31 1961 22 ES 40292 Book 17 Instruments and Avionics Systems
Douglas Mar 31 1961
23 ES 40292 Book 18 Crew and Cargo Compartments Douglas
Mar 31 1961
24 ES 40292 Book 19 Detail Specifications Douglas Mar 31 1961 25 ES 40292 Book 20 Demonstration Program Douglas Mar 31 1961 26 ES 40292 Book 21 Maintenance and Support Douglas Mar 31 1961 27 ES 40292 Book 22 Program Plan – Schedules,
Management and Resources Douglas Mar 31 1961
28 ES 40292 Book 22 Appendix C Cost reductions in Navy Programs Douglas
Mar 31 1961
29 ES 40292 Book 23 Cost and Contract Terms Douglas Mar 31 1961 30 ES 40292 Book 24 Lot III Program Douglas Mar 31 1961 31 Addendum No. 104A (Proposed) to Specification MIL-D
8706(AER)-2 Design Data and Tests Lot I Douglas Apr 15 1961
32 Addendum No. 104B (Proposed) to Specification MIL-D8706(AER)-2 Design Data and Tests Lot II Douglas
Apr 15 1961
Tri-Service VTOL Transport Aircraft - North
128
American Aviation, Inc Document NA61H 61 1 -102 Technical Summary Apr 3 1961
2 -103 Detail Specification Apr 3 1961 3 -104 Master Development Plan Apr 3 1961 4 -105 Technical Development Plan Apr 3 1961 5 -106 Weight and Balance Apr 3 1961 6 -108 Stability and Control Analysis Apr 3 1961 7 -110 Electrical System Apr 3 1961 8 -111 Structural Description and Design Data Apr 3 1961 9 -113 Power Plant Installation and Fuel System Apr 3 1961 10 -114 Hydraulic and Pneumatic Systems Apr 3 1961 11 -115 Maintenance and Support Apr 3 1961 12 -116 General Demonstration Requirements for Tri-Service
VTOL Apr 3 1961
13 -117 Design Analysis and Effects of Dimensional Limitations
Apr 3 1961
14 -118 Reliability and Value Control Apr 3 1961 15 -119 Human Factors Engineering Apr 3 1961 16 -120 Control Systems Apr 3 1961 17 -121 Simulation Study of Hovering and Transition Flight Apr 3 1961 18 -122 Statement of Work Apr 3 1961 19 -123 Electronic System Apr 3 1961 20 -125 Estimated Moments of Inertia Apr 3 1961 21 -126 Tilt-Wing Dynamic Development Vehicle Apr 3 1961 22 -128 Modified Program Statement of Work Apr 3 1961 23 -127 Program Management Report Apr 3 1961 24 -193 Low Speed Wind Tunnel Tests on a .165-scale Full
Span Model of a V/STOL Vehicle to Determine Aerodynamic Characteristics in Transition and Hovering Flight
Apr 3 1961
25 -213 Low Speed Wind Tunnel Tests on a .165-scale Four Engine Tilt Wing Model of a V/STOL Vehicle to Determine Aerodynamic Characteristics in Transition and Hovering Flight
Apr 3 1961
SR-175 (BELL) & DUCTED PROPELLER 62 1 Report No. D181-945-002 Ducted Propeller Assault
Transport Design Report Contract# Nonr-1675(00) May 15 1956
2 Report No. D181-945-003 Ducted Propeller Assault Transport Survey-State of the Art Contract# Nonr1675(00)
May 15 1956
3 Report No. D181-945-004 Ducted Propeller Assault Transport Performance Contract# Nonr-1675(00)
May 15 1956
4 Report No. D181-945-006 Ducted Propeller Assault Transport Duct and Propeller Analysis Contract# Nonr1675(00)
May 15 1956
129
5 NASA TN D-4343 Wind-Tunnel Investigation of Lateral Aerodynamic Characteristics of a Powered Four-Duct-Propeller VTOL Model in Transition
Feb 1968
6 Report No. 2-60-945001 SR-175 VTOL/STOL Logistics Aircraft Parameter Study Bell Aircraft Corp.
Feb 29 1960
7 Report No. D190B-945-008 V/STOL Interim Transport Aircraft Weapons System Analysis Report Bell Aircraft Corp.
Jul 10 1959
8 Report No. D190B-945-009 V/STOL Interim Transport Aircraft Detail Specification Report Bell
Jul 10 1959
9 Report No. D190B-945-010 V/STOL Interim Transport Aircraft Aerodynamics Data Bell
Jul 10 1959
10 Report No. D190B-945-011 V/STOL Interim Transport Aircraft Structural Report Bell
Jul 10 1959
11 Report No. D190B-945-012 V/STOL Interim Transport Aircraft Weight and Balance Report Bell
Jul 10 1959
12 Report No. D190B-945-014 V/STOL Interim Transport Aircraft Stability and Control – Hovering and Transition Bell
Jul 10 1959
13 Report No. D190B-945-015 V/STOL Interim Transport Aircraft Propulsion System Analysis Bell
Jul 10 1959
14 Report No. D190B-945-016 V/STOL Interim Transport Aircraft Electrical System Load Analysis
Jul 10 1959
15 Report No. D190B-945-018 V/STOL Interim Transport Aircraft Technical Summary Bell
Jul 10 1959
16 Report No. D190B-945-020 V/STOL Interim Transport Aircraft for Air Recovery Liaison General Utility Bell
Aug 1959
17 Report No. D190B-945-022 V/STOL Interim Transport Aircraft for Air Recovery Liaison General Utility Bell
Nov 1960
TRI-SERVICE TRANSPORT -BELL/LOCKHEED 63 1 Report No. D2064-953001 Tri-Service VTOL Transport
Volume 1 Part II Technical Summary Bell & Lockheed Apr 1961
2 Report No. D2064-953001 Tri-Service VTOL Transport Volume 2 Detail Specification Bell & Lockheed
Apr 1961
3 Report No. D2064-953001 Tri-Service VTOL Transport Volume 3 Weight and Balance Bell & Lockheed
Apr 1961
4 Report No. D2064-953001 Tri-Service VTOL Transport Volume 4 Power Plant Analysis Bell & Lockheed
Apr 1961
5 Report No. D2064-953001 Tri-Service VTOL Transport Volume 6 Standard Aircraft Characteristics Charts Bell & Lockheed
Apr 1961
6 Report No. D2064-953001 Tri-Service VTOL Transport Volume 7 Stability and Control Bell & Lockheed
Apr 1961
ACADEMIC VTOL & AHS PROCEEDINGS
130
5
10 15
20
25
64 1 IAS Annual Meeting – A Tested Solution of the Problem of Helicopter Stability and Automatic Control by Donald N. Meyets & Edward G. Vanderlip Piasecki & P. Halpert Sperry Gyroscope
Jan 29 1951
2 Report D6-5201 SR-175 Program Study Boeing Jan 1960 3 Report ER-4221 (60WCL-675) SR-175 V/STOL Logistic
Aircraft Parametric Study 1965-1970 Time frame Collection of Pertinent Data Lockheed-Georgia
Feb 1 1960
4 Report 60WWR-930 SR-175 V/STOL Logistic Aircraft Study Summary and Recommendations
Jun 23 1960
VTOL-STOL Hazards and Special Problems Conference Jan 26 1961 6 Report TOR-0073(3657-01)-1 Equipment Systems
Improvement Program – Development Evaluation of Aerial Vehicles for Law Enforcement Applications by J.B. Nichols Contract# F04701-72-C-0073
Jun 1973
7 1st Convertible Aircraft Congress Proceedings Dec 9 1949 8 2nd Convertible Aircraft Congress Proceedings Dec 12 1952 9 3rd Convertible Aircraft Congress Proceedings Nov 25 1955
4th Convertible Aircraft Congress Proceedings 1958 11 Proceedings of the Third Annual Forum of the AHS Mar 27-29 1947 12 Proceedings of the Fifth Annual Forum of the AHS May 12-13 1949 13 Proceedings of the Eleventh Annual Forum of the AHS Apr 27-30 1955 14 Proceedings of the Thirteenth Annual Forum of the AHS May 8-11 1957
Proceedings of the Eighteenth Annual Forum of the AHS May 2-4 1962 16 Proceedings of the Nineteenth Annual Forum of the AHS May 1-3 1963 17 AHS 28th Annual Forum – Presentations and Index May 1972 18 R & D Contributions to Aviation Progress (RADCAP)
Volume I Summary Report Aug 1972
19 R & D Contributions to Aviation Progress (RADCAP) Executive Summary
Aug 1972
Gothert’s Report – VTOL Sections Undated 21 VTOL Technology for Systems Undated 22 Some Thoughts on the Design Philosophy of Subsonic
VTOL Transports by W.Z.Stepniewski Boeing-Vertol Dec 16 1960
23 Looking Ahead in V/STOL by George S. Schairer Sep 1961 24 Lecture Notes from a Short Course in V/STOL Univ. of
Tenn. Space Inst. Nov 18-23 1968
Proceedings of the Experimental V/STOL Aircraft Lessons Learned Sessions of the AIAA/AHS/ASEE Aircraft Design, Systems, and Operations Meeting
Sep 17-19 1990
VTOL TRANSPORTS 65 1 AFFDL-TR-66-195-Volume I The X-19 V/STOL
Technology – A Critical Review ( 2 copies) May 1967
2 Wind Tunnel Report 1005 X-200 Turbine Stability Model Curtiss MIT
Nov 7 1960 to Nov 23 1960
131
3 Wind Tunnel Report 1005 X-200 Turbine Stability Model Curtiss MIT
Jan 16 1961 to Feb 1 1961
4 Report No. 014-544 50-Hour Qualification Test X-19 Propeller Control Coordinator and SAS Assembly Vol. I Curtiss
Oct 25 1965
5 Report No. 030-37 Curtiss-Wright Model 207-8 V/STOL Multi-Mission Support Transport
Sep 19 1965
6 Concept Sketches Curtiss-Wright VTOL Model X-19 C.A. 1965 7 Report SD-139 Curtiss-Wright High-Speed VTOL
Airplane Model 200 General Configuration and Performance
Aug 1960
8 Report VS-118 Comparative Data X-19 Light Utility VTOL Transport
Sep 1964
9 Report No. 200-100 Model Specification Curtiss-Wright Model 200 High Speed VTOL Transport
Feb 15 1961
10 Report PDA 893063 Model 260-7 USAF Multi-Mission (RVX) Aircraft Design Study Curtiss
Aug 30 1963
11 Report VS-112 VTOL Transport Data Based on Preliminary Design Studies Curtiss
Sep 1963
12 Report PDA 10163 Model 203 Light Utility Transport Curtiss
Oct 1 1963
13 AFFDL-TR-66-195-Volume II The X-19 V/STOL Technology – A Critical Review ( 2 copies)
May 1967
14 X-19 Material 1961-1965 15 Evaluation of Curtiss-Wright VTOL Aircraft Programs 1961 16 Dornier DO-29 1960 17 Curtiss-Wright Blueprints 1961 18 Report 200-5.1.0.1 X-19 Landing Loads Criteria Dec 18 1963 19 Curtiss-Wright X-19 Papers 1963
TRI-SERVICE TRANSPORT, ADAM PROGRAM 66 1 NACA TN D-89 Wind-Tunnel and Piloted Flight
Simulator Investigation of a Deflected-Slipstream VTOL Airplane, the Ryan VZ-3RY
C.A. 1958
2 NACA TN 3182 Manual of the ICAO Standard Atmosphere
May 1954
3 Relative Power Requirement Under Static Condition Between the Tilt-Wing-Propeller and Deflected Slipstream VTOL Aircraft by Harlan D. Fowler with Letter to Lindenbaum
Aug 8 1963
4 Fowler Draguration Flap System 1964 5 Harlan D. Fowler Letters 1959-1965 6 Report RAC-1012 Variable Sweep Wing Plus V/STOL –
A New Era in Aircraft Design – Part I – Aerodynamic Design Concepts Republic
Dec 12 1962
7 Report RAC-1012 Variable Sweep Wing Plus V/STOL – Dec 12 1962
132
A New Era in Aircraft Design – Part II – Takeoff and Landing Performance Republic
8 Photos, Clippings of Deflected Slipstream A/C & Prop. STOL
Various
9 Report D3-3900-18 Boeing Model 900 Tri-Service VTOL Prototype Transport
Apr 2 1961
10 Report D3-3900-16 Proposal for a Tri-Service VTOL Prototype Transport Aircraft
Apr 17 1961
11 Report D3-3900-17 Proposal for a Tri-Service VTOL Prototype Transport Aircraft – Price Analysis
Apr 3 1961
12 AIAA Paper No. 69-201 The ADAM III V/STOL Concept by Byron R. Winborn, Jr. LTV
Feb 17-19 1969
13 ADAM (Air Deflection and Modulation) Vought Undated 14 ADAM II LTV Undated
15 The Evolution of the ADAM Concept by B.R. Winborn Vought
Jul 11 1968
16 Report No. EOR-12684 ADAM Air Force Transport Study SR 175
Feb 12 1960
17 ADAM notes and Photos Undated 18 Appraisal of Comparative Evaluation – Fan-in-Wing
Versus ADAM II Jan 10 1964
19 Report No. 2-55300/2R428 ADAM II Test Program Proposal Chance-Vought
Dec 12 1962
20 ADAM II Blueprint and Specifications Undated 21 Report AER-EOR-12725 Low Speed Wind-Tunnel Tests
of a 0.15 Scale Model “ADAM” VTOL Airplane Series I & II
Mar 8 1960
22 ADAM II Ten Ton Transport LTV Correspondence Oct 21 1964 23 Comparative Evaluation of the Fan-In-Wing and ADAM II
V/STOL Surveillance Airplanes LTV Jan 1964
24 AFFDL-TR-68-31 Part II Design, Fabrication, Testing, and Data Analysis of ADAM II Concept Part II, Shakedown Testing on Vought Aeronautics Division 7ft x 10ft Low Speed Wind Tunnel
May 1968
25 AFFDL-TR-68-31 Part III Design, Fabrication, Testing, and Data Analysis of ADAM II Concept Part III, Testing in 17ft Test Section of 7ft x 10ft Wind Tunnel, NASA Langley
May 1968
26 AFFDL-TR-68-31 Part IV Design, Fabrication, Testing, and Data Analysis of ADAM II Concept Part IV, Testing in the Langley Center 16-foot Transonic Wind Tunnel
May 1968
27 Report No. 2-53310/4R-2166 Analysis of a Low Speed Wind Tunnel Test of a High Mass Vectored Propulsion Flow Model Contract DA-31-124-ARO-D-262 LTV
Feb 15 1965
28 Report No. 2-53310/4R-2206 Analysis of a Follow-On Jul 31 1965
133
Low Speed Wind Tunnel Test of a High Mass Vectored Propulsion Flow Model Contract DA-31-124-ARO-D-262 LTV
29 Report No. 2-55400-50309 An Investigation of the Effect of Fan-Generated Turbulence on Flows in Ducts, Diffusers, and Bends LTV
Aug 19 1965
30 Report No. 2-55400-50331 Planning Document – ADAM II Experimental Program LTV
Jan 17 1966
31 Report No. 2-55400-50331 Planning Document – ADAM II Experimental Program Annex I: Estimated Costs
Jan 17 1966
32 ADAM II Hi/Lo Model Undated 33 ADAM Blueprints Various 34 “DISCOJET” Proposal M Research 1969-1970 35 A VTOL Airplane for Commercial Uses Allison 250 HP
by Harlan D. Fowler Nov 10 1960
36 V/STOL Commercial Transport 18 Passengers or 5000 lbs. Cargo Model 70 by Harlan D. Fowler
Nov 18 1964
37 Progress Report No. 25 Model M-224I STOL/VTOL Test Vehicle Contract# DA 44-177-TC-350 Fairchild
Mar 31 1958
SR-175, VTOL TRANSPORTS 67 1 Computed Induced Velocity, Induced Drag, and Angle of
Attack Distributions for a Two-Bladed Rotor by Raymond Piziali & Frank DuWaldt Cornell Contract# DA 44-111TC-698
C.A. 1962
2 YAK-36 & “Freehand” Photos & Articles 1976 3 Flight Test Experiences in Obtaining the First Commercial
Certification of a Helicopter for True Vertical Flight Takeoff and Landing Capability by John Diamond, Herbert H. Moser & Philip Camerano Boeing-Vertol
Undated
4 Miscellaneous Photos – STOL Aircraft Various 5 The Joint Army Navy Aircraft Instrument Research
Program Status Report by Harry W. Mitchel Bell May 1-3 1963
6 US/FRG V/STOL Technology Review May 6-7 1969 7 Report No. 2127-950011 X-22A Tri-Service Dual Tandem
Ducted Propeller VSTOL Aircraft Bell Jan 1968
8 Model 2064 Blueprints Bell – Lockheed Mar 1961 9 AHS 27th Annual V/STOL Forum Paper No. 544 Factors
Affecting Handling Qualities of a Lift-Fan Aircraft During Steep Terminal Area Approaches by Ronald M. Gerdes & Charles S. Hynes Ames Research Center
May 1971
10 Hummingbird Derivatives – “Centerline Lift” VTOL Aircraft Design Approach Lockheed-Georgia
Nov 1964
11 Ejector Thrust Augmentor Various 12 Dornier AG Dornier System GmbH Information Packet Feb 1970 13 VAK 191B Articles and Photos C.A. 1966
134
14 VTOL Transporters Vereinigte Flugtechnische Werke VFW (in German)
Undated
15 Report 60WWR-930 SR-175 V/STOL Logistics Aircraft Study Summary and Recommendations
Undated
16 Report ER-4221 SR-175 V/STOL Parametric Study 19651970 Time Frame Lockheed-Georgia
Feb 1 1960
17 Report SER-50107(Part II) SR-175 VTOL/STOL Logistics Aircraft Part 2 – Mission B – Design Study Sikorsky
Apr 26 1960
18 Review of Lockheed Type A V/STOL Design by B. Lindenbaum
Nov 14 1977
19 Report SER-50107(Part I) SR-175 VTOL/STOL Logistics Aircraft Part 1 – Mission A – Design Study Sikorsky
Mar 21 1960
20 Report R-294 Summary Presentation – USAF SR-175 VTOL/STOL Logistics Aircraft Parametric Study 19651970 Time Frame Kaman
Apr 8 1960
21 Report D6-15362 Flight into the Atmosphere, 1975-1985 With Presentation Handout Boeing
May 16 1966
22 Report H034 Research in Advanced Technology for Naval Vertical Lift Aircraft Final Report Contract# N00014-68C-0441
Mar 15 1969
23 Part C. Technical Possibilities & Technical Program (incomplete)
Undated
24 AIAA-83-2491 On Overview of V/STOL Aircraft Development by S.B. Anderson NASA Ames
Oct 17-19 1983
25 IAS 26th Annual Paper 808 Research in the Field of Wingless VTOL Aircraft by A.M. Lippisch Collins Radio
Jan 27-30 1958
26 IAS Summer Meeting Paper 59-122 Design Philosophy and Test Experiences of a VTOL Aircraft by Bruno J. Uberti & James B. Reichert Doak
Jun 16-19 1959
27 IAS Summer Meeting Paper 59-123 Lifting Systems for VTOL Vehicles by Scott Rethorst & W.W. Royce VRC
Jun 16-19 1959
28 AHS 95-2.5-1-9 Similarly Configured Public Use Vertical Airports for VSTOL Commuter Aircraft by William F. Chana Chana Assoc. & John B. Adams JAG Architecture
Jan 18-20 1995
29 VTOL Transportation for 1985 Presentation Handout Undated 30 Status of STAMP/STARS-V Development Program
Presentation Handout Hydra-Electric Co. Jul 9 1973
31 Performance Possibilities of Subsonic Airplanes Taking Off and Landing on the Ground Cushion by W.Z. Stepniewski Vertol
Oct 21-23 1959
32 ASTOVL – A New Look at Airbase Independence Presentation Handout McDonnell Douglas
Oct 21 1986
33 Limited Flight Experience with Several Types of VTOL Aircraft by John P. Reeder & Fred J. Drinkwater III NASA
Feb 1960
34 Fiat G91 Successor Sketches Undated
135
35 Miscellaneous Copies Undated 36 Mass Transportation – A Systems Concept by F.H.
Furguson Advanced Concepts Feb 1968
37 Report ER 9766 Mass Air Transportation Study Final Report Lockheed-Georgia
Apr 1968
38 R. & M. No. 3263 Measurement of Lift and Ground Interference on a Lifting-Fan Wing at Zero Forward Air Speed
1962
39 SAE 221 Some Performance and Operating Characteristics of Convertiplanes by R.L. Lichten Bell Helicopter
Sep 30-Oct 5 1957
40 NASA TN – D-56, D-372(2), D-444, D445, D513(2), D616, D720, D-733, D-756, D-785, D-1233
1959-1962
41 NACA TN – 3692, 3904, 4181 1956-1957
V/STOL, SR-175 68 1 V/STOL Photos and Miscellaneous Articles Various
2 AHS Eastern Regional meeting – The Convertiplane by Col. William B. Bunker US Army
Jun 8 1954
3 Report No. N79-10024 Study of Aerodynamic Technology for VSTOL Fighter/Attack Aircraft-Horizontal Attitude Concept by S.H. Brown Northrop
May 1978
4 Summary of Recent Vought V/STOL Studies Feb 12 1980 5 Report No. AFWAL-TR-86-3071 Volume I – V/STOL
Concepts and Developed Aircraft Volume I – A Historical Report (1940-1986) by B. Lindenbaum
Nov 1986
6 CAD/Vertol Commercial V/STOL System Analysis – Technical Review Minutes Boeing
Feb 20-22 1967
7 Report No. DM-62-14 A Comparison of VTOL Propulsion Systems in a Subsonic Mission by W.L. Rodenbaugh GE
Jan 18 1962
8 The Convertiplane – Implications of a New Aircraft Type on the National Aviation Policy of the US.
Oct 1954
9 Convertiplane Interest Grows Fast by Robert McLarren from Aviation Week
Dec 26 1949
10 Some Aspects of Convertible Aircraft Design by Robert L. Lichten Bell
May 9 1949
11 NASA Conference on V/STOL Aircraft Nov 17-19 1960 12 NASA SP-116 Conference on V/STOL and STOL Aircraft Apr 4-5 1966 13 Presentation to NASA Advisory Committee on Aircraft
Propulsion May 3-4 1967
14 Report No. PR69-ATT-999 Low Speed Thrust Reverser Technology
May 29 1969
15 Mach 2 V/STOL (VJ 101) Flight Test Program by George L. Bright
Sep 27-28 1963
16 High Speed VTOL Transports Undated 17 Avenues for Research 1966 US Army Aviation Materials Jun 1966
136
Lab. by Henry R. Velkoff 18 Text of Presentation to Aircraft Working Group – USAF
Scientific Advisory Board Nov 1964
19 VTOL/STOL – Aircraft Bibliography Mar 31 1961 20 Report NO. SER-50112 USAF SR 175 VTOL STOL
Aircraft Survey Sikorsky Aug 19 1960
21 Report No. 60WWR-930 SR-175 V/STOL Logistic Aircraft Study Vol. I Appendix Contractor Report Summaries
Jun 1960
22 Looking Ahead in V/STOL by George S. Schairer Sep 1961 23 Report No. FDCC TM 66-11 Research Requirements for
V/STOL Gust Response and Low Altitude Turbulence Model
Oct 1966
24 Report No. AGARDograph 46 Symposium on Vertical & Short Take-Off and Landing Aircraft Part I
Jun 1960
25 AFFDL-TR-68-85 Investigation of the Effects of Gusts on V/STOL Craft in Transition and Hover
Oct 1968
26 USAAVLABS TR 69-13 Review and Preliminary Evaluation of Lifting Horizontal-Axis Rotating-Wing Aeronautical Systems (HARWAS) Contract# DAAJ02-67C-0046
Mar 1969
27 USAAVLABS TR 69-14 A Study of Aerodynamic Performance Evaluation and Comparison Techniques for V/STOL Aircraft Contract# DA 44-177-AMC-376(T)
Jul 1969
28 ASD-TR-69-15 Part II Propeller Static Performance tests for V/STOL Aircraft Part II. Test Data (Appendix III)
Jan 1970
29 Report No. SURVIAC-TR-91-008 V/STOL Compendium and Database
Dec 1990
TRI-SERVICE TRANSPORT - BELL / LOCKHEED VTOL Proposal + WADC 59-21 + WADC 58-96to99
69 1 Report No. D2064-953001 Volume 8 Structural Description and Design Data
Apr 1961
2 Report No. D2064-953001 Volume 9 Power Plant Installation and Fuel System
Apr 1961
3 Report No. D2064-953001 Volume 13 Demonstration Program
Apr 1961
4 Report No. D2064-953001 Volume 15 Effects of Dimensional Limitations
Apr 1961
5 Report No. D2064-953001 Volume 18 Wind Tunnel Test Data
Apr 1961
6 Report No. D2064-953001 Volume 19 Propeller and Gearbox Design
Apr 1961
7 WADC TR No. 59-21 Part I A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-
Nov 12 1958
137
Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part I Containing: Summary of Study Bell report D232-099-009 Contract# AF 33(616)-5089
8 WADC TR No. 59-21 Part II A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part II Containing: Bell Reports D232-099-001, 003, 004 Vol I Contract# AF 33(616)-5089
Nov 1 1957
9 WADC TR No. 59-21 Part III A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part III Containing Bell Reports D232-099-004 Vol II Contract# AF 33(616)-5089
Nov 12 1957 rev Mar 28 1958
10 WADC TR No. 59-21 Part IV A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part IV Containing Bell Report D232-099-001 Vol III Contract# AF 33(616)-5089
Nov 12 1957 rev Mar 28 1958
11 WADC TR No. 59-21 Part VI A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part VI Containing Bell report D232-099-002, 005, 006, 008 Contract# AF 33(616)-5089
Nov 12 1957
12 WADC TR No. 59-21 Part VII A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part VII Containing Bell Report D232-099-007, 010 Contract# AF 33(616)-5089
Nov 11 1957
13 WADC TR 58-96 STOL/VTOL Propeller Study Contract# AF 33(600)-35021 Vertol
Mar 1958
14 WADC TR 58-97 STOL/VTOL Propeller Study – Aerodynamic Analysis Contract# AF 33(600)-35021 Vertol.
Mar 1958
15 WADC TR 58-98 STOL/VTOL Propeller Study – Aero-Elastic Vibration Analysis Contract# AF 33(600)-35021 Vertol
Mar 1958
16 WADC TR 58-98 STOL/VTOL Propeller Study – Stress and Weight Analysis Contract# AF 33(600)-35021 Vertol
Mar 1958
17 Report No. R351-001 M-351 Proposed Low Speed System Investigation for Tri-Service VTOL Assault Transport Fairchild
Apr 3 1961
SR-175 - BELL X-22A & SHROUDED PROPELER 70 1 Report No. D181-945-001 Ducted Propeller Assault
Transport – Summary Report Contract# Nonr-1675(00) May 15 1956
138
Bell 2 Report No. D181-945-005 Ducted Propeller Assault
Transport – Stability and Control Contract# Nonr1675(00) Bell
May 15 1956
3 Report No. D181-945-006 Ducted Propeller Assault Transport – Duct and Propeller Analysis Contract# Nonr1675(00) Bell
May 15 1956
4 Report No. D181-945-007 Ducted Propeller Assault Transport – Preliminary Structural Analysis Contract# Nonr-1675(00) Bell
May 15 1956
5 Report No. 2127-933009 X-22A Progress Report No. 9 Contract# Now 63-0118-ci Bell
Sep 15 1963
6 Report No. 2127-933073 X-22A Progress Report No. 73 Final Contract# Now 63-0118-ci Bell
Apr-Dec 1969
7 Report No. 2-60-945001 SR-175 VTOL/STOL Logistics Aircraft Parametric Study Bell
Feb 29 1960
8 IAS Report No. 59-59 Research Studies on the Ducted fan Equipped with Turning Vanes by A.W. Gilmore & W.E. Grahame Grumman
Jan 26-29 1959
9 Report No. 2127-917003 Aerodynamic Stability and Control and Flying Qualities, X-22A Contract# Now 630118-ci Bell
Dec 28 1962
10 X-22A Miscellaneous Various 11 Report No. 2127-950012 Interim Flight Test
Accomplishments – X-22A Bell Mar 1966 – Feb 1969
12 Report No. 2127-917006 Performance Data Report X-22A Contract# Now 63-0118-ci Bell
Apr 1 1963
13 Report No. D2038-953001 Appendix – Analytical Evaluation and Design of Ducted Propellers
Jul 6 1960
14 Report No. 2-60-945003 Summary of Bell Ducted Propeller
Dec 1960
15 Report No. 2-59-920002 Ducted Propeller Test Stand – Description Bell
Dec 1959
16 Report No. 59-A-3 Stability and Control Analysis – PiAC 59H – Aerial Jeep VZ-8P-II Contract# DA 44-177-TC-449 Piasecki
Feb 24 1962
17 Report No. 59-X-30 Piasecki AIRGEEP Vehicles for Army Tactical Mobility Requirements Board
Jun 15 1962
18 Report No. GDC PIN 68-805 A Proposal Wind Tunnel Test Program for Full-Scale, Single-Place Stacked Rotor Volume I – Technical General Dynamics
Oct 1968
19 Report No. R221-012 Compressibility Effect on a Shrouded Propeller Fairchild
Nov 1955
20 AIAA Paper No. 68-994 Shrouded Propellers – A Comprehensive Performance Study by Donald M. Black & Harry S. Wainauski & Carl Rohrbach United Aircraft
Oct 21-24 1968
139
21 SAE No. 730323 Shrouded Fan Propulsors for Light Aircraft
Apr 3-6 1973
22 IAS No. 621 An Application of the Ducted Propeller to a VTOL Transport Aircraft by James A. O’Malley, Jr. Bell
Jan 23-26 1956
23 NACA TR 3547 Aerodynamic Characteristics of a Small-Scale Shrouded Propeller at Angles of Attack from 0o to 90o
Nov 1955
24 Aero Report 904 Approximate Calculation of the Shrouded Propeller
Jul 1956
25 NASA TN D-995 Aerodynamic Loads on an Isolated Shrouded-Propeller Configuration for Angles of Attack from -15o to 110o
Jan 1962
26 NASA TN D-4142 A Wind-Tunnel Investigation of a 7foot-Diameter Ducted Propeller
Aug 1967
27 FTD-HT-66-273 Applications of Ducted-Fan Propellers in the Ground Forces by J. Soulez-Lariviere (from French)
Oct 14 1966
28 Progress Report No. 10 Two-Ducted Aerial Research Vehicle Period May 1 to May 31 Contract# DA-44-177TC-448
Jun 5 1958
29 Progress Report No. 11 Two-Ducted Aerial Research Vehicle Period Jun1 to Jun 30 Contract# DA-44-177-TC448
Jul 7 1958
30 Progress Report No. 12 Two-Ducted Aerial Research Vehicle Period Jul 1 to Jul 31 Contract# DA-44-177-TC448
Aug 5 1958
31 Report No. 149 Ducted Propeller Weight Lifter Contract Nonr 2199(00) Hiller
Nov 22 1957
TILT-WING V/STOL, CL-84,X-18,VC 400, XC-142A 71 1 AIAA No. 63-484 The Aerodynamic Approach to
Improved Flying Qualities of Tilt-Wing Aircraft by J.F. Martin & O.E. Michaelsen Canadair
Oct 21-24 1963
2 AIAA 90-3204 The LTV XC-142 Experimental Aircraft Lessons Learned by George E. Dausman US Army
Sep 17-19 1990
3 CL-84 Assorted Papers and Photos Canadair Various 4 Tilting Propeller Aircraft – Clippings and Photos Various 5 X-18/19 Photos and Articles 1990 6 Surveillance Aircraft System ASR No. 2-60 Martin Co. Dec 1 1959 7 Report No. R-183 A Proposal for the Design, Construction
& Test of the K-16B VTOL/STOL Research Vehicle Kaman
Nov 6 1957
8 VC 400 VTOL Cargo Aircraft VFW Munich Jun 1966 9 VC 400 Design and Operational Capability VFW Munich Apr 19 1968 10 VC 500 Briefing VFW Munich Dec 13 1969
140
11 VC 400 Articles and Brochures Various 12 Ishida Group Tilt-Wing Proposal Papers 1999 13 Report No. R-284 Shrike, ASR 2-60 Kaman Jan 29 1960 14 VZ-2 Papers Undated 15 The Canadair V/STOL Aircraft Program Nov 11 1963 16 Report No. ERR-CL-RAX-84-118 A Study of Cyclic Pitch
Propeller Application to the CL-84 Tilt Wing V/STOL Prototype Hydro/Aero/Astronautical Sciences Canadair
Oct 1965
17 Report No. RAX-84-121 CL-84G Search and Rescue Variant Canadair
Nov 29 1965
18 Report No. RAX-84-128 Technical Proposal for a Cyclic Pitch Propeller Development and Testing Program Canadair
Apr 1966
19 CL-84-1D Operational Evaluation Study for the USAF Canadair
Sep 1969
20 XC-142A V/STOL Transport Brochure Hiller, Vought, Ryan
Undated
21 NASA TN D-535 Damage Incurred on aTilt-Wing Multipropeller VTOL/STOL Aircraft Operating Over a Level, Gravel-Covered Surface
Dec 1960
22 USAAVLABS TR 67-84 Tri-Service Evaluation of the Canadair CL-84 Tilt-Wing V/STOL Aircraft
1967
23 Report No. 503 Application of Small-Scale Propeller Test Data to V/STOL Aircraft Design by Henry E. Payne III Princeton Univ.
Oct 1961
24 USAAVLABS TR 66-64 Comparison of Longitudinal Stability Characteristics of three Tilt-Wing VTOL Aircraft Designs Contract# DA 44-177-AMC-8(T)
Jan 1968
25 V/STOL’s Time Has Come by Edgar E. Ulsamer Air Force/Space Digest
Oct 1969
26 VC 400 Brochure VFW Munich Undated 27 XC-142A Lessons Learned Papers 1966 28 History of XC-142A Tri-Service Program 1967 29 NASA TN D-4344 Calculation of the Dynamic
Longitudinal Stability of a Tilt-Wing V/STOL Aircraft and Correlation with Model Test Flights
Feb 1968
30 Initial Development and Testing of a Tilt-Wing V/STOL by W.S. Longhurst Canadair
Undated
31 Potential Propeller Technology and Static Thrust Augmentation by George Rosen
May 17 1966
32 Royal Aero Society Volume 67 No. 630 Development of the Tilt-Wing Aircraft by John B. Nichols Hiller
Jun 1963
33 Vietnam/C-142 “What Can BE” Brochure LTV Nov 30 1956 34 Report No. R-219 Development of the US Army VZ 2
(Boeing Vertol -76) Research Aircraft Contract# Nonr 2136(00)
Aug 1963
141
35 Report No. 546.1 Proposal for the Design and Development of a Propelloplane Rescue Aircraft Hiller
Undated
36 Propelloplane Transport Study Summary Report Contract# Nonr 1637(00) Hiller
May 15 1956
37 Hiller VTOL/STOL Logistic Transport tilt Wing Propelloplane
Feb 1960
38 Miscellaneous Illustrations Tilt-Prop Aircraft Various
39 Tilt-Wing Applications by Blaine R. Parkin General Dynamics-Convair & Saul Bernstein Canadair
Sep 13-25 1969
TRI SERVICE TRANSPORT 72 1 Report No. 8069 VTOL Tri-Service Transport Model 175
– Summary McDonnell/Canadair Apr 3 1961
2 Report No. 8070 VTOL Tri-Service Transport Model 175 – Weight and Balance McDonnell/Canadair
Apr 3 1961
3 Report No. 8075 VTOL Tri-Service Transport Model 175 – Power Plant Installation and Fuel System McDonnell/Canadair
Apr 3 1961
4 Report No. 8076 VTOL Tri-Service Transport Model 175 – Hydraulic and Pneumatic Systems McDonnell/Canadair
Apr 3 1961
5 Report No. 8080 VTOL Tri-Service Transport Model 175 – Demonstration Program McDonnell/Canadair
Apr 3 1961
6 Report No. 8082 VTOL Tri-Service Transport Model 175 – Detail Specification McDonnell/Canadair
Apr 3 1961
7 Report No. 8083 VTOL Tri-Service Transport Model 175 – Contract Data Requirements McDonnell/Canadair
Apr 3 1961
8 Hiller Helicopter Model 1069 Rotor-Prop Convertiplane Undated 9 Briefing on the X-18 Research Aircraft and Future
V/STOL Aircraft Design Hiller Nov 11-13 1959
10 Memorandum Report on Safety Inspection – X-18 Tilt Wing VTOL Test Bed Contract# AF33(600)-32749 Hiller
Oct 27-28 1959
11 Report No. 101X90-2 The Kellett Direct Take-Off Airplane
Sep 1 1955 revA Sep 16 1955 revB Oct 4 1955
12 Report No. 106X90-3 Design Study Convertiplane Rotor System Contract# DA 44-177-TC-368 Kellett
Jan 1957
13 Report No. 106X90-1 The Kellett K-25 Flying Test Bed Feb 17 1956 revA Feb 24 1956 revB Feb 28 1956
14 Report No. G-113-36 The Model K-16B V/STOL Research Amphibious Aircraft: Summary Report
Mar 1967
142
Contract# NOa(s) 56-549c Kaman 15 Kaman K-16B Amphibian VTOL Presentation Undated 16 Report No. G-113-7 Estimated Flying Qualities of the
Kaman K-16B VTOL/STOL Aircraft Part II Dynamic Stability in Transitional Flight
Nov 20 1959
17 WADC TR 58-54 A Study of the Feasibility of Using a Semi-Rigid or Articulated Rotor System on a Tilt-Wing VTOL Airplane Part II Kaman
Apr 1958
18 Report No. R-219 Development of the US Army VZ-2 (Boeing-Vertol-76) Research Aircraft
Aug 1963
19 Boeing-Vertol Tilt Wing Development Program Undated
20 Report No. PR-378-20 Boeing-Vertol Model-137 Wind Tunnel Tests
May 22 1961
21 VHR-447 VTOL Tri-Service Transport Vol. 7 Summary report Part 1 Design Philosophy Hiller/Vought/Ryan
Undated
22 AFFTC Presentation – Introduction and Opening Remarks Oct 1966 23 History of the XC-142A Tri-Service Program 1967 24 XC-142A Lessons Learned Presentation Feb 5 1968 25 Report No. PDR-242-1 Part I Tri-Service VTOL Transport
Grumman Design 242 Proposal Summary Apr 3 1961
26 Report No. RAG-084-107 A Comparison of Downwash and Outflow from a Tilt-Wing Aircraft and a Helicopter Canadair
Feb 1971
27 Propeller Lifted Tilt-Wing VTOL Aircraft by Joseph Stuart III Hiller
Jan 23 1956
28 AIAA Paper No. 64-775 Survey of Significant Technical Problems Unique to V/STOL Encountered in the Development of the XC-142A by Lyman C. Josephs LTV
Sep 21-23 1964
29 XC-142A Brochure Undated 30 Report No. PDR-242-21 Grumman Design 242 Brochure Apr 17 1961 31 Ryan Reporter Vol. 22, No. 3 Tilt-Wing VTOL Nov 1961 32 NASA TN D-44 Force-Test Investigation of the Stability
and Control Characteristics of a 1/8-Scale Model of a Tilt-Wing Vertical-Take-Off-And-Landing Airplane
Aug 1959
33 NASA TN D-45 Flight Investigation of the Stability and Control Characteristics of a 1/8-Scale Model of a Tilt-Wing Vertical-Take-Off-And-Landing Airplane
Mar 1960
34 NASA TN D-390 Aerodymanic Characteristics of a ¼Scale Model of a Tilt-Wing VTOL Aircraft at High Angles of Wing Incidence
Sep 1960
TRI-SERVICE TRANSPORT & TILT ROTOR 73 1 VTOL-STOL Progress Report Canadair Jan 1961
2 Report No. 299-099-128 Technical Considerations for Low-Disc-Loading V/STOL Aircraft of the Fixed-Wing
Dec 23 1959
143
and Tilt-Wing Configurations Bell 3 Report No. AER-E1R-13341 VHR-447 Volume 3 –
Performance Data Report Hiller/Vought/Ryan Undated
4 Report No. AER-E1R-13355 VHR-447 Volume 14 – SAC Charts Hiller/Vought/Ryan
Undated
5 Report No. ES 40302 Tri-Service Transport – Book 2 Summary Report (Technical) Douglas
Mar 31 1961
6 Report No. ES 40308 Tri-Service Transport – Book 8 Stability and Control Douglas
Mar 31 1961
7 Report No. ES 40385 Tri-Service Transport – Increased Primary Mission Capability – Model D-828A and D-829B Douglas
Jun 8 1961
8 Report No. ES 40459 Tri-Service Transport – Configuration Comparison – Canard Turboprop vs. Tilt Wing Douglas
Aug 3 1961
9 Report No. NA61H-497 Tri-Service VTOL Transport Supplemental Technical Data and Design Analysis North American
Aug 21 1961
10 Report No. PDR-242-5 Design 242 Stability and Control Part I Grumman
Apr 3 1961
11 Report No. PDR-242-5 Design 242 Stability and Control Part 2 Grumman
Apr 3 1961
12 Report No. PDR-242-6 Design 242 Wind Tunnel Test Part 2 Grumman
Apr 3 1961
13 Report No. PDR-242-6 Design 242 Wind Tunnel Test Part 3 Grumman
Apr 3 1961
14 Report No. PDR-242-6 Design 242 Wind Tunnel Test Part 4 Grumman
Apr 3 1961
15 Boeing-Vertol Model-137 Outline of Oral Presentation Apr 6 1961 16 Report No. PR-378-2 Model-137 Detail Specification
Boeing-Vertol Apr 1961
17 Report No. PR-378-3 Model-137 Weight and Balance Boeing-Vertol
Apr 1961
18 Report No. PR-378-5 Model-137 Stability and Control Boeing-Vertol
Apr 1961
19 Report No. PR-378-9 Model-137 Power Plant Installations and Fuel System Boeing-Vertol
Apr 1961
20 Report No. PR-378-10 Model-137 Hydraulic and Pneumatic System Boeing-Vertol
Apr 1961
21 Report No. PR-378-11 Model-137 Electrical System Boeing-Vertol
Apr 1961
22 Report No. PR-378-12 Model-137 Structural Description and Design Data Boeing-Vertol
Apr 1961
23 Report No. PR-378-13 Model-137 Structural Tests Boeing-Vertol
Apr 1961
24 Report No. PR-378-14 Model-137 Effects of Dimensional Apr 1961
144
Limitations Boeing-Vertol 25 Report No. PR-378-15 Model-137 Demonstration Program
Boeing-Vertol Apr 1961
26 Report No. PR-378-16 Model-137 Maintenance and Support Boeing-Vertol
Apr 1961
27 Report No. PR-378-19 Model-137 Alternate Rigid Propeller Boeing-Vertol
Apr 1961
SERIES VIII: Vertical Lift Theory and Aerodynamics – Non-Helicopter, 1932-1989
Box File Description Date
TRI-SERVICE TRANSPORTS HARRIER 74 1 Conversion of the Vought-Hiller-Ryan Tilt-Wing Tri-
Service Transport into the Fowler System of Deflected Slipstream VTOL by Harlan D. Fowler
May 23 1962
2 Application of the Fowler Principle of VTOL to the Wind Tunnel Model of Vought Tilt-Rotor V-447 by Harlan D. Fowler
Jul 20 1962
3 V/STOL Commercial Transport 18 Passengers or 5000lbs. Cargo Model 70 by Harlan D. Fowler
Nov 1964
4 NASA TN D-444 Lateral Stability and Control Characteristics of a Four-Propeller Deflected-Slipstream VTOL Model Including the Effects of Ground Proximity
Jan 1961
5 V/STOL Research Program for Low Cost Tactical Aircraft Feb 26 1970 6 V/STOL Research Program for Low Cost Tactical Aircraft
(Second Edition) Apr 10 1970
7 NASA TN D-444 Lateral Stability and Control Characteristics of a Four-Propeller Deflected-Slipstream VTOL Model Including the Effects of Ground Proximity
Jan 1961
8 TS 3056 Thrust Vectoring in Combat Rolls-Royce Oct 1978 9 V/STOL and the CV US Naval Institute Proceedings
October 1970 Article Oct 1977
10 The Jet V/STOL Harrier British Aerospace Jul 1978 11 FTD-HC-23-0664-72 The Harrier Avionics System Jun 23 1972 12 Chartered Mechanical Engineer Article Ski-Jump Jet Sep 1978 13 The British Aerospace Harrier, Case Study in Aircraft
Design Jul 1978
14 TS 3080 Vectored Thrust Jet V/STOL Dec 1978 15 XV-6A Carrier Suitability Testing US Naval Institute
Proceedings April 1967 + Harrier Handout Apr 1967
16 Testing the Kestrel by I. A. Fisher Sep 1965
145
17 Kestrel/Harrier Sketches 1956 18 Report 68-978-002 Stability and Control of the X-14
VTOL Research Airplane Contract#AF33(600)-30837 Bell Sep 5 1958
19 V/STOL Articles and Pictures Aviation Week 1977 20 Report 68-981-002 X-14 VTOL Research Progress Report
2 Contract# AF33(600)-30837 Bell Sep-Oct 1955
21 Report 68-981-007 X-14 VTOL Research Progress Report 7 Contract# AF33(600)-30837 Bell
Jul-Aug 1956
22 X-14 Articles and Pictures 1957
23 Report DCR-219 An Investigation of the Thrust Augmentation Characteristics of Jet Ejectors Contract# DA44-177-322(T) Dynasciences
c.a. 1967
24 WSWD-211 RV-X Air Sea Rescue and Recovery Design Study SOR 187 Northrop
Mar 7 1962
25 WSWD-209 RVX System Cost Analysis Northrop Jan 25 1962 26 NOR-62-113 Analytical Study of the VTOL Suckdown
Phenomenon Northrop Jul 31 1962
27 NOR-60-269 Research Study of a NORAIR Proposed VTOL Cascade Nozzle Northrop
Aug 1960
28 NOR-62-23 A Preliminary Human Engineering Control-Display Analysis for a VTOL Weapons System Northrop
Jan 29 1962
29 D3-3900-1 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
30 D3-3900-2 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
31 D3-3900-3 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
32 D3-3900-4 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
33 D3-3900-5 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
34 D3-3900-6 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
35 D3-3900-7 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
36 D3-3900-8 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
37 D3-3900-9 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
38 D3-3900-10 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
39 D3-3900-11 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
40 D3-3900-12 Proposal for a Tri-Service VTOL Prototype Apr 3 1961
146
Transport Aircraft Boeing 41 D3-3900-13 Proposal for a Tri-Service VTOL Prototype
Transport Aircraft Boeing Apr 3 1961
42 D3-3900-14 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
53 D3-3900-14 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing
Apr 3 1961
44 D3-3900 Loose Drawings Boeing Apr 3 1961
V/STOL 75 1 NASA SP-406 Powered Lift Aerodynamics and Acoustics May 24-26 1976
2 TM 761-98 Summary of the Development Work on Combination Helicopter and Fixed Wing Aircraft (Convertiplane or Heliplane)
Apr 14 1948
3 Jet Propulsion for Convertiplanes 1952 4 The Economies of VTOL Systems Apr 29 1966 5 Flight in the Earth’s Atmosphere, 1975-1985 May 17 1966 6 Report DAC 56017 Vertical Takeoff and Landing
Transports Douglas Jun 7 1966
7 VTOL Transportation Group Jun 28 1966 8 NACA TN3629 Investigation of the Effects of Ground
Proximity and Propeller Position on the Effectiveness of a Wing with Large Chord Slotted Flaps on Redirecting Propeller Slipstream Downward for Vertical Takeoff
Mar 1956
9 US/UK Advanced Short Takeoff and Vertical Landing (ASTOVL) Program + Pictures & Articles
Jul 31-Aug 2 1989
10 ETP 167 C/66616VTOL Surveillance System for the US Army Volume 1 Lockheed/Bendix
Aug 17 1959
11 ETP 167 C/66616VTOL Surveillance System for the US Army Volume 2 Lockheed/Bendix
Aug 17 1959
12 AFWAL-TR-82-3059 Proceedings: Ejector Workshop for Aerospace Applications
Jun 1962
13 Ejector Workshop for Aerospace Applications Aug 2-5 1981 14 A Jet Flap Diffuser Injector Oct 12 1971 15 NB66-204 VTOL Fighter System Trends Northrop May 1966 16 RAC 1012 Variable Sweep Wing Plus V/STOL Part 1
Aerodynamic Design Aspects Republic Dec 12 1962
17 RAC 1012-1 Variable Sweep Wing Plus V/STOL Part 2 Takeoff and Landing Performance Republic
Dec 12 1962
18 64-543Z V/STOL Design Studies c.a. 1964 19 NA-56-1418 Dispersed Site Fighter Bomber Briefing
Charts Undated
20 Report 44238 VTOL Advanced Tactical Fighter Configuration and Propulsion Study
Apr 25 1963
21 Dornier VTOL Pictures 22 Lift Jet Installational Experience Nov 14-18 1965
147
23 US Army VZ-11 Liftfan V/STOL Aircraft Pamphlet Undated 24 XV-5A Lift Fan V/STOL Aircraft Flight Test
Accomplishments c.a.1966
25 V/STOL Pictures and Articles 1962-1963 26 Dornier-Post V/STOL (in German) 1969
Location 52, File 3 V/STOL Aircraft Summary Chart Undated
VERTICAL TAKEOFF 76 1 AD 34451 Report CVAL 132A Additional Low-Speed
Wind Tunnel Tests on a 1/7 Scale Model of the Ryan Model R-38 Helicopter: Volume I & II, Force Data: Investigation of Various Vertical Tails, Modified Wing Tips and Roll Jets Ryan
Dec 16 1953
2 NASA TN D-404 Hovering and Transitional Flight of a 1/5 Scale Model of a Jet Powered Vertical Altitude VTOL Research Aircraft Ryan
May 1961
3 Report 6954-7 General Flying Qualities in the Conventional Flight Regime Based on Flight Test Results: USAF Model X-13 Airplane Contract# AF33(600)-25895 Ryan
May 11 1956
4 Report 6955-1 Systems Analysis Report on USAF Model X-13 Airplane Stabilization System Contract# AF33(600)25895
Mar 15 1956
5 Report 6927-12 Performance Report; Rolls-Royce RA-2849 Turbojet as Installed in the X-13 Research Aircraft Contract# AF33(600)-25895
Aug 1 1954
6 Report 6910-25 Project MX-1976 Monthly Progress Report- X-13 – Vertical Takeoff Research Airplane (Ryan Model 69) Contract# AF33(600)-25895
Sep 1 1955
7 Report 6910-7 Estimated Aerodynamic Performance of USAF X-13 Airplane Contract# AF339600)-25895
1 August 1954
8 Tail Sitting Fighters, Article and Photos(X-13) Undated 9 D189-14797-1 Sea Control Fighter System Development
Proposal Boeing Jan 10 72
10 Convair XFY-1 “POGO” Photograph Undated 11 Proposal G.O. 20438 for Construction of Heliplane; Model
XGEH-1C General Electric Feb 8 1944
12 LR 26175 Final Report VTOL Strike RPV Study Contract# F33657-74-C0190 Lockheed
Dec 12 1973
13 Report CVAL 132B Additional Low-Speed Wind-Tunnel Tests on a 1/7 Scale Model of the Ryan Model R-38 To Investigate a Modified Vertical Tail and an Elevon to
Mar 12 1954
148
Increase Span 14 N79-10026 Study of Aerodynamic Technology for VSTOL
Fighter/Attack Aircraft – Vertical Attitude Concept May 1978
15 Wind Tunnel Photos of FW 860 Jet Fighter c.a. 1960 16 Photo Negatives of FW -860 Aircraft c.a. 1960 17 Photo Prints of FW-860 Aircraft 1960 18 Propeller Driven Vertical Altitude Takeoff and Landing
Concepts for Remotely Piloted Vehicles Dec 21 1976
19 Grumman Aerospace Horizons, Vol.12 no.3 Revolutionary V/STOL for Small Ships Magazine
1976
20 Bell Aerospace LFV and MFS Pamphlets 1964-1965 21 NASA Memo 5-7-59L Flight Investigation of Effects of
Transition, Landing Approaches, Partial-Power Vertical Descents and Droop-Stop Pounding on the Bending and Torsional Moments Encountered by a Helicopter Rotor Blade.
May 1959
22 NASA TN D-818 Method for Calculating Induced Velocities at the Blades of a Slightly Inclined Propeller with Constant Circulation
May 1961
23 NASA TN D-404 Hovering and Transition Flight of a 1/5 Scale Model of a Jet Powered Vertical-Altitude VTOL Research Aircraft
May 1961
24 Ryan Model 115C Vertical takeoff Aircraft Proposal Dec 3 1957 25 SNECMA Pamphlet for C400 P-2 ATAR Volant (in
French) May 14 1957
26 SNECMA Pamphlet for C.450 “Coleoptere ( in French) Jun 1967 27 “Nutcracker VTOL System Concept and Articles
Grumman 1976
28 XFV-1 VTOL Fighter, Articles and Pictures undated 29 Propeller Driven Vertical Altitude Takeoff and Landing
Concepts for Remotely Piloted Vehicles Dec 21 1976
30 NACA RM L51H13a Dynamic Stability and Control Characteristics of a Delta-Wing Vertically Rising Airplane Model in Takeoffs, Landings and Hovering Flight
Oct 9, 1951
31 NACA RM53G27 Wind-Tunnel Investigation at Low Speed of the Pitching Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft
Jul 23 1953
32 NACA RM SL54B03a Flight Determination of the Longitudinal Stability Characteristics of a 0.133 Scale Rocket Powered Model of the Consolidated Vultee XFY-1 Airplane Without Propellers at Mach Numbers from 0.73 to 1.19
Feb 14 1954
33 NACA RM SL53E13 Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertical Rising
May 20 1953
149
Aircraft 34 NACA RM SL53B20 Wind-Tunnel Investigation at Low
Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft
Feb 11 1953
35 NACA RM SL52L10 Investigation of Spinning and Tumbling Characteristics of a 1/20 Scale Model of the Consolidated Vultee XFY-1 Airplane in a Free Spinning Tunnel
Dec 10 1952
36 NACA RM SL54F11 Longitudinal Stability Characteristics of the Consolidated Vultee XFY-1 Airplane with Windmilling Propellers as Obtained from Flight of 0.113 Scale Rocket Propelled Model at Mach Numbers from 0.70 to 1.13
Jun 11 1954
37 NACA RM SL52I26 Stability and Control Flight Tests of a 0.13 Scale Model of the Consolidated Vultee XFY-1 Airplane in Takeoffs, Landings and Hovering Flight
Oct 1 1952
38 NACA RM SL53E18 Flight Investigation of the Stability and Control Characteristics of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Aircraft During Constant Altitude Transitions
May 21 1953
39 NACA RM SL54E07 Flight Tests of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Airplane with the Lower Vertical Tail Removed
May 12 1954
40 NACA RM SL54C19a Vertical Descent and Landing Tests of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Airplane in Still Air ( 2 copies)
Mar 16 1954
41 NACA RM SL53D01 Wind-Tunnel Investigation at Low Speed of the Yawing Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft
Mar 31 1953
42 NACA RM SL54E28 Takeoff and Landing Characteristics of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Airplane in Steady Winds
Jun 23 1954
43 NACA RM SL54B16a Flight Tests of a 0.13 Scale model of the Convair XFY-1 Vertically Rising Airplane in a Setup Simulating That Proposed for Captive Flight Tests in a Hanger
Feb 12 1954
44 P.F.Girard (Test Pilot) 2 Articles on Vertical Attitude Jet Powered Airplanes
1953
45 Report 239 Medical and Human Engineering Aspects of Flight In Ryan VTOL and STOL Aircraft
May 1959
46 NACA RM SL53E18 Flight Investigation of the Stability and Control Characteristics of a 0.13 Scale Model of the
May 21 1953
150
Convair XFY-1 Vertically Rising Aircraft During Constant Altitude Transitions
47 NACA RM L56H29a Dynamic Model Investigation of Two Tail-Sitter Vertically Rising Airplanes to Determine the Altitude Required to Approach Normal-Flight Conditions After Power Failure on Hovering Flight
Nov 9 1956
48 NACA RM SL53B20 Wind-Tunnel Investigation at Low Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft
Feb 11 1953
49 NACA RM SL53E13 Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertical Rising Aircraft
May 20 1953
50 Rolled Diagrams of Northrop VATOL Aircraft Apr 18 1978
V/STOL PROPELLER TECHNOLOGY CONCEPTS 77 1 Report No. LB-30684 Advanced STOL Assault &
Logistics Transport Model 2217 Douglas Aircraft Oct 12 1961
2 Report No. LB-30652 Advanced STOL Assault & Logistics Transport Model 2217A Douglas Aircraft
Apr 12 1962
3 Report 30959 STOL Turboprop Assault Transport Model 2252 Douglas Aircraft
Jul 20 1962
4 AIAA Paper No. 71-982 Canada’s STOL Program – A Progress Report by C.C. Halton Ministry of Transport (Canada)
Oct 25-28 1971
5 AIAA Paper No. 71-983 The Trends of the STOL System by M. Avramito Aerospatiale
Oct 25-28 1971
6 AIAA Paper No. 71-990 Performance Prediction and Evaluation of Propulsion-Augmented High Lift Systems by R.L. Gielow Lockheed Georgia
Oct 25-28 1971
7 STOL Aircraft Technology in Relation to Military/Civilian Requirements by Marvin D. Marks & James P. Caldwell McDonnell Douglas
Sep 23 1969
8 AIAA Paper No. 71-578 Douglas Paper 5928 Recent Developments in Jet Flap Theory and its Application to STOL Aerodynamic Analysis by M.L. Lopez & C.C. Shen McDonnell Douglas
Jun 21-23 1971 rev. Jul 23 1971
9 Report LR 23916 60-Passenger STOL Test Aircraft for NASA Flight Research Center Lockheed-California
Sep 2 1970
10 Report MDC 69-027 (Paper C-WP 2.1) Simulation of STOLport Runway and Gate Operations by J.E. Hosford & J.R. Lovit McDonnell Douglas
Nov 10-12 1969
11 Report AERO.2645 Theoretical Analysis of a Gust Alleviator Used on a Lancaster Aircraft and Comparison
Jan 1961
151
with Experiment by J.K. Zbrozek British Ministry of Aviation
12 Report MCL-927/1+2 The STOL Dornier Jun 26 1961 13 AEREON Dynairship – History and Articles 1973 14 NASA SP-320 STOL Technology Oct 17-19 1972 15 USAAMRDL TR 73-34A Summary of Propeller Design
Procedures and Data Volume I – Aerodynamic Design and Installation
Nov 1973
16 USAAMRDL TR 73-34A Summary of Propeller Design Procedures and Data Volume II – Structural Analysis and Blade Design
Nov 1973
17 USAAMRDL TR 73-34A Summary of Propeller Design Procedures and Data Volume III – Hub, Actuator and Control Designs
Nov 1973
18 NACA ARR No. 3E19 Formulas for Propellers in Yaw and Charts of the Side-Force Derivative
May 1943
19 NACA ACR No. L4I19 The Theory of Propellers II – Method for Calculating the Axial Interference Velocity
Nov 1944
20 NACA ACR No. L4J10 The Theory of Propellers III – The Slipstream Contraction with Numerical Values for Two-Blade and Four-Blade Propellers
Nov 1944
21 NACA ARR No. 3L09 Propellers in Yaw Dec 1943 22 NACA RB No. 3L02 Proposal for a Propeller Side Force
Factor Dec 1943
23 NACA ACR No. L5F30 Effect of the Lift Coefficient on Propeller Flutter
Jul 1945
24 NASA TN D-434 Low-Speed Investigation of a Full-Span Internal-Flow Jet-Augmented Flap on a High-Wing Model with a 350 Swept Wing Aspect Ratio 7.0
Aug 1960
25 AEDC-TR-72-139 Simulation of a High Disc Loading Free Propeller in a Cross Flow by the Vortex-Lattice Method
Nov 1972
26 WADC TR 58-564 Study of Propeller Controls for VTOL Aircraft Applications
Dec 31 1958
27 Q-FAN Generalized Performance, Noise and Weight Data for Sev Applications
Jan 25 1972 rev Jul 15 1972
28 NASA CR111842 Prop-Fan Results of Initial Prop-Fan Model Acoustic Testing Volume I – Discussion
Dec 4 1970
29 NASA CR111842 Prop-Fan Results of Initial Prop-Fan Model Acoustic Testing Volume II Appendices B thru F
Dec 4 1970
30 NASA CR111956 Results of Prop-Fan/STOL Wing Acoustics Tests
Jul 29 1971
31 Hamilton Standard Letter to Aeronautical Engine Laboratory , Naval Air Engineering Center
Sep 9 1966
32 USAAVLABS TR 68-33 Extracts Feasibility Study for Advanced V/STOL Propeller Technology
Undated
152
33 Report No. 8820-2 Propeller Static Thrust Ryan Aeronautical Co.
Aug 24 1955
34 Propeller and Gearbox Propulsion Technology Forecast (Rough Draft)
1985
35 DOWTY Variable Pitch Fans with Cover Letter Nov 12 1971 36 Q-FAN Performance and Scaling Data for Two Q-FAN
Design Undated
37 Prop-Fan Generalized Performance Hamilton Standard May 18 1970 rev1 Aug 28 1970 rev2 Jun 1973
38 Physics and Flow of a Propeller and Rotor System by Paul E. Williams MDC
1970
39 Physics and Flow of a Propeller and Rotor System Supplement 1 by Paul E. Williams MDC
May 11 1970
LIFT-FAN 78 1 Lift Fan Flight Research Aircraft Program Quarterly
Technical Progress Report No 1 Contract# DA44-177-TC715 GE
Mar 31 1962
2 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 2 Contract# DA44-177-TC715 GE
Jun 30 1962
3 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 3 Contract# DA44-177-TC715 GE
Sep 30 1962
4 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 4 Contract# DA44-177-TC715 GE
Dec 31 1962
5 Lift Fan Flight Research Aircraft Program X353-5B Propulsion System Flightworthiness Test Report Volume 1 Contract# DA44-177-TC-715 GE
Jan 1963
6 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 5 Contract# DA44-177-TC715 GE
Apr 30 1963
7 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 6 Contract# DA44-177-TC715 GE
Jun 30 1963
8 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 7 Contract# DA44-177-TC715 GE
Sep 30 1963
9 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 8 Contract# DA44-177-TC715 GE
Dec 31 1963
10 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 10 Contract# DA44-177
Jul 1964
153
TC-715 GE 11 Lift Fan Flight Research Aircraft Program Quarterly
Technical Progress Report No 11 Contract# DA44-177TC-715 GE
Oct 1964
12 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Volume I – Description of Technical Program
May 1961
13 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Volume III – Aircraft Specification NS-145 (Preliminary)
May 1961
14 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Powered Model Tests and Data Analysis
Jun 1961
15 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Refinement and Substantiation of Technical Proposal
Jul 1961
16 An Analysis of a Two-Dimensional Propulsion Wing by Galen Hu Stanford University
1971
17 XV-5A Contractor Flight Test and Evaluation 1964-1965 18 Report No. 62B133 Operational V/STOL Ryan Jan 1 1963 19 Report AD 657 992 X353-5B Propulsion System
Flightworthiness Test Report Volume 1 Contract#DA44177-TC-715 GE
Jan 1963
20 DADD TR 60-371 Volume II Study of Submerged Fan Type VTOL Aircraft Contract#AF33(616)-6605 GE
Mar 1960
21 NASA CR-761 Lift Fan Technology Studies Contract# NAS 2-3077
Apr 1967
22 Vanguard Model 3 VTOL/STOL Rescue Aircraft -Aircraft Characteristics
Undated
23 Appraisal of Comparative Evaluation Fan-In-Wing versus Adam II LTV Vought
Jan 10 1964
24 Lift Fan Thrust Augmentation Aircraft – Illustrations, Articles and Photos
1964-1965
25 Report PR-316 Proposal for a Wind Tunnel Program to Study “Jet Wall” Applications to Wing-Submerged Ducted Fans Vertol
Jun 17 1959
26 NASA TN D-731 Induced Interference Effects on Jet and Buried-Fan VTOL Configurations in Transition
Mar 1961
27 Report 25-X-2 Vanguard Heavy Lift System for Transportation of Very Large Military Equipment
Jan 15 1962
28 Feasibility Study of a M3 Fighter Airplane with Lift Fans for V/STOL Operations Ryan
Jan 17 1963
29 Report No. 62B136 Planning Proposal for XV-5A V/STOL Operational Evaluation Aircraft – Ryan Model 167
Dec 12 1962
154
30 Report No. 63B045 V/STOL Weapon System Development Plan Ryan & Raytheon
May 10 1963
31 Report No. 290-70-2 Proposal for F-104 Fan Design Study – Ryan Model 190D
May 28 1965
STRUCTURES/AERODYNAMICS 79 1 Report #25 Flight Research Investigation of Laminar
Separation of a High Lift Boundary Layer Control Airplane by Dezso Gyorgyfalvy Mississippi State Univ.
Jun 26 1959
2 Model 34 Aerodynamic Report 158 Analysis of Model 34 Wind Tunnel Tests Beech
Dec 27 1945
3 Model 38 Aerodynamic Report 238 Analysis of Model 38 Wind Tunnel Tests Beech
Jun 3 1947
4 Model 305 Report No. 951 Flight Test Performance Cessna
Mar 17 1950
5 Report F-TS-668-RE The Influence of Fuselage and Wing Sweepback on the Range and Speed of Turbo-Jet Airplanes by Siegfried Gunter (Heinkel) (Germany)
Sep 1946
6 Airpower Journal Air Occupation –Asking the Right Questions by MAJ Marc K. Dippold USAF
1997
7 NASA CR-137894 Civil Uses of Remotely Piloted Vehicles (Final Report) Contract# NAS 2-8935
Jul 1976
8 NASA CR-137895 Civil Uses of Remotely Piloted Vehicles (Summary Report) Contract# NAS 2-8935
Jul 1976
9 Paraglider Recovery Systems by Francis M. Rogallo NASA
Apr 30-May 2 1962
10 NASA Research on Flexible Wings by Francis M. Rogallo NASA
Apr 3-6 1967
11 Parawings for Astronautics by Francis M. Rogallo NASA Sep 10-12 1963 12 An Aviation Milestone – Man Achieves the Age Old Goal
of Self-Powered Flight by Peter B.S. Lissaman The Gossamer Condor
1977
13 Report No. 5069 Performance Flight Testing Methods in Use by the Flight Section AAF Technical Service Command, Wright Field
Jan 15 1944
14 AAF Inspector’s Familiarization Manual – Midwest Procurement District, Material Command
Mar 1 1943
15 AAF TR 5242 Stability and Control Flight Test Methods Jul 14 1945 16 Report ANC-18 Design of Wood Aircraft Structures Jun 1944 17 Report ANC-19 Wood Aircraft Inspection and Fabrication Dec 20 1943 18 DR Report No. 1139 Aircraft Design Analysis Methods as
Employed by The Research Division of BuAer Oct 6 1949
19 Report TN-70-AM-01 Drag Estimation Procedures for Preliminary Design Configuration Studies General Dynamics
Mar 23 1970
20 ANA Bulletin No. 421 Atmospheric Properties – Extreme Sep 24 1953
155
Cold and Hot; Standard for Aeronautical Design 21 ANC-5 Strength of Metal Aircraft Elements Mar 1955 22 ANC-5a Strength of Metal Aircraft Elements Rev May 1949 23 AAF TR 5193 A Method for Estimating Gas Turbine – Jet
Airplane Performance Mar 8 1945
24 Simplified Methods of Horsepower Correction for Single-Speed and Two-Speed Engines Wright Aeronautical Corp.
Apr 1944
25 Engineering Notes Wright Aeronautical Corp. Undated 26 Homebuilt Airplanes – Articles Various 27 Bede 5 Aircraft Information Various
28 “Toward New Horizons” A Report to General of the Army H.H. Arnold by Thomas Von Karman
Nov 7 1944
29 FTD-TT-65-1573 Aircraft Construction (Selected Parts) (Russian)
Undated
30 Ocean Surveillance and Control Boeing Nov 1972 31 The Potential Contribution of Subsonic Aviation to Short
Haul Transportation by R.H. Miller MIT Apr 1967
32 FS-26 Concept (IN German) Undated 33 The De Havilland Dragon – Six Apr 26 1934 34 NACA Report L4D18 Stability of a Body Stabilized by
Fins and Suspended from an Airplane Apr 1944
35 NACA Memorandum Report of Oct 1942 A Flight Investigation of the Stability of a Towed Body
Oct 1942
36 NACA Report 3K17 Theoretical Analysis of the Lateral Stability of a Glider Towed by Twin Parallel Tow Lines
Nov 1943
37 Project 72011461 Advanced Systems Concepts Lockheed May 31 1972 38 Report TM 73-38 PTT Teleplane Progress Report Apr 1973 39 Report ST-CS-01-147-72 DIA Task T70-01-13
Aerodynamics (Research and Development) Free World Sep 21 1972
40 Unmanned Aerial Vehicle (UAV) Master Plan 1992 Apr 15 1992 41 Unmanned Aerial Vehicle (UAV) Master Plan 1993 Mar 31 1993 42 Aircraft Photos – Miscellaneous Most WW II Undated
VTOL 80 1 FSTC-HT-23-967-68 Vertical Landing and Takeoff
Aircraft (USSR) 1966
2 Symposium on Vertical and Short Take-Off and Landing Aircraft Part 2 (NATO)
Jun 1960
3 Report Beyond the Horizon Flight in the Atmosphere, 1975-1985 Volume III Vertical Takeoff and Landing
Jan 1967
4 Report D8-2194-1 Drag Estimation of V/STOL Aircraft Boeing
Sep 20 1968
5 Research and Development of Advanced Rotorcraft Concepts by Evan A. Fradenburgh Sikorsky
Feb 17-19 1969
6 Systems Considerations in VTOL Notes by C.C. Wood May 17 1966
156
Sikorsky 7 Foreign VTOL Progress Draft and Slides Undated 8 Contributions of Bell Helicopter Company to Helicopter
Development by Bartram Kelley Undated
9 US Navy VSTOL Technology Assessment Volume II Final Report
Jun 1975
10 Deployable Airfoil Structure and Application Parsons Corp.
Undated
11 Report PB 111633 Special Types of Rotary Wing Aircraft Volume II Contract# W33-038-ac-21804(20695)
1954
12 Joint DOD-NASA-DOT Study – R&D Contributions to Aviation Progress (RADCAP) Volume II Appendices 1 thru 9
Mar 1972
13 NASA V/STOL and STOL Conference – Program and Slides
Apr 4-5 1966
14 AHS 1st National V/STOL Aircraft Symposium Supplement
Nov 3-4 1965
15 Report 60WWR-930 SR-175 V/STOL Logistic Aircraft Study Vol. I Appendix Contractor Report Summaries
Jun 1960
V/STOL AERODYNAMICS 81 1 Ryan Reporter Vol.22 No.3; Vol.23 No.1; Vol 23 No.2 Nov 1961- Mar
1962 2 Project No. AU-419-63-ASI Test and Evaluation of
Combat Functions May 1963
3 AFFDL TM-73-4-PTC Assessment of VTOL Concepts for RPV Applications
Jan 17 1973
4 Report No. 5 Development of Methods for Predicting V/STOL Aircraft Characteristics Contract# Nonr 3099(00)
Apr 15 1960
5 AFFDL TM-73-100-PTB Design Investigation of Three Vertical Landing Concepts for RPV Application, Phase II
Aug 1973
6 Report PR-107 Proposal for the Advancement of Techniques for Very Large Vertical Lift Systems Vanguard Air and Marine Corp.
Jan 15 1962
7 Report PR-316 Proposal for a Wind Tunnel Program to Study “Jet Wall” Applications to Wing-Submerged Ducted Fans Vertol
Jun 17 1959
8 NASA TN D-4448 Large-Scale Wind-Tunnel Tests of a Deflected Slipstream STOL Model with Wings of Various Aspect Ratios
Mar 1968
9 Report TR-29 An Experimental Investigation of an External Aerodynamic Diffuser Contract# N00014-68-A0512 West Virginia University
Apr 1971
10 Report 64-1 Hiller Model 1117 Light Armed Reconnaissance V/STOL Aircraft with Associated Documentation
Mar 1964
157
11 Report 64-1 Hiller Model 1117 Light Armed Reconnaissance V/STOL Aircraft Reference 2
March 1964
12 Air Products Co. Proposal VTO Lift & Transport Vehicle (Heavy Duty)
Undated
13 Air Products Co. Scientific & Technical Brochure Undated 14 Report APR-64-4 Investigation of the Process of Energy
Transfer from an Intermittent Jet to Secondary Fluid in an Ejector-Type Thrust Augmenter – Interim Summary Report Covering the Period Oct 30 1962 to Mar 31 1964 Contract# Nonr 3082(00)
Mar 31 1964
15 Report No. 298 Hiller Pulse Reactor Lift-Propulsion Engine
Feb 1962
16 Report ARL 71-0236 The Performance Characteristics of the 7/10’s Nozzles in the Five Foot Single Channel Vertical Ejector
Oct 1971
17 Report No. 2099-928003 A Generalized Experimental Study of Inlet Temperature Rise of Jet V/STOL Aircraft in Ground Effect Contract# BuWeps N600(19)63320
Apr 5 1966
18 NASA TN D-372 A Flight Study of the Conversion Maneuver of a Tilt-Duct VTOL Aircraft
Nov 1960
19 WADC TR 58-630 Study of Propeller Controls for VTOL Aircraft Applications (Item III-Final TR) Contract# AF 33(616)5294
Undated
20 Report PSAD-78-61 Status of the Navy’s Vertical Short takeoff and Landing Aircraft
Feb 23 1978
21 V/STOL Type A Technical Briefing Lockheed-California Jul 26 1977 22 Ryan Reporter 1964 23 Report LR 19755 Advanced Transport Aircraft 1975-1985
Lockheed-California May 19 1966
24 Report NA-70-327-1 VTOL Integrated Flight Control System R&D Final TR Volume I Technical Summary
1969
25 Report R60FPD148 SR-175 VTOL/STOL Logistics Aircraft Volume II – TR Parametric Study
Mar 1960
26 Report ASD-TDR-62-578 Suppression of Jet Noise with Emphasis on the Near Field
Feb 1973
27 Report EWR-Nr. 4-66 Experience with the Flight Test Instrumentation System of the VTOL Aircraft VJ 101 C.
Mar 21-24 1966
28 NAVAIR-1R-76 USN/FMOD FRG VAK-191B Joint Flight Test Program Final Report Volume No. 1 Summary
Aug 1976
29 V/STOL Handling Qualities Criteria Compared with Flight Test Results of the V/STOL – Supersonic Fighter VJ 101 C and the V/STOL – Transport Aircraft DO-31 E Dornier-MBB
Sep 28-Oct 1 1971
30 Alternate Designed/Propulsion Concepts for a Low-Signature, Small Military transport by Charles Patterson , Jon Champion & Lt. Ken Sebek Wright Labs, WPAFB
Undated
158
31 Using New Technology – The AV-8B Harrier II by Stan Lewis Rockwell
Undated
32 Report ER 4222 New Surveillance Aircraft System Parametric Study 1965-1970 Time Frame
Feb 1 1960
33 Report 64-1 Hiller Model 1117 Light Armed Reconnaissance V/STOL Aircraft Reference 3
Mar 1964
34 Report 14647 CL-519 Lockheed V/STOL Utility Aircraft Undated 35 Report 64-1 Hiller Model 1117 Light Armed
Reconnaissance V/STOL Aircraft Reference 1 Mar 1964
36 WRDC-TR-89-6011 Special Operations Forces (SOF) Transport Aircraft Study Volume I: Executive Summary
Jan 1990
37 WRDC-TR-89-6011 Special Operations Forces (SOF) Transport Aircraft Study Volume II: Technical Analysis
Jan 1990
38 WRDC-TR-89-6012 Special Operations Forces (SOF) Transport Aircraft Study Volume I: Executive Summary
Jan 1990
39 WRDC-TR-89-6012 Special Operations Forces (SOF) Transport Aircraft Study Volume II: Technical
Jan 1990
40 AIAA Papers No. 71-576: No. 74-995 1971/1974 41 SURVIAC-TR-91-008 Special Operations Aircraft
Technology Assessment – V/STOL Compendium and Database
Dec 1990
VTOL RESEARCH 82 1 Report No. G-113-1 Design Detail Specification for Model
K-16B Wind Tunnel Model Contract# NOa(s) 56-549c Kaman
Jun 30 1958
2 Report 9433 Proposal for Study of VTOL Day Fighter Lockheed
Oct 9 1953
3 Report No. G-113-3 Pilot Compartment Mock-Up review Kaman
Feb 12 1959
4 Report No. G-90 Experimental Investigation of a Trailing Edge Flap as a Means of Propulsive Rotor Cyclic Pitch Control of VTOL/STOL Aircraft Contract# NOA(S) 56549C Kaman
Apr 27 1956
5 Report No. R-183A An Alternate Proposal for the Design, Construction and Test of the K-16B VTOL/STOL Research Aircraft Kaman
Jan 29 1958
6 Report No. G-111-1 An Experimental Investigation of a Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part 1 Design and Planning Contract NOa(s) 56549c Kaman
Jun 15 1958
7 Report No. G-111-2 An Experimental Investigation of a Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part II Test Operation and Structural Evaluation
Nov 5 1958
8 Report No. G-111-3 An Experimental Investigation of a Aug 1958
159
Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part III Controllability Contract# NOa(s) 56-549c Kaman
9 Report No. G-111-4 An Experimental Investigation of a Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part IV Performance Contract# NOa(s) 56-549c Kaman
Sep 1958
10 Report No. G-113-2 Methods of Analysis for Free Flight Loading Conditions Contract# NOa(s) 56-549c Kaman
Dec 12 1958
11 Report No. G-113-4 Estimated Flying Qualities of the Kaman K-16B VTOL/STOL Aircraft Contract# NOa(s) 56-549c Kaman
Feb 20 1959
12 Report No. G-113-5 K-16B Calculated Airloads Report Contract# NOa(s) 56-549c Kaman
Jul 15 1959 Rev.A Jan 6 1960
13 Report No. G-113-6 Flutter Analysis of the Kaman K-16B VTOL/STOL Research Aircraft Contract# NOa(s) 56-549c Kaman
Oct 15 1959
14 Report No. G-113-8 Model K-16B Estimated Weight and Balance Contract# NOa(s) 56-549c Kaman
Dec 18 1959
15 Report No. G-113-10 Mechanical Instability Analysis of the Kaman K-16B VTOL/STOL research Aircraft Contract# NOa(s) 56-549c Kaman
Jan 15 1960
16 Brochure No. B-12 The Model K-16B Research Amphibian Contract# BUAER NOa(s) 56-549c Kaman
Oct 30 1959
17 Kaman K-16B Hover Undated 18 Report No. 10699 Flight Tests of the Lockheed XFV-1 Jun 15 1955 19 M=1.2 Fighter Attack Technology Lockheed May 31 1972 20 Report No. 9122 Aerodynamic Characteristics of the
Lockheed XFV-1 in the Hovering and Transition range Lockheed
Jun 1 1953
21 Turboprop Propulsion/Control System for Transonic V/STOL Military Aircraft Lockheed-California
Feb 15 1972
22 AERO Report 902 Wind-Tunnel Tests of a 1/16-Scale Model of a Rotatable-Wing Seaplane Part II – Longitudinal and Lateral Characteristics
Dec 1959
23 V/STOL Propulsive Rotor – Recommendations for Further Research Kaman
Dec 5 1968
24 Report LR 25170 Proposal for Turboprop Propulsion/Control System for Transonic V/STOL Aircraft Lockheed-California
Mar 1972
25 Report LR 24441-1 Research Program for M=1.2 V/STOL Tactical Fighter Lockheed-California
Apr 6 1971
26 Report No. 8072 VTOL Tri-Service Transport Model 175 Stability and Control McDonnell/Canadair
Apr 3 1961
160
27 FDV 9-7-13 VC-400 Cargo and Passenger Aircraft Undated 28 Non-Rotary Wing Aircraft research by John P. Rabbott, Jr.
Sikorsky Jul 11 1963
29 Report 224-41-61 Analysis of a Wind Tunnel Test of a 0.08 Scale Tilt-Wing VTOL Model, NACAL #59
Apr 28 1961
30 Report No. 8077 VTOL Tri-Service Transport Model 175 Structural Description and Design Data McDonnell/Canadair
Apr 3 1961
31 Tilt-Wing Photos Undated
HIGH LIFT DEVICES 83 1 Louis Breguet 1911-1961 Commemorative Booklet (in
French) May 15 1961
2 Breuget Aviation Facilities and Aircraft Brochure C.A. 1970 3 Reports and Memoranda No. 1520 Air Torque on a
Cylinder Rotating in an Air Stream by A. Thom & S.R. Sengupta U. of Glasgow
Oct 22 1932
4 Reports and Memoranda No. 1623 On the Effect of Discs on the Air Forces on a Rotating Cylinder by Alexander Thom U. of Glasgow
Jan 5 1934
5 USAAVLABS TR 66-39 Principles for Improving Structural Crash Worthiness for STOL and CTOL Aircraft
Jun 1966
6 Custer Channel Wing, Information Submitted to W.J. Boyne by B. Lindenbaum
Nov 30 1976
7 Custer Channel Wing – Assessment Jan 1971 8 Custer Channel Wing – Correspondence 1971 9 STOL – Miscellaneous Articles and Photos C.A. 1970 10 Hispano-Suiza Flexible Transmission System for Breguet
943 Aircraft Jul 17 1962
11 TR No. RCF-1 A Study of the Aerodynamic Characteristics of a High-Lift Device Based on a Rotating Cylinder and Flap Contract# NONR-225(54) (NR 212217) Stanford Univ.
Sep 1961
12 ER No. 249 Evaluation of the Performance, Stability and Control of the Helio Coutier Airplane – Progress Report for Oct 1956 Contract# DA 44-177-TC-369 Univ. of Wichita
Nov 1956
13 ER No. 252 Evaluation of the Performance, Stability and Control of the Helio Coutier Airplane – Progress report for Nov 1956 Contract# DA 44-177-TC-369 Univ. of Wichita
Dec 1956
14 ER No. 260 Evaluation of the Performance, Stability and Control of the Helio Coutier Airplane – Progress report for Dec 1956 Contract# DA 44-177-TC-369 Univ. of Wichita
Jan 1957
15 Report No. 1 Lift Characteristics of Wings Extending Through Propeller Slipstreams Contract# Nonr 2388(00) VRC
Sep 1958
161
16 Report D210-10201-1 STOL High Lift Design Study Contract# USAF F33615-70-C-1277 Boeing
1971
17 An Investigation of the Feasibility of a Common Boundary Later Control System for High-Lift and Low-Drag on an Airfoil Section by Sean C. Roberts Miss. State Univ.
Jun 1966
18 Research Report No. 66 (USAAVLABS TR 66-36) Flight Evaluation of a Distributed Suction High-Lift Boundary Layer Control System on a Modified L-19 Liaison Aircraft Contract# DA 44-177-AMC-265(T) Miss. State Univ.
May 1966
19 STOL Report Issue 2 Fairchild Hiller Aircraft Division Apr 1966 20 Executive STOL from FLYING Mar 1962 21 Breguet STOL Transport 941 Photo Booklet Undated 22 New-Generation Airlifter (YC-14) Brochure Boeing Undated 23 deHavilland High Lift Vol.2, No.2 Feb-Mar 1978 24 STOL Airplanes – A New Approach to Air Transport by
R.A. Darby Fairchild Aircraft Division Nov 8 1955
25 AMST: Tactical Airlift Into the 21st Century (YC-14) Boeing
Undated
26 ASE 700837 Designing the OV-10A Forward Air Control and Light Attack Aircraft by Jack E. Wagner & Richard J. Arnold North American Rockwell Corp.
Oct 5-9 1970
27 Breguet 941 Manufacturer’s Model Specification Jan 15 1962 28 Breguet 941/942 Photos and Brochure Undated 29 Breguet 941S (942) Data and Drawings Undated 30 Breguet 941 Brochure Jun 1959 31 Report No. 9732 Model 188E (Breguet 941) STOL Assault
Transport with Takeoff and Payload Slide-rule May 24 1963
32 ASE S259 The Lockheed BLC Hercules – A Practical STOL Transport (with Specs. And Photo of C130B) by F.N. Dickerman & C.F. Branson Lockheed- Georgia
Nov 1 1960
33 AIAA Paper No. 71-993 Factors in STOL Flight Control Configuration by William P.A. Harris Boeing
Oct 25-28 1971
34 Autogiro Articles 1990-1994 35 SAE 960C Determination of Breguet 941 STOL Aircraft
Transition Velocities with Various Flap Settings by Harlan D. Fowler
Jan 11-15 1965
36 Report PDP-15 GL-200 STOL Army Utility Transport Lockheed-Georgia
Jan 16 1959
37 Report 43176 Small Armed Reconnaissance Aircraft D855 Douglas Aircraft
Nov 24 1962
38 Proposal for Converting the Ryan VZ-3RY Aircraft into the Fowler System for Comparative V/STOL Flight Performance Data by Harlan D. Fowler
Aug 1954
39 A VTOL Airplane for Commercial Uses Allison 250 HP by Harlan D. Fowler
Nov 10 1960
162
40 NASA TN D 4489 Large-Scale Wind-Tunnel Tests of an Airplane Model with Two Propellers and Rotating Cylinder Flaps
Mar 1968
41 NASA CR 2135 Flight Tests of a Rotating Cylinder Flap on a North American Rockwell YOV-10 Aircraft
Nov 1972
42 Research Report No. 19 Practical High Lift Systems Using Distributed Boundary Layer Control by J.J. Cornish III Miss. State Univ.
Jan 26-29 1959
43 USAAVLABS TR 70-37 XV-11A Flight Test Program Feb 1971 44 Development of Distributed Suction High-Lift STOL
Aircraft by Sean C. Roberts Miss. State Univ. Nov 16 1965
45 ER No. 235 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Aug 1956 Contract# DA 44-177-TC-370 Univ. of Wichita
Sep 1956
46 ER No. 255 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Nov1956 Contract# DA 44-177-TC-370 Univ. of Wichita
Dec 1956
47 ER No. 261 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Dec 1956 Contract# DA 44-177-TC-370 Univ. of Wichita
Jan 1957
48 ER No. 268 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Mar 1957 Contract# DA 44-177-TC-370 Univ. of Wichita
Apr 1957
49 Delay of the Stall by Suction Through Distributed Performations by A. Raspet, J.J. Cornish III & G.D. Bryant Miss. State Univ.
Jan 23-26 1956
50 STOL Articles Various 51 Progress Report from Nov 1 1958 to Dec 31 1958
Contract# Nonr 978(01) Jan 5 1959
52 Examination of Some of the Problems Involved in the Design of Propeller-Driven Vertical-Take-Off Transport Airplanes by M.O. McKinney, R.E. Kuhn & J.B. Hammack NACA
Jan 23-26 1956
53 Some design Problems of Tilt Wing VTOL Aircraft by W.Z. Stepniewski Vertol
Oct 4 1957
54 NASA Memorandum 1-16-59L Semiempirical Procedure for Estimating Lift and Drag Characteristics of Propeller-Wing-Flap Configurations for Vertical-and-Short-take-Offand –Landing Airplanes
Jan 1961
55 NASA TN D-5742 Large-Scale Wind-Tunnel Tests of an Airplane Model with Four Propellers and Rotating Cylinder Flaps
Apr 1970
163
56 NASA TN D-1430 Longitudinal Trim Characteristics of a Deflected Slipstream V/STOL Aircraft During Level Flight at Transition Flight Speeds
Oct 1962
57 NASA TN D-1891 Some Flight Characteristics of a Deflected Slipstream V/STOL Aircraft
Jul 1963
58 ASE 700811 Synthesis of Future High Lift Systems by Richard Scherrer Lockheed-California
Oct 5-9 1970
VTOL/GETOL GROUND EFFECTS 84 1 Report No. 203-P-1 Proposal for Test Evaluation of a
Flying Platform for the Individual Soldier by E. K. Liberatore
Feb 6 1958
2 GETOL Presentation Charts General Dynamics May 1963 3 Symposium on Ground Effect Phenomena Princeton Univ. Oct 21-23 1959 4 Ground Effect Vehicles – Photos and Articles Various 5 TR 011-2 Static Stability of Ground Effect Machines –
Thick Jet Theory by J.D. Lin Contract# Nonr-3189(00) Jun 1 1961
6 NASA TN D-660 Effects of Various Arrangements of Slotted and Round Jet Exits on the Lift and Pitching-Moment Characteristics of a Rectangular-Base Model at Zero Forward Airspeed
Feb 1961
7 NASA TN D-756 Effects of Geometric Variations on Lift Augmentation of Simple-Plenum-Chamber Ground-Effect Models
Apr 1961
8 AFFDL-TR-72-87 A Study of Air Cushion Landing Systems for Recovery of Unmanned Aircraft
Jul 1972
9 Aero Report 923 Theory of the Annular Nozzle in Proximity to the Ground
Jul 1957
10 Report No. 349 Design of Wing Sections for Use Near the Ground by T. Strand & J.J. Brainerd Air Vehicle Corp. Contract# Now 64-0349-f
Mar 1965
11 Report No. 208A90-1 On the Aerodynamic Design of Propellers and Duct Systems for Ground Effect vehicles Contract# DA 44-177-TC-524
Jan 15 1962
12 Aero Report 947 Preliminary Study of the Hovering Performance of Annular Jet Vehicles in Proximity to the Ground
Aug 1958
13 Aero Report 954 Comparison of Experimental and Theoretical Design Parameters of a 6-inch-diameter Annular Jet Model with a Jet Angle of -45o Hovering in Proximity to the Ground; and Experimental Results of Forward Flight at Zero Angle of Attack
May 1959
14 Report No. AR 581-R Aerodynamic Theory of the Annular Jet Part I Contract# Nonr-2398(00) and Nonr-2747(00)
Dec 1958
15 NASA TM X-67876 A Nuclear Powered Air Cushion Freighter for the 1980’s
Oct 17-21 1971
164
16 Report No. NA 59H-715 Analysis of NAA Tests of ground-Effect machine Concept North American
Jan 8 1960
17 IAS Proceedings Hydrofoils and Air Cushion Vehicles Sep 17-18 1962 18 SAE 133A Basic Principles of Air Cushion Vehicles by
Gabriel D. Boehler Aerophysics Company Jan 11-15 1960
19 Forward Flight Characteristics of Annular Jets by Garriel D. Boehler Aerophysics Company
Oct 21-23 1959
20 Aero Report 966 Report 1371 A Preliminary Design Technique for Annular-Jet Ground-Effect Machines (GEM’S) TED No. TMB AD-3242
Sep 1959
21 SAE 508A Some Aerodynamic Aspects of the Ground Effect by Phillippe Poisson-Quinton & Amedee Bevert
Apr 3-6 1962
22 SAE 700840 Navy Application of the ACV to Amphibious Operations by Melvin W. Brown
Oct 5-9 1970
23 IAS Preprint No. 832 The Flying Platform as a Research Vehicle for Ducted Propellers by Alvin H. Sacks Hiller Helicopters
Jan 27-30 1958
24 IAS Hydrofoil Transmissions by Eugene E. Shipley General Electric
Sep 18 1962
25 Report No. NADC-ED-L6326 Nondimensional Analysis and Parameter Optimization of Over-Water Ground Effect Vehicle types Including Aerodynamic and Wave drag Effects Contract# WEPTASK R360FR 102/2021/R011-01001
Aug 29 1963
26 TCREC TR 62-28 An Experimental Investigation of the Response Characteristics of Two Man-Carrying Ground Effect Machines Contract# DA 44-177-TC-733
Apr 1962
27 Report GD/C-62-288 GETOL Multibased VP Concept Sep 1962 28 NASA TN D-119 Investigation of a High-Speed Hydrofoil
with Parabolic Thickness Distribution Nov 1959
29 Wing-In-Ground Effect Technology Workshop Proceedings
Sep 19-20 1978
30 Report No. 464 Longitudinal Stability and Control of a Ducted-Rotor Flying Platform by Joseph J. Trayber Contract# DA 44-177-TC-392 Princeton Univ.
May 1959
31 Convair VTOL/GETOL ZP-60-00001 (March) C.A. 1960 32 Report No. ZP-296 Convair VTOL/GETOL Logistic
Transport Vehicle Feb 28 1960
33 ADC Report No. 520-3/R24/46 Aerial Jeep Phase I Final Report Volume I of II Contract# DA-44-177-TC-397
Dec 1 1957
34 ADC Report No. 520-3/R24/46 Aerial Jeep Phase I Final Report Volume II of II Contract# DA-44-177-TC-397
Dec 1 1957
35 The Dynamic Interface Vehicle Lockheed – California Aug 1963 36 Report LR 22620 Propulsion Study for STOL Air-Sea
Craft Contract# ONR NR212-191/8-168 Code 461 Jun 29 1969
165
37 IAS Paper No. 59-121 Ground Proximity: A Critical Review by G.B. Matthews & J.L. Wosser ONR
Jun 16-19 1959
38 Aerophysics Report No. 520-2/R40/46 Aerial Utility Vehicle Monthly Progress Report for Oct 1958 Contract#DA 44-177-TC-397
Nov 6 1958
39 SBD Report No. 59-26 Aerial Utility Vehicle Monthly Progress Report for Mar 1959 Contract# DA 44-177-TC397
Apr 3 1959
40 SBD Report No. 59-32 Aerial Utility Vehicle Monthly Progress Report for Apr 1959 Contract# DA 44-177-TC397
May 6 1959
41 SBD Report No. 59-49 Aerial Utility Vehicle Monthly Progress Report for Jun 1959 Contract# DA 44-177-TC397
Jul 10 1959
42 SBD Report No. 59-60 Aerial Utility Vehicle Monthly Progress Report for Aug 1959 Contract# DA 44-177-TC397
Aug 12 1959
43 PESCO Aerial Jeep Study Proposal Feb 1958 44 PESCO “FLEEP” Phase I – Study Program Proposal Mar 1958 45 NASA TN D-1234 Force-Test Investigation of a Model of
an Aerial Vehicle Supported by Four Unshrouded Propellers
Apr 1962
46 NASA TN D-1235 Flight-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellers
Apr 1962
47 WASP by T.L. Metzgar 1987
VTOL FIGHTERS 85 1 XBQM-108A Papers, Articles and Photos Various
2 WADC TR 59-357 Survey and Study of VTOL-STOL Stability and Control Characteristics
Aug 1959
3 Report No. NADC-ED-5822 Study of Stability and Control of VTOL Aircraft
Jun 5 1959
4 Ryan X-13 “Vertijet” – Article and Specifications Jun 1977 5 Report 4697 Remotely Piloted Vehicle/Vertical Take-Off
and Landing Demonstration Vehicle by Warren H. Eilertson
Aug 1975
6 NARPV 75 Proceedings Jun 2-4 1975 7 Report No. 11254-1 VTO High Altitude Visual Fighter,
Ryan Model 112 Stability and Control Report Feb 13 1957
8 Report No. 11255-1 VTO High Altitude Visual Fighter, Ryan Model 112 Stabilization System Report
Sep 30 1956
9 Report No. 11518-3 Dispersed Site Fighter Bomber Ryan Model 115 Airplane Design Summary Report
Nov 26 1956
10 Report 10707 Vertical Take-Off Fighter Design Study Contract# AF 18(600)-1232
Aug 1955
166
11 Report No. 8457-3 Summary Report Jet Reaction Control Development Contract# AF 18(600)-1157
Jul 15 1955
12 Report ZP-108 Summary Report – Preliminary Design Study VTOL Day Fighter Contract# AF 33(616)-2313 Convair
Jul 30 1954
13 Report ZA-237 Estimated Stability and Control of a VTOL Day Fighter Powered by a Turbofan Engine Contract# AF 33(616)-2313
Jul 30 1956
14 Report 11518-4 Dispersed Site Fighter Bomber Ryan Model 115 Development Plan Contract# AF 18(600)-1641
Nov 1956
15 Report No. 10441-12 Interim Progress Report – Advanced Jet Reaction Control Development Contract# NOa(s)10035
Dec 31 1956
14 Report No. ZW-038 VTOL Day Fighter – Preliminary Weight and Balance Report Contract# AF 33(616)-2313
Jul 30 1954
15 Report No. 39.50.41 Final Summary Report – Design Study of a VTOL Dayfighter Aircraft Powered by a Turbo-Fan Engine Contract# AF33(616)-2314
Jun 15 1954
16 Report No. LR 10707 Summary Report Vertical Take-Off Fighter Design Study Lockheed-California
Aug 1955
17 Report No. 11518-2 Program Summary Report – Dispersed Site Fighter-Bomber Study Ryan Model 115
Nov 30 1956
18 Report No. 8452-1 Final Report – VTO Fighter Design Study Contract AF18(600)-1157
Jul 15 1955
VERTICAL LIFT RESEARCH / WINGLESS AIRCRAFT
86 1 Report X-475 Proposal for a Hot Cycle Compound Helicopter Feasibility Program plus Cover Letter HTC
Jul 1960
2 Report No. 159-5 Aerodynamic Analysis Model 159 Convertiplane AHC
Dec 15 1950
3 The TRW Approach to Complete Assessment of the Cheyenne by John F. Mosher TRW
C.A. 1967
4 Operating Problems and Experience with the Sikorsky Skycrane by Miller A. Wachs Sikorsky
1967
5 K-16B reports List 1956-1965 6 AFFDL-TR-67-93 Effects of Gust Velocity Spatial
Distributions on Lateral-Directional Response of a VTOL Aircraft
Jun 1967
7 The Challenge of Aerial Systems Analysis by LTG William B. Bunker
Undated
8 Operational Problems and Experience with Vertical-Lift Aircraft Light and Utility Helicopters by John W. Oswalt
Nov 15 1967
9 Dynamic Analysis in Weapons System Design and Evaluation by Carl V. Swanson
Undated
167
10 The Analog Approach to Aerial Weapon Systems Analysis by William J. Kenneally
Undated
11 Technical Paper No. 309 Some Performance and Weight Aspects of the GETOL Transport by W.Z. Stepniewski & A.H. Schmidt Boeing-Vertol
May 14-17 1962
12 SAE 624A The T65 and T72 Shaft Turbines by I.W. Nichol
Jan 14-18 1963
13 Zeitschrirt Fur Flugwissenschaften – article about Claudius Dornier (in German)
May 1964
14 Maneuverable Long Line Loiter System (MALLLS) – Miscellaneous Articles and Slides
Undated
15 Computation of Rotary Wing Harmonic Airloads and Comparison with Experimental Results by Raymond A. Piziali & Frank DuWaldt
May 2-4 1962
16 Experimental Research on 4-Duct Tandem VTOL Aircraft Configurations by M.O. McKinney & W.A. Newsom NASA Langley
May 3-5 1962
17 Design and Test of a Helicopter Turbine Inlet Foreign Particle Separator by R. Hooper & D.A. Richardson Boeing-Vertol
Undated
18 A Review of Low Airspeed Measurement Techniques by John Leak Boeing-Vertol
Undated
19 Observations on Subsonic V/STOL Aircraft Designs by Bernard Lindenbaum
Jun 30 1960
20 SAE 266G Mass TRANSPORTATION BY High-Speed VTOL by H.V. Borst & J.M. Mergen Curtiss
Jan 9-13 1961
21 A Generalized Experimental Study of Inlet Temperature Rise and near Field temperature Contours of Jet V/STOL Aircraft in Ground Proximity by Robert F. Speth & Patrick E. Ryan Bell
Undated
22 SAE 670352 Turbofan/Turboshaft Powerplant for Composite Helicopters by W.O. Gaffin & S.E. Wilcox Pratt and Whitney
Apr 24-27 1967
23 SAE 660763 Multiroller Planetary Friction Drives by Algirdas L. Nasvytis TRW
Oct 17-21 1966
24 Report No. R-849 Remote Flight Delivery System Concept Presentation Kaman
Apr 20 1970
25 Remote Retrievable Parapoint for Special Operations Sep 1987 26 AMRL-TR-69-140 Long-Line Loiter: Personnel Retrieval
System Mar 1971
27 AMRL-TR-70-104 Long Line Loiter: Personnel retrieval System : Triaxial Acceleration Tests
May 1972
28 AMRL-TR-71-85 Long Line Loiter: Psychological Warfare Package
Jul 1971
168
29 Report PDR-306-II Surface-to-Air Retrieval of Heavy Spacecraft by Fixed-Wing Aircraft Volume II – Development of Analytical Techniques Contract# NAS9195
Jun 1962
30 A Preliminary Design of a Remotely-Controlled Glider for a Long-Line Operation – Thesis by 1LT Eldridge L. Snapp III USAF
Jun 1979
31 Report No. R-407 10-Ton Intra-Theater Transport Kaman Jul 11 1962 32 Piasecki Model 16H Compound Helicopter Proposal 1962 33 Some Basic Derivations About the Action of a Shrouded
Propeller Collins Jul 16 1956
34 Report CER-924 Preliminary ER on the .4 Scale Aerodyne Model Static Tests Collins
Feb 1959
35 Report No. CER-1014 Final Report on Research on Wingless Aircraft Contract# NOnr-2566(00)
Jul 1 1959
36 Report No. CER-1045 Part I Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)
Aug 1 1959
37 Report No. CER-1045 Part II Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)
Aug 1 1959
38 Report No. CER-1045 Part II Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)
Aug 1 1959 rev Jan 15 1960
39 Report No. CER-1045 Part III Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)
Jan 31 1960
40 SAE 747C An Economic Assessment of the Hot Cycle Compound Helicopter for VTOL Transport by Malcolm Harned & Harvey O. Nay HTC
Sep 23-27 1963
41 Ejector Shroud Articles (7) Undated 42 NACA RM L55F28 An Experimental Investigation of a
Flat Ram-Jet Engine on a Helicopter Rotor Jan 4 1956
43 Report ER 4221 New Light Observation Aircraft Lockheed-Georgia
Feb 1 1960
44 Report 2-Y-2 Wind Tunnel Tests of ¼-Scale Model of PiAC VTOL Aircraft PA-2C Contract# NOa(s)56-834-c
Jan 5 1959
45 Report 2-Y-4 Ring-Wing V/STOL Logistics Aircraft Contract# ARDC-SR No. 175
Feb 25 1960
46 XV-1 Flight Safety Inspection Jun29-Jul 1 1954 47 NACA TN 4117 Experimental Investigation of Lift, Drag,
and Pitching Moment of Five Annular Airfoils Oct 1957
48 Report No. RAC 651-901A VTOL/STOL Logistics Aircraft Parametric Study 1965-1970 Time Period Republic
Feb 19 1960
169
49 Report 57-59 1031-B Wind Tunnel Model Specification and Tunnel Program Hiller
Jun 3 1957
50 Report NA-62-954 Ten Ton Assault Transport NAA Aug 29 1962 51 Recollections- Chapter 5 Wright Field and Aircraft
Laboratory WWII 1941-1945 by Dr. Courtland Perkins C.A. 1989
52 TR D3-3512-1 Human Reaction to Low Frequency Vibration Contract# NONR 2994(00) Boeing
Undated
53 Miscellaneous Papers 1953-1956
DOWNWASH AND GROUND EFFECT 87 1 Symposium on Ground Effect Phenomena Princeton Univ. Oct 21-23 1959
2 WADD Technical Note 60-183 Hot Gas Surface Erosion Studies
Aug 1960
3 Report No. FDDS-67-6 Test Report on Measurements for V/STOL Vehicle Downwash Characteristics
Sep 22 1967
4 USAAVLABNS TR 68-52 Investigation of the Downwash Environment Generated by V/STOL Aircraft Operating in Ground Effect Contract# DA 44-177-AMC-316(T)
Jul 1968
5 Kellett Downwash Contract# Now 61-0926-C C.A. 1963 6 Report No. 179T80-2 An Investigation of VTOL
Operational Problems Due to Downwash Effects Contract# Now 60-0450-f Kellett
Jun 12 1961
7 Report No. 179T80-6 Effects of Airframe Geometry on Downwash Problems of Tandem Ducted-Propeller VTOL Aircraft Contract# Now 61-0926-c
Jan 1964
8 Report No. 179T80-12 Downwash Tests of the Dual tandem Ducted Propeller VTOL Research Aircraft Configurations to Evaluate Single Inlets, Protection Devices and Study Aerodynamic Interference Kellett
Nov 1 1965
9 Report No. 2023-917001 VTOL/STOL Flying Handling Qualities Specification Study Contract# NOas 60-6067-f Bell
Jun 25 1960
10 WADC TR 59-357 Survey and Study of VTOL-STOL Stability and Control Characteristics
Aug 1959
11 NASA TN D-4624 Study of Optimum Values of Several Parameters Affecting Longitudinal Handling Qualities of VTOL Aircraft
Jul 1968
12 Report No. 484 Theoretical Investigations Related to Unsteady Air Forces on Wing/External Store Combinations of VTOL Aircraft by J. Becker & A. Lotze (From German)
Nov 20 1969
13 Report No. 012-26 An Investigation of the Over Water Aspects of VTOL Airplanes at High Disc Loading Contract# Now 62-0279-d Curtiss
Dec 1963
170
14 AHS 28th Annual National Symposium Paper 642 An Experimental Investigation of STOL Longitudinal Flying Qualities in the Landing Approach Using the Variable Stability X-22A Aircraft by J.M. Schuler, R.E. Smith & J.V. Lebacqz Cornell
May 1972
15 AHS 28th Annual National Symposium Paper 644 A Pilot’s Opinion: VTOL Control DesignRequirements for the Instrument Approach Task by James M. Patton, Jr. NASA Langley
May 1972
16 AHS 28th Annual National Symposium Paper 654 An Integrated System of Airborne and Ground-Based Instrumentation for Flying Qualities Research with the X22A Airplane by John L. Beilman Cornell
May 1972
17 AIAA Paper No. 64-777 Handling Qualities of VTOL Aircraft by Richard K. Wilson & Charles B. Westbrook AF Flight Dynamics Lab, WPAFB
Sep 21-23 1964
18 AGARD Flight Mechanics Panel (27th Meeting) Application of the Model Technique to a Variable-Stability Helicopter for Simulation of VTOL Handling Qualities by John F. Garren, Jr. & James R. Kelly NASA Langley
Oct 11-12 1965
19 Analysis of a Jet in a Subsonic Crosswind NASA Symposium
Sep 9-10 1969
20 Report No. CAL NO. 171 An Experimental Study of Pilot Visibility from a VTOL Aircraft in Overwater Hover Contract# N00014-68-C-0241 NR 212-182 Cornell
Apr 1969
21 Recirculation Model Tests (condensed paper) by Felix Aulehla (stamped 5)
Jan 15 1970
22 V/STOL Technology Briefing 1970 (Stamped 4) Jan 15 1970 23 Handling Qualities and Pilot Dynamics by Charles B.
Westbrook WADC & Duane T. McRuer Systems technology, Inc from Aero/Space Engineering
May 1959
24 Stabilisation en vol Vertical Des Avions VTOL by G. Ernst & J. Jardinier SNECMA (in French)
Jun 1960
25 Standard Flight Control Systems for Aircraft designed at Present in the Federal Republic of Germany, incl. VTOL
Undated
26 NASA TN D-977 An Investigation of the Downwash from a VTOL Aircraft and a Helicopter in the Ground Environment
Oct 1961
27 NASA TN D-5175 An Investigation of a Direct Side-Force Maneuvering System on a Deflected Jet VTOL Aircraft
Apr 1969
28 NASA TN D-5617 Review of Propulsion-Induced Effects on Aerodynamics of Jet VTOL Aircraft
Feb 1970
29 NASA TN D-5729 An Exploratory Wind-Tunnel Investigation of the Wake Effect of a Panel Tip-Mounted Fan-Jet Engine on the Lift-Induced Vortex
May 1970
171
30 AFFDL-TR-68-69 Study and Simulation Program to Investigate the Mechanization of an Aircraft Flight Control System that Employs Direct Lift Volume I: Preliminary Design of Direct Lift Controls
Jun 1968
31 Bad Weather Landing of VTOL Aircraft by Dr. K.H. Fischer (from German)
Mar 1970
32 A Review of AGARD Recommendations for V/STOL Handling Qualities (Report 408) in the Light of US Army Experience with the XV-5A and Other V/STOL Aircraft Including Helicopters by US Army Test & Evaluation Command
Undated
33 VTOL Six Degree of Freedom Control System Colt Industries
Undated
34 Report No. 214-100-59 Aero-Thermo Requirements for ESA 4209 NAA
Sep 11 1959
35 Report No. 210-98-59 V/STOL Simulation Scheduling and Utilization NAA
Oct 27 1959
36 Report No. 210-102-59 Analysis of V/STOL Wind Tunnel Testing Requirements NAA
Nov 11 1959
37 Report No. 214-3-60 A Note on Stability and Control Problems of VTOL Aircraft in Hovering and very Slow Flight NAA
Jan 11 1960
38 Simulator Photos (2) May 25 1966 39 SAE 700785 A Fluidically-Augmented Artificial Feel
System for High Performance Aircraft by Tor W. Jansen & Walter W. Kaniuka NADC
Oct 5-9 1970
40 Downwash in Connection with Rescue Papers, Letters & Notes
C.A. 1968
41 AHS 24th Annual National Symposium Paper 204 Avionics and Armaments Panel Session
May 8-10 1968
42 AHS 24th Annual National Symposium Paper 219 VTOL Handling Qualities Crireria and Control Requirements – Analysis and Experiment by Thomas E. Lollar & Gerhard K.L. Kriechbaum Boeing
May 8-10 1968
43 AHS 26th Annual National Symposium Paper 444 Models for a VTOL Airplane in Transition by David L. Key Cornell Aero Labs
Jun 1970
44 VTOL Control/Stability Articles (3) 1962-1965 45 Report No. 179T80-11 Interim Report on Tests of Engine
Injection of a Full-Scale Reflection Plane Model of the Ducted Fan Tandem VTOL Research Aircraft Kellett
Jul 17 1964
46 Report No. DCR-268 Downwash Environment for the Boeing Model 160 V/STOL Aircraft Dynasciences
Jan 1968
47 Report No. D6-9908 Design Surface temperatures for V/STOL Aircraft Boeing
Jan 30 1964
48 Applied Aerodynamics for V/STOL Northrop Mar 1970
172
49 Study of Application of Pure Fly-By-Wire Primary Flight Control Systems to Propeller Driven V/STOL Aircraft Curtiss-Wright
Sep 13 1965
50 Report No. NOR 67-135 VTOL Aircraft Reaction Control Technology Studies Northrop
Jun 1967
51 Report No. NA61H-804 An Analytical Study of the Dynamic response of V/STOL Vehicles NAA
Dec 21 1961
VTOL PROPOSALS/CONCEPTS 88 1 Report No. C-2842 Summary Flight Test Report on the
Curtiss-Wright X-100 VTOL Aircraft Nov 30 1960
2 Report No. SD-139A Curtiss-Wright High-Speed VTOL Aircraft Model 200 General Configuration and Performance
Mar 1961
3 Report No. PDA-70461 Curtiss-Wright VTOL Aircraft for Air Force Recovery Missions
Jul 3 1961
4 Report No. C-2798 Design and Performance of the Lifting Propeller X-100 VTOL Airplane Curtiss
Oct 8 1959
4 Presentation to AFSC V/STOL Aircraft Curtiss Oct 18 1963 5 Curtiss-Wright High-Speed VTOL C.A. 1963 6 Report No. 014-252 X-19 Aerodynamic Stability and
Control Summary Curtiss Feb 19 1964
7 AFFTC TR 66-27 X-19 Category I Limited Flight Evaluation
Oct 1966
8 Glass Fiber Reinforced Plastic Blades Brochure Curtiss 1961 9 Curtiss-Wright High Speed VTOL Brochure (3) Undated 10 AFSC System 664A System Package Program – X-19
VTOL Research Aircraft Mar 15 1965
11 Development of the Curtiss-Wright V/STOL Airplanes by Henry V. Borst Borst Assoc.
Undated
12 VTOL The Significance of Radial Force Pamphlet Curtiss Undated 13 Report No. 014-523 Stability and Control Analysis of X-19
Flight Testing for Flights 2 Through 22 Curtiss Dec 31 1964
14 Report No. 014-731 X-19 power Required Derived From Category I Flight test Results Curtiss
Dec 3 1965
15 Blueprints of M-260 Recovery Vehicle Curtiss Jun 27 1961 16 Report of X-19 VTOL Program Technical Review (2) Jan 1965 17 The High-Speed VTOL X-100 and M200 Aircraft by H.V.
Borst Curtiss Aug 1962
18 Can the Osprey Survive in Combat? An Assessment of MV-22 Combat Effectiveness by Maj.George J. Trautman, III USMC Naval War College
Feb 16 1988
19 AIAA Paper 63-483 The Domain of the Convertible Rotor by R. Hafner Westland Aircraft Ltd.
Oct 21-24 1963
20 Verticraft Corporation Lift-Fan Aircraft – Photos and Drawings
1961
173
21 Malvestuto Proposal – Documents, Drawings, Presentations
1969
22 Malvestuto Proposal Presentation C.A. 1969 23 Curtiss-Wright X-19 Miscellaneous Photos & Articles C.A. 1962 24 NASA TN D-1239 An Experimental Study of the Effect of
Downwash from a Twin-Propeller VTOL Aircraft on Several Types of Ground Surfaces
May 1962
25 Letters to Hon. F.C. Carlucci re: JVX 1982 26 WFG-P16 & P23 (in German) Undated 27 Investigation of Change in Horsepower with Early
Transitions from Propeller Mode to Helicopter Mode with Handwritten Notes. Sikorsky
Undated
28 Rotavion, Inc – Correspondence and Notes C.A. 1960 29 Report XR-62 VTOL Aircraft Votavion, Inc 1961 30 Report No. PR-4 Proposal for a Flight test Program on the
Vanguard 2 Fan-In-Wing VTOL/STOL Aircraft Feb 23 1960
31 Report No. T-2-T Tie-Down Tests of the Vanguard Model 2 Fan-In-Wing VTOL Aircraft
Nov 28 1959
32 Vanguard Model 2 – Miscellaneous Photos and Papers C.A. 1960 33 Report No. PR-106 Proposal for the Advancement of
Techniques for V/STOL Lift and Propulsion Systems Vanguard Corp.
Aug 31 1961
34 Report 28-X-1 SR-175 Study Report – VTOL/STOL Logistics Aircraft A Parametric Study for the 1965-1970 Time Period Vanguard Corp.
Feb 23 1960
35 Report No. PR-4(2) Proposal for the Continuation of test program on the Vanguard 2 Fan-In-Wing VTOL/STOL Aircraft
Apr 8 1960
36 Vanguard Model 2 Miscellaneous Correspondence and Proposals
C.A. 1960
37 Vanguard Model 2C Tests Ames Research 1962
TILT WING AIRCRAFT 89 1 Report No. TS-152 Type Specification for Tri-Service
VTOL Prototype Transport Aircraft Jan 13 1961
2 Tilt Wing VTOL Aircraft – Sketches & Charts Undated 3 VC 400 VTOL Cargo Aircraft by Dr. Siegfried Gunter
VFW Munchen Jun 1966
4 Report No. D8-2076 Evaluation of Geared Flap Control System for Tiltwing V/STOL Aircraft Boeing Co.
Aug 11 1970
5 Tilt Wing Proposal and Papers Boeing Aircraft Co. May 18 1967 6 AIAA Paper No. 71-992 A Comparison of Outflows from
a Helicopter, Tilt-Wing and Jet Lift Hovering Aircraft by Odd E. Michaelsen Canadair
Oct 25-28 1971
174
7 AFFDL-TR-70-124 Detail Design of Critical Components for a Prop/Rotor Aircraft Final Report, Phase II Boeing-Vertol
Jul 1970
8 ASD-TR-69-15 Propeller Static Performance Tests for V/STOL Aircraft
Jan 1970
9 NASA TN D-946 Rapid-Transition Tests of a 1/4 – Scale Model of the VZ-2 Tilt-Wing Aircraft
Oct 1961
10 NASA TN D-989 Summary of Flight test results of the VZ-2 Tilt-Wing Aircraft
Feb 1962
11 NASA TN D-1365 Longitudinal Stability and Control of a Tilt-Wing VTOL Aircraft Model with Rigid and Flapping Propeller Blades
Jul 1962
12 NASA TN D-1375 Flight Test Investigation of Ailerons as a Source of Yaw Control on the VZ-2 Tilt-Wing Aircraft
Jun 1962
13 NASA TN D-1389 Force-Test Investigation of the Stability and Control Characteristics of a Four-Propeller Tilt-Wing VTOL Model with a Programmed Flap
Sep 1962
14 NASA TN D-1390 Flight Investigation of the Longitudinal Stability and Control Characteristics of a Four-Propeller Tilt-Wing VTOL Model with a Programmed Flap
Sep 1962
15 NASA TN D-2680 Flight Investigation of the VZ-2 Tilt-Wing Aircraft with Full-Span Flaps
Mar 1965
16 NASA TN D-4030 Aerodynamic Data on Large Semispan Tilting Wing with 0.5-Diameter Chord, Single-Slotted Flap, and Single Propeller 0.08 Chord Below Wing
Jul 1967
17 NASA MEMO 1-16-59L Semiempirical Procedure for Estimating Lift and Drag Characteristics of Propeller-Wing-Flap Configurations for Vertical-and Short-TakeOff-And-Landing Airplanes
Dec 1958
18 Report No. 478 A Stability Analysis of Tilt-Wing Aircraft by Henry E. Payne III & Charles H. Cromwell III Princeton Univ.
May 1960
19 Tilt-Wing Applications by Blaine R. Parkin General Dynamics & Saul Bernstein Canadair
Undated
20 Vertol MOCO (Monocyclic Control)Programs 1966 21 Flight Test Experience of a Tilt Wing VTOL by W.Z.
Stepniewski Vertol Jun 15-18 1959
22 Report No. PR-543 Monocyclic Control Program (MOCO) Revision A
May 28 1965
23 Proposal to Test a Simplified Tilt-Wing with MOCO (Appendices)
Dec 1965
24 Report No. PR-394 Proposal – Boeing-Vertol 119F Tilt-Wing Aircraft
Undated
25 Report No. D8-2369-4 V/STOL Propeller Design Parameters Boeing
Apr 1969
26 MBB GMBH BO-140 V/STOL Transport Nov 1969
175
27 Grumman Design 242 Tri-Service Transport Pamphlet Apr 17 1961 28 Grumman Design 170a Tilt-Wing Rescue Aircraft Dec 21 1959 29 Grumman design 134E VTOL Mohawk Jan 1959 30 Conclusions and Recommendations for XC-142A Undated 31 Requirements for Automatic Stabilization of the XC-142A
in the V/STOL Flight Modes Chance-Vought 1963
32 Report No. 2-51072/2R6A detail Specification for Model XC-142A VTOL Cargo Assault Aircraft Contract# AF 33(657)-7868 Chance Vought
Oct 4 1963
33 XC-142A V/STOL Transport Transmission System Brochure Hiller Vought Ryan
Undated
34 Report No. 56-61 Tilt Wing Propelloplane Selection and Optimization for Transport – Rescue Missions Hiller
Jun 1956
35 Report No. AER-E1R-13347 VHR-447 Tri-Service Transport Vol.7 Summary Report Part 2 Airplane Description Hiller Vought Ryan
Apr 1961
36 VTOL Amphibious Assault Transport Systems 1962-1967 Phase II Summary Report – Assault Helicopters
Nov 15 1957
SHROUDED PROPELLERS AND PROPULSION SYSTEMS
90 1 AFFDL-TR-71-88 Volume II – Advanced V/STOL Propeller Technology – Static Thrust Prediction Method Development
Sep 1971
2 AFFDL-TR-71-88 Volume V – Advanced V/STOL Propeller Technology – Surface Pressure Measurements on a Propeller Blade Operating at Zero Advance Ratio
Sep 1971
3 AFFDL-TR-71-88 Volume VI – Advanced V/STOL Propeller Technology – Small Scale Cyclic Pitch Investigation
Jun 1972
4 AFFDL-TR-71-88 Volume VII – Advanced V/STOL Propeller Technology – Large Scale Cyclic Pitch Investigation
Jun 1972
5 AFFDL-TR-71-88 Volume IX – Advanced V/STOL Propeller Technology – Advanced Materials Study
Mar 1973
6 AFFDL-TR-71-88 Volume X – Advanced V/STOL Propeller Technology – Advanced Propeller Design
Dec 1971
7 AFFDL-TR-71-88 Volume XI – Advanced V/STOL Propeller Technology – Advanced Gearbox Design
Jul 1972
8 AFFDL-TR-71-88 Volume XII – Advanced V/STOL Propeller Technology – Advanced Propeller Manufacture and Test
Apr 1974
9 AFFDL-TR-71-88 Volume XIII – Advanced V/STOL Propeller Technology – Far-Field Noise Investigation
Mar 1972
10 AFFDL-TR-71-88 Volume XIV – Advanced V/STOL Propeller Technology – Program Summary Report
Apr 1974
176
11 Report No. 213-1 Shrouded Propeller Investigations: Wind Tunnel Tests of a Shrouded Propeller with a 17-Bladed Rotor, Inlet and Exhaust Stators, and Long Shroud with High-Speed Inlet and No Exit Diffusion Contract#NONR201(01) Univ. of Wichita
Jun 1958
12 Report No. 213-8 A Method of Design of Shrouded Propellers Contract#NONR-201(01) Univ. of Wichita
Oct 1959
13 Report No. 213-9 Shrouded Propeller Investigations: Shroud and Centerbody Pressure Distributions of a Shrouded Propeller with 17-Bladed Rotor, Inlet and Exit Stators and Long Chord Shroud Contract# NONR-201(01) Univ. of Wichita
Oct 1959
14 Report No. 213-10 Shrouded Propeller Investigations: Shroud and Centerbody Pressure Distributions of a Shrouded Propeller with 10-Bladed rotor, Exit Stators and Long Chord ShroudContract#NONR-201(01) Univ. of Wichita
Jan 1960
15 Report No. 213-11 Shrouded Propeller Investigations: Wind-Tunnel Tests of a 2-Bladed Shrouded Propeller Model Contract#NONR-201(01) Univ. of Wichita
Nov 1960
16 Report No. 213-12 Shrouded Propeller Investigations: Wind-Tunnel Tests of a 4-Bladed Propeller Model having a 0.30 Hub/Tip Diameter Ratio Centerbody Contract#NONR-201(01) Univ. of Wichita
Mar 1961
17 Report No. 213-13 Shrouded Propeller Investigations: Wind-Tunnel Tests of a 4-Bladed Propeller Model having a 0.4 Hub/Tip Diameter Ratio Centerbody Contract#NONR-201(01) Univ. of Wichita
Mar 1961
18 Report No. 213-15 Shrouded Propeller Investigations: Propeller Tip Clearance EffectsContract#NONR-201(01) Univ. of Wichita
Apr 1961
19 Report No. 337 Shrouded Propeller Investigations: Aerodynamic Characteristics of a Shroud with Centerbody Contract#NONR-201(01) Univ. of Wichita
Feb 1959
20 WADC TR 58-604 Wind Tunnel Tests of Shrouded Propellers at Mach Numbers from 0 to 0.60 Contract# AF 33(616)-5363 (Copy)
Dec 1958
21 Research Note #7 Ducted Propeller Studies at Mississippi State Univ. Contract# Nonr 978(01)
Nov 28 1958
22 Aero Report 951 Shrouded Propeller Thrust Ratio as a Measure of Shroud and Propeller Static Performance
Jan 1959
23 Document No. 70-6568(25) Investigation of a Low Loading High tip Speed Transonic Fan Stage NASA Progress Report May 29 to Jul 2 1972 Contract# NAS313498 Garrett
Jul 26 1972
177
24 Document No. 72-8597(4) Application of Holography to Flow Visualization within Rotating Blade Row Monthly Technical Progress Narrative Aug 27 to Oct 1 1972 NASA Contract# NAS 3-15336 Garrett
Oct 30 1972
25 Research Report No. 20 Study of a Shrouded Propeller with Distributed Suction on the Inlet Profile by Henry Marshall Claybourn, Sr. Contract# Nonr 978(01) Mississippi State Univ.
Jan 20 1959
26 Bi-Monthly Progress report No. 1 Analytical Study of Shrouded Propellers Contract# AF33(616)-2765 Longren Aircraft Co.
Feb 1955
27 Report No. ARD-224 Wind Tunnel Test of Several Ducted Propellers in Non-Axial Flow Phase IV Contract# Nonr 1357(00) Hiller
Apr 20 1959
28 Theory and Testing of Jet Propulsion Motors and Rockets by Zygmunt Fonberg Aircraft Jet and Rocket Corp.
1945
29 Propulsion – Miscellaneous Articles Various 30 SAE 650201 Lift Engine technology by T. Foster & H.D.
Paget Continental Apr 12-15 1965
31 Propulsion for VTOL GE Mar 18 1963 32 Report NO> DM 62-14 A Comparison of VTOL
Propulsion Systems in a Subsonic Mission by W.L. Rodenbaugh GE
Jan 18 1962
33 Propulsion for Army VTOL Requirements GE Undated 34 Q-Fan folder and Articles Hamilton-Standard 1972-1973 35 Report No. EDR 5584 Allison Model 501 Free Turbine
Turboshaft Engines Jan 1968
36 Propulsion Systems for Remotely Piloted vehicles GE Undated 37 Report No. D210-10696-1 Study of Extreme High Altitude
Propulsion Contract# F33657-74-C-0166 Beoing-Vertol Sep 1974
38 Report No. QFT-55-18 rev A Q-Fan Propulsion System Preliminary Specification – QFT-55-18 Hamilton-Standard
Sep 20 1971
39 Report No. QFT-55-18 rev B Q-Fan Propulsion System Preliminary Specification – QFT-55-18 Hamilton-Standard
Jun 1972
40 Report No. QFT-64-18 rev B Q-Fan Propulsion System Preliminary Specification – QFT-64-18 Hamilton-Standard
Jun 1972
41 Re-Design of a Lightweight, Low-Volume, Piston Engine Hydra-Electric Co.
May 17 1973
V/STOL FIGHTERS 91 1 V/STOL Fighter Blueprints 1963
2 10-Ton V/STOL Assault Transport Blueprints 1962 3 V/STOL Fighter Pamphlets and Overlays Various
178
4 NASA TN D-4812 Aerodynamic Characteristics of a Five-Jet VTOL Configuration In the Transition Speed Range
Oct 1968
5 NASA TN D-5727 Induced Interference Effects on the Aerodynamic Characteristics of a 0.16-Scale Six-Jet V/STOL Model in Transition
Mar 1970
6 NASA TN D-5770 Wind-Tunnel Investigation of a VTOL Jet-Transport Model with Powered Lift Engines in Pods at Wing Midspan or Inboard
Apr 1970
7 Progress Report on Fiat G 95/4 Program Presented in Rome the 13th of April
Undated
8 Proposal for T-38 ARPS V/STOL Trainer Aircraft Northrop Norair
Mar 1965
9 Society of Experimental Test Pilots – Mach 2 V/STOL (VJ 101) Flight Test Program by George L. Bright
Sep 27-28 1963
10 V-465 V/STOL Transport Charts and Diagrams (incomplete)
Undated
11 Report No. 2000-910200 VTOL Fighter Program – Bell VTOL/STO-VL Airplane – Detail Specification
Dec 23 1958
12 VTOL Technology Status NAA Nov 1965 13 Tech. Memo AERO 911 Results of Flight Tests on the
Short SC1 VTOL Research Aircraft with Particular Reference to Handling Qualities in the Hover and Transition Royal Aircraft Establishment
Sep 1965
14 NAA CX-6 Study Undated 15 Report No. 2000-927007 VTOL Fighter Program –
Experimental Model Programs Contract# NOas 57-836-c Bell
Feb 6 1959
16 Report No. 2000-902058 VTOL Fighter Program – Ground Velocities and Temperatures Jet Impingement Tests (Model 2000-971111) Contract# NOas 57-836-c Bell
Jan 30 1959
17 Navy D-188A VTOL Fighter Program Presentation Bell Feb 19959 18 Document No. D2-4918 Technical Design Studies –
Interim Report Boeing Oct 8 1959
19 Document No. D2-4918-1 Supplemental Information for D2-4918, Technical Design Studies – Interim report Boeing
Oct 26 1959
20 Document No. D2-4943 Tactical Test Program – Past, Present and Future Boeing
Oct 10 1959
21 Document No. D2-5032 Tactical Design Studies – Trade Data Boeing
Oct 26 1959
22 Document No. D2-5161 VTOL/STOL Airplane – Engine matching Study Boeing
Nov 13 1959
23 Report No. D188A-945-238 Navy VTOL Fighter Program – Progress Report No. 2 Contract# NOas 57-836-c
Apr 11 1958
24 Vertical Take-Off Research Aircraft Specification No. ER.143.T Shorts Aircraft, Ltd.
Feb 1954
179
25 Report No. M42-945-001 Summary of V/STOL Tactical Fighter Investigations Bell
Jun 24 1959
26 Report No. 2000-933001 V/STOL Tactical Fighter Bell Aircraft – Convair
Oct 1 1959
27 The Design of a Supersonic V/STOL Fighter-Bomber by James A. O’Malley, Jr. Bell
Jun 14 1961
28 Report No. 2000-902058 VTOL Fighter Program – Progress Report for April 1958 Contract# NOas 57-836-c Bell
May 15 1958
29 Report No. 2000-953001 XF-109 V/STOL Tactical Fighter Weapons System Bell
Feb 17 1959
30 NACA RM SL58H15 Low-Speed Wind-Tunnel Tests of a 1/8-scale Model of the Bell D-188A VTOL Airplane
Aug 15 1958
31 Report No. D188A-945-206A Standard Aircraft Characteristics Model D188A Bell
Jan 24 1958
32 VJ 101C Pamphlet (in German) Undated 33 Report No. 2000-927006 VTOL Fighter Program –
Description and Technical Data for Mock-Up Inspection Contract# NOas 57-836-c Bell Aircraft
Feb 6 1959
34 Report No. 2000-927010 VTOL Fighter Program – Proposal Bell
Oct 1 1959
35 Report No. LR 17896 Proposal for VTOL Test vehicles Using F-104A Lockheed-California
May 28 1964
36 Report No. ER-6182 GL293 – VTOL C130 Lockheed-Georgia
Oct 1963
VTOL – GENERAL 92 1 AGARDograph 46 Symposium on Vertical & Short Take-
Off and Landing Aircraft Part I Jun 1960
2 AGARDograph 89 V/STOL Aircraft Part I Sep 1964 3 AGARD-CP-126 Military Applications of V/STOL
Aircraft Volume I Oct 1972
4 Report No. 350 Unified Performance Theory for V/STOL Aircraft in Equilibrium Level Flight Contract# Nonr4926(00)(X) Air Vehicle
May 1966
5 Report No. FAA-ADS-26 STOL-V/STOL City Center Transport Aircraft Study Contract# FA64WA-5012
Oct 1 1964
6 Report NO. NA-63-1262 V/STOL Convictions NAA Nov 6 1963 7 Report No. ARD-182.1 Supplementary Technical Data to
High Performance Missile Resupply Aircraft May 2 1958
8 Report No. 182 Proposal for the Study of a High Performance Missile Resupply Aircraft Hiller
Jan 24 1958
9 Future of Military V/STOL Oct 4 1977 10 Report No. 553-6 (ARD 758-400) A Study of the
Comparative Effectiveness of V/STOL and STOL Aircraft in Limited and General War Environments
Oct 11 1962
180
11 Report No. R-670 Post 1980 Navy Air Rescue Presentation Kaman
Feb 27 1967
12 Report No. NADC-76019-30 Parametric and Conceptual Design Study of Small V/STOL Sea Loiter Aircraft Lockheed-California
Feb 1977
13 AFAPL-TR-66-90 An Analytical Method of Determining General Downwash Flow Field Parameters for V/STOL Aircraft
Nov 1966
14 USAAVLABS TR 67-40 Investigation of Hydraulic Power Transmission Systems for V/STOL Aircraft
Aug 1967
15 NASA TN D-862 A Flight Examination of Operating Problems of V/STOL Aircraft in STOL-Type Landings and Approach
Jun 1961
16 Ten-Ton V/STOL Transport Presentation Chance-Vought Undated 17 Tactical Employment of Brigades and Battalions of
Infantry and Mechanized Divisions by Col. Ralph L. Whitt US Army
Undated
18 Some Aspects of Convertible Aircraft Design by Robert L. Lichten Bell
May 9 1949
19 IAS No. 724 Evaluation of VTOL Systems Suitable for Transport Aircraft by W.Z. Stepniewski & Joseph Mallen Vertol
Jan 28-31 1957
20 AIAA Paper No. 71-980 The V/STOL Projects of the Federal Republic of Germany by Drury W. Wood Dornier
Oct 25-28 1971
21 Technical Paper No. 309 Some Performance and Weight Aspects of the GETOL Transport by W.Z. Stepniewski Boeing-Vertol
May 14-17 1962
22 Design Considerations for VTOL Aircraft by Edward E. Swanson & Donald W. Robinson, Jr. Kaman
Dec 11 1962
23 AHS 24th National Forum Paper No. 222 Power Spectral Density Analysis of V/STOL Aircraft Structures by Melvin J. Rich, Martin H. Israel, Irwin J. Kenigsberg & Peter P. Cook Sikorsky
May 8-10 1968
24 SAE 650193 Helicopters and Propeller-Type VTOL Aircraft in the Light of technologies by W.Z. Stepniewski & M.I. Young Boeing-Vertol
Apr 12-16 1965
25 SAE 660316 The Effect of Size on the Economics of a V/STOL Transport Airplane by George D. Ray Boeing
Apr 25-28 1966
26 SAE 680330 Large Military Transport (V/STOL) by John C. Ford North American Rockwell
Apr 29-May 2 1968
27 SAE 680699 Forward Area Air Cargo Systems by Lewis G. Knapp Sikorsky
Oct 7-11 1968
28 SAE 680301 Possible Navy Applications of V/STOL Transports by Hugo G. Sheridan
Apr 29-May 2 1968
29 The Aerodynamic Effects of Lift Jet and Lift Fan Inlets in Transition Flight by William E. Grahame Northrop
Jun 13 1968
181
30 VTOL Advances as Determined from Analysis of Future Needs and Technological Potentials by Bernard Lindenbaum, Robert Malbi & Richard Krabel AFSC (3 copies)
Dec 6 1967
31 Design Philosophy of Subsonic Compound Aircraft vs. Operational Requirements by W.Z. Stepniewski, J.J. Schneider Boeing-Vertol
Undated
32 Report NO. NA-68-224 Large Military Transport (V/STOL) by John C. Ford NAA/ Rockwell
C.A. 1968
33 Engineering Paper No. 1224 Factors Involved in the Design of a VTOL Propulsion System by Charles O. Gunderson Douglas
Oct 12 1961
34 Application of Optimization Techniques to the Design and Operation of V/STOL Aircraft by W.Z. Stepniewski Boeing-Vertol & M.Z.v.Kryzwoblocki Michigan State Univ.
Apr 3-6 1967
35 Vertical Takeoff Aircraft by L. Gil’berg Oct 26 1960 36 VTOL-STOL Survey for NACA by Grover Loening Nov 30 1957 37 AIAA Paper No. 69-326 Future Military Applications of
VTOL Aircraft by Col. John W. Oswalt & Gen. Hamilton H. Howze
Feb 17-19 1969
38 AHS 13th Annual Forum Military Aspects of VTOL Aircraft Development by LTC John L. Klingenhagen
May 9 1957
39 NASA TN D-735 Handling Qualities Experience with Several VTOL Research Aircraft
Mar 1961
40 Proprotor Short-Haul Aircraft – STOL and VTOL by Kenneth W. Sambell Bell
Jul 5 1972
41 Running Takeoff Overload Limitations of Some VTOL Aircraft Piasecki
May 25 1961
42 Advanced Configurations Boeing Jun 1963 43 Report No. 30863 V/STOL in a 10-Ton Payload Assault
Transport Douglas Apr 27 1962
44 SR-175 3-5 Ton Class Doak Undated 45 Current Status of VTOL Research and Development at
Sikorsky Dec 8 1959
46 V/STOL Capabilities Lockheed-California Undated 47 Vertol Status Report on VTOL Projects 1959 48 VTOL Studies Presentation Chance-Vought Undated 49 Report No. 2-59-945001 Summary of VTOL at Bell
Volume I Nov 1959
50 Report No. G-10-1 V/STOL Concepts Summary Dec 1 1959 51 VTOL Miscellaneous Papers Various 52 VTOL Miscellaneous Photos & Transparencies Undated
STOL/VSTOL PROPOSALS AND CONCEPTS 93 1 YC-14 Brochure Boeing Sep 1976
182
2 YC-15 Brochure McDonnell-Douglas Sep 1977 3 SAE 700811 Synthesis of Future High Lift Systems by
Richard Scherrer Lockheed-California Oct 5-9 1970
4 A Boeing View of Commercial STOL by Richard D. FitzSimmons Boeing
Sep 1969
5 YC-14 AMST Brochure Undated 6 Report No. ER-9801 A Preliminary Report of the
Spanwise Blowing Concept Lockheed-Georgia Mar 1968
7 NASA TN D-2231 A Flight Investigation of the Performance, Handling Qualities, and Operational Characteristics of a Deflected Slipstream STOL Transport Airplane Having Four Interconnected Propellers
Mar 1964
8 Report No. 2-53310/6R-6084 Analysis Report for the C142 Configuration Study Wind Tunnel Tests Contract# AF 33(657)-16202 LTV
Aug 9 1966
9 Report No. R221-004 Design Studies of High-Speed-Ratio STOL Aircraft Power Plant and Propeller Data Fairchild
Jun 29 1956
10 XC-142 Reviews Aug-Sep 1963 11 Report No. AER-E1R-13339 VHR-447 VTOL Tri-Service
Transport Vol. 1 Detail Specification Hiller, Vought, Ryan Apr 1961
12 Report No. AER-E1R-13342 VHR-447 VTOL Tri-Service Transport Vol. 4 Part 1 Stability and Control Hiller, Vought, Ryan
Apr 1961
13 Report No. AER-E1R-13352 VHR-447 VTOL Tri-Service Transport Vol. 11 Hydraulic System Hiller, Vought, Ryan
Apr 1961
14 Report No. AER-E1R-13354 VHR-447 VTOL Tri-Service Transport Vol. 13 Demonstration Program Report Hiller, Vought, Ryan
Apr 1961
15 A Review of the Structural Dynamic Characteristics of the XC-142A Aircraft by A.L. Head, Jr. Chance Vought
Jun 26-27 1963
16 Dynamic Model Testing of the XC-142 Aircraft by A.L. Head, Jr & W.D. Smith LTV
Sep 23-25 1963
17 Report No. 2-53310/4R939 Estimated Flying Qualities of the XC-142A V/STOL Assault Transport Contract# AF 33(657)-7868 LTV
May 22 1964
18 Report No. 2-53330/9R-6146 Evaluation of Propeller Forces and Moments at High Inflow Angles Including the Effects of Monocycle Action Contract# AF 33(657)-7968 LTV
Sep 19 1969
19 XC-142 VTOL Transport No. 23 Monthly Progress Report Contract# AF 33(657)-7868 LTV
Nov 1963
20 XC-142A System 478A System Package Program Mar 15 1965 21 Report No. 2-55120/2R789 XC-142 Growth Airplane
Payload and Cargo Compartment Size Study LTV May 1962
183
22 Report No. R-221-002A Interim Report No. 1 Design Studies of High-Speed-Ratio STOL Aircraft Contract# Nonr-1733(00)
Jul 29 1955
23 Report No. R-221-002C Interim Report No. 3 Design Studies of High-Speed-Ratio STOL Aircraft Contract# Nonr-1733(00)
Sep 30 1955
24 Report No. R-221-002H Interim Report No. 8 Design Studies of High-Speed-Ratio STOL Aircraft Contract# Nonr-1733(00)
Feb 29 1956
25 Report No. R221-010 Study of STOL Airplane with Direct-Lifting Turbojets M-221G Fairchild
May 31 1965
26 Report No. R221-003 Methods of STOL Airplane Analysis M-221G Fairchild
Jun 21 1956
27 Report No. R224B-005 M224B Vectored Slipstream Tests Contract# DA 44-177-TC-350 Fairchild
Nov 19 1956
28 Report No. R224-006 Interim Summary Report M-224B Contract# DA 44-177-TC-350 Fairchild
Dec 19 1956
29 Report No. R246-001 Jet Wing Configuration Studies Fairchild
Oct 28 1957
30 Short Take-Off and Landing for the High-Speed Aircraft by John K. Wimpress Boeing
Feb 1966
31 IRAD Review Aerodynamics of STOL Lift Systems May 1972 32 XC-142 Material Various 33 SAE 680645 Distributed Suctiion Boundary Layer Control
for High Lift by S.C. Roberts Miss. State Univ. Oct 7-11 1968
34 SAE 710464 The Future of STOL by Richard D. FitzSimmons & LTC William E. Thurman NASA
May 10-13 1971
35 SAE 710465 Comparison of STOL Design Criteria for Commercial and Military Transport Aircraft by Jesse C. Peaslee Boeing
May 10-13 1971
36 SAE 710468 Military/Commercial STOL Transport Commonality by Harold F. Kleckner McDonnell Douglas
May 10-13 1971
37 SAE 710469 STOL Engine Systems and Sensitivity Factors by Joel Godston Pratt & Whitney
May 10-13 1971
38 Synthesis of Future High Lift systems by Richard Scherrer Lockheed-California
Undated
39 AIAA No. 67-741 The Augmentor-Wing Research Program – Past, Present and Future by D.C. Whittley De Havilland Aircract, Canada
Oct 18-200 1967
40 ICAS Paper No. 68-07 Researches About the Use of STOL Aircraft in Civil Transport Aviation. Some Experimental Results on a STOL Aircraft Model by A. Salvetti Univ. of Pisa, IT.
Sep 9-13 1968
41 Aero Report 894 Preliminary Wind-Tunnel Investigation of a Method of Suppressing the Leading-Edge Stall on a Wing by Tangential Blowing by H.R. Chaplin
Mar 1956
184
42 NASA TN D-1857 Large-Scale Wind-Tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust
Sep 1964
43 NASA TN D-7034 Wind-Tunnel Investigation of a Four-Engine Externally Blowing Jet-Flap STOL Airplane Model
Dec 1970
44 NASA TN D-658 Ground Influence on a Model Airfoil with a Jet-Augmented Flap as Determined by Two Techniques
Feb 1961
45 FTD-MT-24-1674-71 Investigation of the Takeoff-Landing Characteristics of Short takeoff and Landing (STOL) Jet Aircraft by V.I. Surus
May 19 1972
46 USAAVLABS TR No. 68-19 Investigation of the Lateral/Directional Stability Characteristics of a Four-Propeller Tilt-Wing VTOL Model Contract# DA 44-177AMC-8(T)
Apr 1968
47 Report No. GD/C-64-063A STOL Technology Development and Systems Study General Dynamics/Convair
May 1974
DUCTED/SHROUDED PROPELLER & DOAK, DOUGLAS, HILLER PROPOSALS
94 1 Report No. GDC PIN 66-947 A Proposal for (AID) Addressed Infantry Delivery System Volume I – Advanced Development Technical Proposal General Dynamics
Nov 1966
2 NASA TN D-776 A Wind Tunnel Investigation of a 4Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing
Feb 1961
3 NASA TN D-981 Aerodynamic Characteristics of a Powered Semispan Tilting-Shrouded-Prepeller VTOL Model in Hovering and Transition Flight
Jan 1962
4 NASA TN D-1301 Aerodynamic Characteristics of a 4Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing
Apr 1962
5 NASA TN D-1491 Transition and Hovering Flight Characteristics of a Tilt-Duct VTOL Research Aircraft
Nov 1962
6 NASA TN D-1802 Flight Operating Problems and Aerodynamic and Performance Characteristics of a Fixed-Wing, Tilt-Duct, VTOL Research Aircraft
Jul 1963
7 SR-175 3-5 Ton Class VTOL Aircraft Doak 1965-1970 Time Period
Undated
8 Report No. ES 29793 V/STOL Design Studies Douglas Mar 11 1960 9 Report No. ES 29530 VTOL Propulsion System Study
Douglas Sep 25 1959
10 Report No. ES 29735 Preliminary Results of an Analytical Study of Shrouded Propeller Inlet Design Requirements Douglas
Jul 8 1960
185
11 Report No. ES 29674 Model D-793 US Army Surveillance Aircraft Study ASR 2-60 Douglas
Jan 25 1960
12 Report No. ES 29675 Model D-791 VTOL/STOL Tactical Transport Aircraft for the US Army ASR 3-60 Douglas
Jan 25 1960
13 Report No. ES 29759 V/STOL Logistics Aircraft Study SR-175 Vol. I Technical Analysis Douglas
Jan 26 1960
14 Report No. ES 29759 V/STOL Logistics Aircraft Study SR-175 Vol. II Operational Analysis Douglas
Jan 26 1960
15 Report No. ES 40371 Operational Improvement Modification for Army DOAK VZ-4DA Aircraft Douglas
Jun 5 1961
16 Encl. (1) to B-25-M-870 Small Parasite VTOL Aircraft Capabilities
Undated
17 Report No. 680.2 Truck Test Stand Tests of Hiller Airborne Personnel Platform Phase II Hiller
Sep 15 1955
18 Report No. 56-108 Aerodynamics of Ducted Propellers as Applied to the Platform Principle Model No. 1031-A Hiller
Nov 30 1956
19 Report No. ARD No. 111 Some Remarks on the Control and Stability Characteristics of the Flying Platform Hiller
Apr 26 1956
20 Report No. ARD No. 112 Stability Analysis of Flying Platform in Hovering and Forward Flight Hiller
Oct 12 1956
21 Report No. ARD No. 198.1 Proposal for Static Tests of a Ducted Propeller Slipstream Deflection System Hiller
May 17 1958
22 Report No. ARD-233 Dynamic Stability Analysis of Ducted Fan Type Flying Platforms Contract# NONR 1357(00) Phase IV Hiller
May 29 1959
23 Report No. 56-110 Summary Report – Phase III – Airborne Personnel Platform Contract# Nonr 1357(00)
Nov 30 1956
24 Report No. FTD-HT-66-273 Applications of Ducted-Fan Propellers in the Ground Forces by J. Soulez-Lariviere (from French)
Oct 14 1966
25 NORD Cadet 500 Information 1967-1969 26 Piasecki PA-2 Blueprints 1955 27 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale
Model PA-2C VTOL Aircraft Part I – Power Off Tests Feb 1958
28 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale Model PA-2C VTOL Aircraft Part II – Tee-Tail Tests
May 1958
29 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale Model PA-2C VTOL Aircraft Part III – Propulsion System calibration
Mar 1960
30 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale Model PA-2C VTOL Aircraft Part IV – Power Tests of a VTOL Configuration
Mar 1960
186
DEFLECTED SLIPSTREAM V/STOL 95 1 Report No. 407 The Static and Dynamic Stability of a
Deflected Slipstream Vehicle by G.A. Cincotta & H.S. Dunn Princeton Univ.
Mar 1958
2 Report No. 437 An Investigation of the Fundamental Parameters Which Govern the Aerodynamics of Various Wing-Propeller Combinations as Related to Vectored Slipstream Aircraft by Norman R. Augustine Princeton Univ.
Oct 1958
3 Report No. LR 11908 Aerodynamics CL-346 Dispersed Site VTOL Fighter-Bomber Design Study Contract# AF 18(600)-1642 Lockheed-California
Dec 5 1956
4 Report No. 13063 VTOL-STOL Test Bed Research Aircraft Summary Report Lockheed-California
May 22 1958
5 Report No. 13064 VTOL-STOL Test Bed Research Aircraft Aerodynamics Report Lockheed-California
May 22 1958
6 Report No. 8820-3 Static Characteristics of the Ryan Model 88 Monoplane and Biplane-Type Apparatus for Deflecting a Propeller Slipstream Through Large Angles Contract# NOnr-1710(00) Ryan
Apr 27 1956
7 Report No. 8818-4 TR – Parametric Studies Pertaining to Direct Ascent Aircraft Employing the Deflected Slipstream Principle Contract# NOnr-1710(00) Ryan
Apr 15 1956
8 Report No. 8818-3 Summary Report – Direct Ascent Aircraft Employing the Deflected Slipstream Principle Contract# NOnr-1710(00) Ryan
Apr 15 1956
9 Report No. 709 Report on Wind Tunnel Tests of a 0.20 Scale Model of the DOAK Model 16 Airplane Cal. Institute of Technology
Jan 2 1959
10 Report No. PDR-674A-2 Advanced Shipbased/Dispersed-Site VTOL System (Nutcracker) Grumman
May 1975
11 NASA CR-152132 Study of Aerodynamic Technology for VTOL Fighter/Attack Aircraft Phase I Final Report Contract# NAS2-9772 BY LTV
May 1978
12 Deflected Slipstream Aircraft Photos and Articles Various 13 NASA TN D-649 Loads Induced on a Flat-Plate Wing by
an Airjet Exhausted Perpendicularly Through the Wing and Normal to a Free-Stream Flow of Mach Number 2.0
Mar 1961
14 Report No. DS 210.3 Wind Tunnel report DOAK Model 18 Contract# DA-44-177-TC-351 Doak
Aug 1 1958
15 Dornier Do231 VSTOL Transport Brochure (in German) Undated 16 Report No. DS 210.1 Design, Fabrication, and general
Aerodynamics report of the DOAK Model 16 20% Scale Low-Speed Wind Tunnel Model Contract# DA-44-177TC-351 Doak
Dec 6 1957
187
17 Report No. DS-208 Revision A Control System Report Contract# DA-44-177-TC-351 Doak
Jul 31 1959
18 Phase II 50 Hour Ground Test Report Doak Model 16 Jul 31 1959 19 Proposal 50-Hour Pre-Flight Ground test Doak Model 16
VTOL Flight Test Vehicle Undated
20 Propulsive Wing Articles, Photos and Brochures Various 21 AHS 24th Annual Forum No. 203 A Promising Concept for
the Joint Development of Military Intra-Theater and Commercial Inter-Urban VTOL Transports by T. Gardner Hill Lockheed-Georgia
May 8-10 1968
22 Report No. D6-9904 Ground Survivability of Aircraft – II, VTOL Dispersal – Survival Boeing
Dec 26 1963
23 AFFDL-TR-70-88 Background Information and User Guide for MIL-F-83300 – Flying Qualities of Piloted V/STOL Aircraft
Nov 1971
VTOL, DOWNWASH 96 1 Report No. LR 20468 Downwash Effects Study Contract#
F33657-67-C-0703 Lockheed-California C.A. 1962
2 V/STOL Aircraft Downwash Characteristics and Simulated Forest Rescue Test ASD
Sep 1967
3 V/STOL Technology Presentation 1978 4 The Value of Various Technology Advances for Several
V/STOL Configurations by W.B. Peck & A.H. Schoen Boeing-Vertol
Sep 13-15 1978
5 Summary of V/STOL State-of-the-Art Bell Undated 6 Report No. D2-4600 VTOL General Information Boeing Sep 9 1959 7 Report No. 65-978-004 A Review of Technical Literature
on Jet Propelled Vertical Takeoff and Landing Aircraft Bell
Jan 3 1953
8 AHS Dayton Chapter Notes and Vuegraphs May 21 1982 9 Report No. LR 14218 V/STOL Airplanes Lockheed-
California Dec 28 1959
10 Report No. D6-6892 Rapid Site Preparation Presentation Boeing
Feb 1964
11 Journal of the Royal Aeronautical Society Volume 66 Number 614 VTOL and STOL: Simple Solutions to Some of the Operating Problems During Take-off and Landing by J.R.C. Fearon & D.H. Norman Rolls-Royce
Feb 1962
12 Survey of Available Material on Downwash Prediction US Army Material Command
Feb 1971
13 Propulsion/Airframe/Aerodynamics Integration Presentation
Undated
14 V/STOL Aircraft Technology Assessment USAF Flight Dynamics Lab
Oct 1968
188
15 WADD TN 59-374 A Study of Vertical and Short Take-Off Landing Propulsion System State-of –the-Art
Dec 1959
16 Report No. 64575 Assault Transports 1960-1965 Logistics Systems Study ORD 150 Lockheed-Georgia
May 30 1958
17 Material from By Winborn Early VTOL Various 18 Report No. DR-1744 Level Attitude, Propellered VTOL
Comparative Study USNavy BuAir Mar 1957
19 NASA TN D-733 Review of Basic Principles of V/STOL Aerodynamics
Mar 1961
20 Rotor Recovery Systems Various 21 V/STOL Aircraft Designs Article for AAHS plus
Supporting Documents Undated
22 SAB Briefing Papers 1967 23 WADC TR58-564 Appendix I Bibliography of Report
References C.A. 1958
24 Report Bibliography – Tail-Sitter Aircraft May 31 1972 25 Report No. PAR 238/10 Report of Ad Hoc Group on Short
and vertical Take-Off and Landing Aircraft Nov 15 1956
26 Design Considerations for VTO Aircraft Hiller Undated 27 Book on Vertical Flight In German Jan 1961 28 Miscellaneous Articles and Papers on Vertical Flight Various
TILT-WING, X-18(HILLER MODEL 1051), GEM, STOPPED-ROTOR COMPOUND HELO
97 1 X-18 Correspondence Hiller 1960-1961 2 X-18 Blueprints Hiller Sep 1956 3 X-18 Inspection Report Oct 27-28 1959 4 Report No. 461.3 A Simplified Theoretical Investigation of
a Wing-Propeller Combination Through a Range of Angleof-Attack from 0o to 90o and a Comparison with Experimental Results Hiller
Oct 15 1955
5 Report No. 56-65 The Aerodynamic Characteristics of Tilt-Wing Propelloplane Model 1051 Hiller
Jul 17 1956
6 Report No. 56-79 Specification for Ground testing of the X-18 Tilt-Wing, VTOL, Test Bed Contract# AF 33(600)32749 Hiller
Sep 14 1956
7 Report No. 56-68 Wind Tunnel Test Program for Model 1051 Tilt-Wing Flying Test Bed Hiller
Aug 7, 1956
8 Report No. 56-78 Specification for Flight Testing of the X18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)32749 Hiller
Sep 14 1956
9 Report No. 56-97 Preliminary Design Study Summary Report – Tilt-Wing, VTOL, Test Bed, X-18 Contract# AF 33(600)-32749 Hiller
Oct 11 1956
189
10 Report No. 57-58-1 Estimated Flight Test Performance – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)32749 Hiller
May 31 1957
11 Report No. 57-58-2 Estimated Flight Test Performance – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)32749 Hiller
May 31 1957
12 Report No. 57-114-3 Ground and Lift-Off Test Schedule for the X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
Oct 7 1957
13 Report No. 58-74 An Analysis of the Variation of Pitching Moment in Transition Flight – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
May 27 1958
14 Report No. 58-80 Flight Test Schedule for the X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
Nov 1 1958
15 Report No. 58-130 Force Testing of a One-Eighth Scale Model X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
Oct 6 1958
16 Report No. 58-132 Available Thrust Analysis – J34-WE36 Pitch Control Engine Installation X-18 Aircraft Hiller
Oct 28 1958
17 Report No. 58-136 Remote-Controlled Free-Flight Test of a 1/8-Scale Model X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
Oct 31 1958
18 Report No. 58-154 Estimated Performance Report X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
Dec 1 1958
19 Report No. 59-15 Flight Simulation of the X-18 in Hover – Edwards AFB Contract# AF 33(600)-32749 Hiller
Feb 4 1959
20 Report No. 59-34 Airplane Stability and Control – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
May 15 1959
21 Weight and Balance Status Report No. 37 X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller
Nov 15 1959
22 Report No. HTC 64-38 Interim Report Rotor-Wing Concept Study Contract# Nonr-4588(00) HTC
Oct 1964
23 Report No. 859-099-001 Trailing Rotor Convertiplane Model Rotor System Wind Tunnel Test Contract BHC W.O. 4280-059; R.T. 059-1 Bell
Aug 14 1964
24 Report No. 5059-099-001 Trailing Rotor Convertiplane Configuration Study Twin Rotor TRC-1A Contract# BHC WO 5059; RT 059-1 Bell
Feb 10 1965
25 Report No. SEP-6260 Stowed Rotor V/STOL Proposal Sikorsky
Oct 30 1964
26 Report No. LR 17844 Proposal for a Stopped Rotor Research Compound Helicopter Lockheed-California
May 7 1964 Rev Jun 3 1964 Rev Aug 10 1964
190
27 Proposed Program for R&D Hot Cycle Rotor-Wing High Speed VTOL Aircraft Concept Hughes
Undated
28 Report No. 2017-933001 GEM Morphology Study Progress Report Contract# Nonr-3074(00) Bell
Nov 14 1960
29 Report No. ZP-319 Study of Impact Loads and Motions of Ground Effect Machines (GEM) Report to Contractors Meeting Convair
Nov 16-18 1960
30 Report No. AP-5024-R Third Progress Report GEM Propulsion System Study Contract# Nonr 3024 Garrett
Nov 11 1960
31 Letter 65T-0209/2189 Progress Report No. 1 Rotor/Wing Wind Tunnel Tests at David Taylor Model Basin: Stopped Rotor Tests Contract# Nonr 4588(00) HTC
Apr 7 1965
32 Progress Report No. 2 Rotor/Wing Wind Tunnel Tests at David Taylor Model Basin: Stopped Rotor Tests HTC
May 26 1965
33 Alouette 3 Brochure SUD Jan 1960 34 SA. 3210 Brochure SUD Feb 1960 35 Alouette II Brochure SUD Undated 36 Djinn IIIB Brochure SUD Jan 1960 37 Djinn Description Brochure SUD Undated 38 Fiat 7005 Helicopter Brochure Fiat Oct 1964 39 Fiat 7005 Photos Fiat C.A. 1964 40 Fiat 7002 Blueprints 1958 41 Lindenbaum File – Assorted Photos and Sketches Undated
VECTORED THRUST & DIVERTED SLIPSTREAM VTOL
98 1 NACA TN 3919 Investigation of Effectiveness of a Wing Equipped with a 50-Percent-Chord Sliding Flap, a 30Percent-Chord Slotted Flap, and a 30-Percent-Chord Slat in Deflecting Propeller Slipstreams Downward for Vertical takeoff
Jan 1957
2 NASA TN D-89 Wind-Tunnel and Piloted Flight Simulator Investigation of a Deflected-Slipstream VTOL Airplane, The Ryan VZ-3RY
Nov 1959
3 NASA TN D-331 An Examination of Handling Qualities Criteria for V/STOL Aircraft
Jul 1960
4 NASA TN D-433 Low-Speed Measurements of Static and Oscillatory Lateral Stability Derivatives of a 1/5-Scale Model of a Jet-Powered Vertical-Attitude VTOL Research Airplane
Sep 1960
5 NASA TN D-735 Handling Qualities Experience with Several VTOL Research Aircraft
Mar 1961
6 Report No. N79-10024 Study of Aerodynamic Technology for VSTOL Fighter/Attack Aircraft – Horizontal Attitude Concept Northrop
May 1978
191
7 Report No. FTC-TR-66-30 Flight Evaluation of the XV-5A VSTOL Aircraft
Mar 1967
8 Report No. 407 Dynamic Stability Analysis of a VTOL Vectored Slipstream Vehicle During Transition by Guy G. Williamson Princeton Univ.
Mar 1958
9 Report No. 535 The Static and Dynamic Stability of a Deflected Slipstream Vehicle by G.A. Cincotta & H.S. Dunn Princeton Univ.
Apr 1961
10 Report No. UER 18-601 Maintenance and Rigging Manual for Air & Space Model 18A Gyroplane Air & Space
Mar 30 1965
11 Report No. TS 3080 An Evaluation of the Harrier AV-8A and the Pegasus Engine Rolls-Royce/British Aerospace
Dec 1978
12 Recent Ejector Technology Programs at the Naval Air development Center by K.A. Green
C.A. 1979
13 Status and Trends in Powered Lift Systems by Peter G. Kappus
Undated
14 A Simple Graphical Method for Evaluating the Effect of Thrust Vector Tilt on the Aircraft Performance by Peter Bielkowicz
Jul 1 1968
15 The Rebirth of the Tiltrotor by Robert R. Lynn Bell Jun 1992 16 Vectored Thrust – Europe Photos & Graphs Various 17 Vectored Thrust – Dassault(Fr) Photos Various 18 Vectored Thrust - Hawker-Sidderly (UK) Photos &
Articles Various
19 Vectored Thrust – Fiat(It) Photos Various 20 Vectored Thrust – VFW(Ge) Photos & Articles Various 21 Vectored Thrust – VFW VAK-191B Photos & Articles Various 22 Vectored Thrust – Hawker-Sidderly KESTREL P-1127
Photos & Articles Various
23 Vectored Thrust US/FRG Fighter Photos Various 24 Vectored Thrust – Short SC.1 Photos Various 25 Vectored Thrust – Dassault(Fr) MIRAGE III Photos Various 26 Vectored Thrust – Bell D-188A Article Undated 27 Vertical Thrust – Boeing Tri-Service Transport Various 28 Vertical Thrust – USSR Various 29 Vertical Thrust – Northrup Various 30 Vertical Thrust – SUD/EWR Various 31 Vertical Thrust – Vought Various 32 Vertical Thrust - Hiller/Vought/Ryan XC-142A Various 33 Custer Channel Wing (CCW) Concept and Information 1971 34 Roadable Aircraft Various 35 Individual Mobility Concepts Various 36 Lift-Fan Material Various 37 Report No. 2-60-953001 V/STOL Fighter-Bomber State
of-the-Art Presentation Bell Oct 1960
38 WASP II – Preliminary Airworthiness Evaluation Jun 1982
192
39 Foreign V/STOL Progress 1965 40 Turbo-Jet/Turbo-Fan MVTOL Technology Status NAA Nov 1965 41 Turbulence Measurements in an Ejector Wing Flow Field
by G.D. Catalano – LSU, H.E. Wright & D. Stevens – AFIT, K.S. Nagaraja – AF Wright Labs
Aug 3-5 1981
42 AIAA Paper No. 71-980 The V/STOL Projects of the Federal Republic of Germany by Drury W. Wood Dornier
Oct 25-28 1971
43 SAE No. 680644 Low-Speed Characteristics of High-Performance Lift-Engine V/STOL Aircraft by Jerry P. Barrack & Jerry V. Kirk NASA Ames
Oct 7-11 1968
44 Kestrel P-1127 Evaluation Trials by Major John A. Johnston USA
Undated
45 Studies of the Transition of VTOL-Aircraft by S. Gunter Undated 46 ICAS Paper No. 68-49 Developing a V/STOL Combat
Aircraft by B.P. Laight Hawker-Sidderly Sep 9-13 1968
47 AHS Paper No. 234 Experience of and Methods to be Used in Clearing a Jet-Lift Aircraft for Service Use by Ian A. Fisher
May 8-10 1968
48 AHS Paper No. 220 Control Characteristics of Vectored Thrust V/STOL Vehicles in the Transition Regime by Alan V. Coles Bell
May 8-10 1968
49 IAS Paper No. 624 Reverse Thrust, Vertical Lift, and Side Force by Means of Controlled Jet Deflection by Leonard Meterhoff – Brooklyn Polythecnic & Stanley Meterhoff – Eastern Research Group
Jan 23-26 1956
50 AIAA Paper No. 78-1082 Aerodynamic Effects Induced by a Vectored High Aspect Ratio Nonaxisymmetric Exhaust Nozzle by Douglas L. Bowers AF Flight Dynamics Lab
Jul 25-27 1978
51 AIAA Paper No. 78-956 Design and Experimental Studies of a Type A V/STOL Inlet by H.C. Potonides, R.A. Cea & T.F. Nelson Grumman
Jul 25-27 1978
52 AIAA Paper No. 78-1022 Installed Performance of Vectoring/Reversing Nonaxisymmetric Nozzles by P.E. Hiley, D.E. Kitzmiller & C.M. Willard McDonnell Douglas
Jul 25-27 1978
53 Miscellaneous VTOL Photos & Articles Various 54 Report No. 62B125 XV-5A Detail Aircraft Specifications
Contract# DA44-177-TC-715 Ryan Dec 15 1962
55 Report No. 477 A Stability Analysis of Tilt-Wing Aircraft (Analytical) by Charles H. Cromwell III & Henry E. Payne III Princeton Univ.
May 1960
56 Report No. 478 A Stability Analysis of Tilt-Wing Aircraft (Experimental) by Charles H. Cromwell III & Henry E. Payne III Princeton Univ.
May 1960
193
SERIES IX: Escape Systems, Crash and Rescue, 1929-1999
Box File Description Date
ESCAPE SYSTEMS 99 1 Report R-760 Technical Proposal for Stowable Aircrew
Vehicle Escape Rotoseat AERCAB Concept Volume I Kaman
Oct 11 1968
2 Report PDR-306-1 Grumman Project 306 Surface to Air Retrieval of Heavy Spacecraft by Fixed-Wing Aircraft Contract# NAS9-195
Jun 1962
3 Report P-3003 Interim Progress Report IPR-4 SR-49759 Retrieval Concept Study
Feb 28 1961
4 Saver AERCAB Test Data & Results Briefing Notes C.A. 1970 5 Discretionary Descent Using Rotary Wings by B.
Lindenbaum Undated
6 AERCAB Phase III Program Review Fairchild-Hiller Mar 2 1971 7 Proposal (09-0198) for the Development of a Prototype
Aircraft Escape System Parsons Corp. Apr 21 1969
8 Report GAP-68-5189 Integrated Aircrew Escape/Rescue System Capability (AERCAB) Goodyear
Oct 10 1968
9 Report GER 8597 Summary ER on the Development of a Two Place Inflatoplane Contract NOnr 1860(00)
Jul 31 1958
10 Goodyear Inflatoplane Brochures 1971 11 Report No. 15-94-1 Report on Performance Tests of
Rotochute Models Contract# W33-038 ac-18190 Oct 8 1948
12 Report No. 15-130-1 Basic ER Rotochute Phase I Contract# W33-038 ac-18190
Nov 9 1948
13 Report No. 55230 Development of “Rotochute” Rotary Wing Air Brake GE
Nov 3 1947
14 Report TSEAL2-672-1-2 Flight Tests of the Gyro-Container
Mar 30 1945
15 Proposal 520/35-4/RL Development of the Helicycle Vehicle Revision A Wyle Labs
Jun 7 1958
16 NACA RM L54B12a Flight Tests of a Man Standing on a Platform Supported by a Teetering Rotor
Mar 24 1954
17 Mobility Effectiveness of Air Cushion Craft by William C. Walter
Undated
18 NASA TN D-189 Static-Stability of a Stand-On Type Helicopter with Rigid Blades, Including a Comparison of Theory
Feb 1960
19 Discretionary Descent – Clippings and Information Various 20 Discretionary Descent – Project File Various 21 Report No. ARD-233 Dynamic Stability Analysis of
Ducted Fan Type Flying Platforms Contract# NONR 1357 (00) Phase IV
May 29 1959
194
22 AFFDL-TR-66-97 Study of Heavy Equipment Aerial Delivery and Retrieval Techniques
Jan 1967
23 Approaches to Individual Lifting Devices by B. Lindenbaum
Undated
24 Report GER-8465 Proposed Air Rescue System (Mother-Daughter Concept) Goodyear
Dec 18 1957
25 NACA RM L52D10 Preliminary Experimental Investigation of the Flight of a Person Supported by a Jet Thrust Device Attached to His Feet
Jan 15 1953
26 AHS Newsletter Vol. 2 No. 12 Dec 1956 27 Report No. 404 Stability and Control of Unducted Stand-
On Helicopters: Preliminary Theoretical and Flight Test Results Contract# DA 44-177-TC-392 Princeton Univ.
Nov 1957
28 Report TR-737 Jet Lift Concepts to Improve Individual Soldier Mobility Thiokol
Jun 3 1959
29 Report TR 3355-1 Rocket Jump Belt Thiokol Aug 1 1960 30 Introducing the Reaction Motors – Rocket Jump Belt
Thiokol Undated
31 Jump Belt Photos and Articles Various 32 Report ARD-236 Summary Report Airborne Personnel
Platform Contract# Nonr 1357(00) Jun 9 1959
LOCAL CRASH RESCUE HELICOPTERS 100 1 Report AU-74b Model Specification XR-9B Helicopter
G&A Aircraft Jul 4 1945
2 FSTC-HT-23-911-72 Results of the Theory of Rotor Flow According to Miller and Scully (W. German)
Aug 23 1972
2 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Cessna
Undated
3 The Piasecki Story of Vertical Flight Brochure C.A. 1969 4 AF TR No. 6162 Development of the G&A Model XH-9,
XH-9A, and XH-9B Helicopters May 1950
5 Report No. 47-945-045 Model 47J Local Crash Rescue Mission – Weight and Balance
Jul 20 1956
6 Hughes OH-6A Physical Configuration and Flight Characteristics
Undated
7 AF TR No. 6272 Performance Testing Methods for Helicopters
Dec 1950
8 Report No. 57-76 Two-Place Observation Helicopter Preliminary Design Study Hiller
Aug 1957
9 Report HTC-AD 64-25 Design Specification – Hughes 300 Model 269B Helicopter
Undated
10 Report No. SER-100 Stress Analysis of Main Rotor Head Contract# W535 AC-29845 DA W535 AC 2514 Sikorsky
Aug 1 1943
195
11 Report No. X-1513 Flight Test Report XR-4B Section III – Synchronization of the Throttle with the Main Pitch Control Contract W535 AC-29845 Change 1 DA W535 AC 2514
Aug 27 1943
12 AFFTC 52-41 Phase IV Performance Tests of the H-23B Helicopter
Dec 22 1952
13 DAVI – Dynamic Antiresonant Vibration Isolator Kaman Undated 14 Development of the Helicopter Lockheed Dec 1967 15 Progress in Rotor-Blade Aerodynamics by P.F. Yaggi &
I.C. Statler USAAMRDL C.A. 1971
16 AFFTC-TR-57-12 H-13H Phase IV Performance Test Jul 1957 17 AFFTC-TR-57-12 H-13Addendum no. 1 Phase IV
Performance Mar 1958
18 FSTC-HT-1348-71 Specifics of Aerodynamics of the Lifting Rotor of a Helicopter by A.M. Mkhitaryan (USSR)
1970
19 YH-41 (Modified) Air Force Local Crash Rescue helicopter Preliminary Model Specification Cessna
Jul 30 1956
20 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Performance Report Cessna
Jul 30 1956
21 Report HTC-AD 369-Y-8003 Detail Specification for a Single Engine, Single Main Rotor Light Observation Helicopter Army Model Designation OH-6A Contract IFB AMC(T)23-204-65-222
Apr 21 1965
22 AFFTC-TR-59-33 YH-40 Performance Evaluation Jan 1960 23 AWST Article Hughes269A Aimed at Untapped market Jan 15 1962 24 NACA TN 2154 An Analysis of the Autorotative
Performance of a Helicopter Powered by Rotor-Tip Jet Units
Jul 1950
25 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Weight and Balance Report Cessna
Jul 30 1956
26 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Summary Report of Flight Tests (CH-1A) Cessna
Jul 30 1956
27 Gazelle Brochure Undated 28 Enstrom Guardian II Police/Ambulance Helicopter
Brochure Undated
29 FTD-HC-23-0697-72 Bolkow BO 105 Multipurpose Helicopter (W. German)
Aug 31 1972
30 Optimization of Design Data for Reaction Drive Helicopters by Werner Goller Dornier
Jan 1970
31 Bristol 173 (Hafner) Parts Pictures Undated 32 Doman-Frasier Helicopters – Rotor Head Assembly
Blueprint May 17 1948
33 Design Details of Aeronautical Products, Inc. Helicopter Jun 1945 34 Principles of Helicopter Design (INCOMPLETE) by
Wayne Wiesner Hiller Undated
196
35 NASA TN D-38@ Effect of Blade Cutout on Power Required by Helicopters Operating at High Tip-Speed Ratios
Sep 1960
36 Ground and Flight Test Experience with the Westland Scout Hingeless Rotor Helicopter
Sep 20-23 1971
37 AGARD Advanced Rotorcraft Meeting Notes and Papers Sep 20-23 1971 38 Limitations in Helicopter Design by J.A.J. Bennett Feb 22 1947 39 MC-9 Helicopter Blueprints Mar 5 1952 40 Kaman Model K-190 Utility helicopter Brochure Undated 41 Assorted Helicopter Brochures Undated 42 AHS Assorted Presentations Various 43 Use of Thrust and Lift Augmentation for Increasing
Helicopter Operating Speed by Donald W. Robinson Jr. Kaman
Jan 23 1963
44 What’s Wrong with Today’s helicopters by F.N. Piasecki Jun 20 1950 45 Miscellaneous Articles Various 46 Patent Copies, Helicopter Related
LOCAL CRASH/ RESCUE HELICOPTER & ROTOR AERODYNAMICS
101 1 Report No. DR-210 General Description and Preliminary Model Specification Doman LZ-5-3 Local Crash Rescue Helicopter
Jul 24 1956
2 Report No. DR-211 Preliminary Weight and Balance Report Doman LZ-5-3 Local Crash Rescue Helicopter
Jul 27 1956
3 Report No. DR-212 Preliminary Performance Report Doman LZ-5-3 Local Crash Rescue Helicopter
Jul 27 1956
4 Report No. DR-216 Design, Development, Testing Service, Life and Overhaul Doman LZ-5-3 Local Crash Rescue Helicopter
Jul 30 1956
5 Report No. DR-228 Performance Characteristics of the Doman LZ-5 with the Artouste III or Turmo III French Gas Turbine
Dec 12 1956
6 CAA Approved Rotorcraft Flight Manual for Model LZ-5 Helicopter
Dec 30 1955
7 Drawings and Photographs – Crash Rescue, Uses and Applications, and Design Features Doman LZ-5-3 Local Crash Rescue Helicopter
C.A. 1956
8 USAAVLABS TR 69-94 An Experimental Investigation of the Effects of Rotor Head Configuration and Fuselage Yaw on the Wake Characteristics and Rotor Performance of a 1/8 Scale Helicopter Contract# DA 44-177-AMC-203(T)
Feb 1970
9 State of the Art Advancement in Helicopter Design Lockheed-California
Oct 1963
10 Report No. 204-099-308 Moment of Inertia Calculations – XH-40 Helicopter Contract# AF 33(600) 30229
Dec 19 1956
197
11 Report No. TB-1288-F-1 / WADC TR 59-754, Part I Flight Test Determination of Lateral Stability and Control Derivatives for a Single Rotor Helicopter
Aug 1959
12 Technical Papers – Rotary Wing Pre 1946 13 Report No. 100 Helicopter Blade Analysis Contract# W33
038 AC5238 Princeton Univ. Jan 31 1947
14 Report No. BB-437-S-1Helicopter Dynamic Stability and Control Studies Part I Contract# W33-038 ac 14248 Exh. J Cornell Univ.
Sep 29 1950
15 Report No. BB-437-S-2 Helicopter Dynamic Stability and Control Studies Part II Contract# W33-038 ac 14248 Exh. J Cornell Univ.
Jun 1 1951
16 An Aerodynamic Comparison of Two Airfoils Based Upon Full Scale Rotor Whirl Tests by Lt. Hamilton R. Harris & Henry R. Velkoff WADC
Sep 1958
17 R. & M. No. 2695 Wind-Tunnel Tests on a 12-ft Diameter Helicopter Rotor
1953
18 Helicopter Blind Flying Trials Fairey Aviation Ltd. Undated 19 WADC TR 55-438 The Determination of Helicopter
Longitudinal Stability Derivatives from Flight Test Data Part II
Mar 1959
20 NACA Wartime Report Airfoil Section Data from Tests of 10 Practical-Construction Sections of helicopter Rotor Blades Submitted by the Sikorsky Aircraft Division, United Aircraft
Sep 1944
21 NACA MR L5C10 Flight Tests of the Sikorsky HNS-1 (Army YR-4B) Helicopter Part I
Mar 1945
22 NACA MR L5D09a Flight Tests of the Sikorsky HNS-1 (Army YR-4B) Helicopter Part II
Mar 1945
23 NACA MR L5C29a Full-Scale-Tunnel Performance Tests of the PV-2 Helicopter Rotor
Apr 1945
24 NACA Restricted Bulletin L5K02 Aerodynamic Characteristics of Four NACA Airfoil sections Designed for Helicopter Rotor Blades
Feb 1946
25 SAE 1999-01-5609 Rotary Wing Flight Display Test and Evaluation by Richard L. Newman Crew Systems
Oct 19-21 1999
26 AIAA 99-3421 The Fluid Dynamics of Rotor Wakes: Theory, Computation and Experiment (Invited) by A.T. Consilk Ohio State Univ.
Jun28-Jul 1 1999
27 Report No. 63B063 Ryan Vertiwing Jul 15 1963 28 Report No. HTC-AD-66-1 TR Hot Cycle Rotor/Wing
Composite research Aircraft Section I Summary of Design HTC
May 1966
29 High Speed VTOL Recovery/Transport Aircraft HTC C.A. 1966 30 Report No. LR 21776 Responses to Questions Regarding
Stoppable Rotor Concepts Lockheed-California Aug 19 1968
198
31 Report No. 67-1 Reverse-Velocity Rotor Program Fairchild-Hiller
Nov 15 1967
32 TCREC TR 62-109 An Experimental Investigation of a Second Harmonic Feathering Device on a UH-1A Helicopter Contract# DA-44-177-TC-806
Jun 1963
33 AHS #603 Design Considerations of Circulation Control Blades by Robert M. Williams & Ernest O. Rogers Naval Ship R&D Center
May 1972
34 R. & M. No. 2997 Second Harmonic Control on the Helicopter Rotor by W. Stewart
Aug 1952
35 NASA TN D-73 Comparison of Calculated and Measured Stall Boundaries of a Helicopter Rotor at Advanced Ratios from 0.3 to 0.4
Sep 1959
36 The Propulsion of Helicopter Rotors by Edward A. Stalker Univ. of Michigan
Undated
37 Helicopter Photos, Articles and Hand Written Calculations C.A. 1949 38 An Introduction to Soviet Helicopters Brown & Shaw
Company Oct 1962
39 R. & M. No. 331, 1132, 1157 Pre 1929 40 NACA RM L51H20a Some Flying-Qualities Studies of a
Tandem Helicopter Oct 1951
41 NACA RM L53F15a Studies of the Speed Stability of a Tandem Helicopter in Forward Flight
Aug 13 1953
42 NACA TN 1799 On the Flying Qualities of Helicopters Jan 1949 43 NACA TN 2309 Charts for Estimation of Longitudinal-
Stability Derivatives for a Helicopter Rotor in Forward Flight
Mar 1951
44 NACA TN 2459 Some Effects of Varying the damping in Pitch and Roll on the Flying Qualities of a Small Single-Rotor Helicopter
Jan 1952
45 NACA TN 3156 Charts for Estimating Tail-Rotor Contribution to Helicopter Directional Stability and Control in Low-Speed Flight
May 1954
46 NACA TN 3201 Directional Stability Characteristics of Two Types of Tandem Helicopter Fuselage Models
May 1954
47 NACA TN 4330 Flow Induced by a Rotor in Power-On Vertical Descent
Jul 1958
48 NASA TN D-97 A Note on the Calculation of Helicopter Performance at High Tip-Speed Ratios
Sep 1959
49 F-TS-688-RE Longitudinal Stability of the Helicopter in Forward Flight by K. Hohenemser (from German)
Aug 1946
50 F-TS-691-RE Lateral Stability of the Helicopter in Forward Flight by K. Hohenemser (from German)
Aug 1946
51 F-TS-692-RE The Pull-Up of the Helicopter by K. Hohenemser (from German)
Aug 1946
199
52 F-TS-1002-RE The Dynamic Stability of Helicopters with Articulated Rotors by Sissingh (from German)
Sep 1946
53 F-TS-1004-RE The Theory for the Control of the Blade Angle of the Helicopter by K. Hohenemser (from German)
Sep 1946
54 F-TS-1005-RE Theory of Oscillations of Blades in the Plane of Rotation by Dr. Kurt Hohenemser (from German)
Sep 1946
55 F-TS-1006-RE Theory of Helicopter Control in Hovering Flight by Dr. Kurt Hohenemser (from German)
Sep 1946
SERIES X: Power Plants, Propellers, RPV, Drone, Small Tactical Aerial Vehicle, and STAMP, 1930-1981
Box File Description Date
RPV/DRONE 102 1 MIL-A-8860(ASG) Military Specification: Airplane
Strength and Rigidity, General Specification for May 18 1960
2 Airplane and Runway Floatation, Document and Pamphlet Boeing
Jul 1979
3 Navy Remotely Piloted Vehicles (RPVS) for Non-Aviation Ships
1976
4 Remotely Piloted Vehicles and Recovery Systems, Pamphlets and Articles
1976
5 Teleplane Briefing Nov 22 1971 6 Rotor Recovery System-Horizontal Type, Notes and
Calculations May 25 1976
7 Balloon Based Recovery System for RPV Notes, Drawings and Calculations
Oct 6 1977
8 VTOL Drone for Army Battlefield Use, Notes and Calculations
1974-1976
9 RPV Correspondence 1976 10 Stoppable Rotor VATOL, Notes and Drawings 1976 11 Para Drone Tasker Systems 12 AFFDL(PTB) TM-71-1 Teleplane Preliminary Design
Study Dec 1971
13 IR&D Project# 0103D8 Summary Report on Low Cost Rigid Structures for Drones Goodyear
Aug 8 1972
14 Drones – XMQM-105 and XBQM-106 Pamphlets 15 Drones for Aerodynamic and Structural Testing (DAST) Aug 1979 16 MQM-107 Overview Pamphlet Undated 17 MQM-107A Overview Pamphlet Undated 18 Mini-RPV Concept Articles 1977 19 RPV Industry Conference: Agenda, Notes, Handouts and
Drawings Feb 23-24 1978
20 NARPV Proceedings and Pamphlets 1976
200
21 High Lift Wing for RPV Recovery: Notes, Graphs and Drawings
Jul 1977
22 DAAB07-78-Q-1533 Mini-RPV Automatic Recovery System Contract Proposal and Notes
Dec 30 1977
23 Ryan Flexbee Surveillance Drone System and Photos Undated 24 RPV Industry Pamphlets Undated 25 Propeller Propulsion for RPV’s: Articles and notes 1976 26 Report R-585-1 The Aeroelastic Behavior of Rotary Wings
in Forward Flight Volume II Correlation with a Servo-Flap Rotor System Contract#64-0488f Kaman
Undated
27 The Application of Reliability Concepts to Fatigue Loaded Helicopter Structures
May 3 1962
28 WADC TR 59-714 Study and Development Criteria for High-Speed Power Transmission Shafts
Dec 1960
29 FTD-TT-63-792 Flexible Heavy-Duty Transmissions Undated 30 Rotor Systems and Control Problems in the Helicopter Sep 5 1947 31 Resonant Fatigue Failures Associated with Noise 32 WCT 2366 Phase II Flight Tests of the Seibel YH-24SE
Helicopter, USAF 51-5113 Oct 22 1951
33 TN WCT-52-47 Functional Development Test of the YH24SE Helicopter
Dec 1952
34 AFFTC-TH-59-4 Limited Performance Evaluation of the H-43A Helicopter
Mar 1959
35 AFFTC-TR-60-2 Air Force Flight Evaluation of the YHO2HU Helicopter
Feb 1960
36 Theoretical Investigation of Coaxial Rigidly-Mounted, Two-Bladed Rotors, Final Report Contract# W 33-038 AC-9772 Bendix
Aug 7 1946
37 USAAVLABS TR 70-59 Effect of Rotor Blade Root Cutout on Vertical Drag Contract# DAJ02-70-C-0010
Oct 1970
38 USAAVLABS TR 70-24 An Investigation on the Structural Dynamics of Helicopter Rotors Contract# DAAJ02-67-C-0099
Apr 1970
39 WADC TR 55-437 Part II An Investigation on the Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Contract# AF 33(616)-2780
Mar 1959
40 Natural Antiresonances in Structural Dynamics Sep 24 1971 41 Application of Advanced Composites to Helicopter
Airframe Structures May 1974
42 The Application of Fracture Mechanics to the Design of Damage-Tolerant Components of the UTTAS Helicopter
May 1974
43 The Use of Test Data to Improve Large Scale Dynamic Models of Structures
Nov 8-9, 1973
44 WADD TR 61-177 Structural Safety Under Conditions of Ultimate Load Failure and Fatigue
Oct 1961
201
45 WADC TR59-507 Fatigue of Aircraft Structures Aug 11-13 1959
POWERPLANTS 103 1 An Experimental Investigation of a Low-Speed
Circulation-Controlled Aerofoil by R.J. Kind & D.J. Maull Cambridge University
Jul 1967
2 Tech Proposal No. 927 Model A51605-274 Propeller for Bell Aircraft Model D190-B Aeroproducts
Jul 1959
3 AHS 24th National Forum – No. 213 The Toroidal Rotary Regenerator for Gas-Turbine Engines by Henry J. Selfors Pratt & Whitney
May 8-10 1968
4 AHS 24th National Forum – No. 212 Allison T63 Regenerative Engine Program by Edward J. Privoznik General Motors
May 8-10 1968
5 LTS 101 Turboshaft Engine Avco Lycoming Apr 1974 6 LTS 101 Turboshaft Engine Avco Lycoming Apr 24 1974 7 T5508D Turbine Engine for the Bell Model 214B Avco
Lycoming Undated
8 USAAVLABS TR 66065 An Experimental Investigation of the Effect of Forward and Rearward Motion on the Thrust of a Shrouded Propeller Contract# DA 44-177AMC-892(T)
Sep 1966
9 NASA CR-121095 High-Tip-Speed, Low-Loading Transonic Fan Stage – Part I Aerodynamic and Mechanical Design Contract# NAS 3-13498
Apr 1973
10 Proceedings of the 1980 Conference on Propeller Propulsion
Apr 1980
11 Report DM 62-14 A Comparison of VTOL Propulsion Systems in a Subsonic Mission by W.L. Rodenbaugh General Electric
Jan 18 1962
12 High Bypass Turbofan Engines Avco Lycoming Undated 13 Advanced Lift Cruise Engines and Lift Fan Systems Pratt
& Whitney May 17 1966
14 Report PDS-3384 STF/S-351 Convertible Engine Studies 2500-6000 SHP Pratt & Whitney
Sep 5 1969
15 Report GP 73-127RVP Propulsion Summary Pratt & Whitney
Undated
16 USAAVLABS TR 69-59 Detailed Design of a 2000-SHP Advanced Technology V/STOL Propeller System
Sep 1969
17 IAS Paper No. 59-107 Wind Tunnel Tests of Shrouded Propellers and Their Application by Robert K. Wattson, Jr & Vernon O. Hoehne Univ. of Wichita
Jun 16-19 1959
18 FTD-MT-24-141-70 Gas Turbine Engines for Helicopters (from Russian)
Jun 24 1971
202
19 Report HSER 2417 Static Whirl Test Evaluation of a Full-Scale Variable Camber Propeller Phase I Contract# Now 60-0564-d Hamilton Standard
May 31 1961
20 Experimental Rotating Combustion Engines – A New Shape in Power Curtiss
C.A. 1963
21 SAE 650200 Advanced Propeller Developments for V/STOL Aircraft by George Rosen Hamilton Standard
Apr 12-15 1965
22 SAE 730911 Lycoming LTS 101 – Low Cost Turbine Power in the 600 hp Class by A. Myers & E. Pease Avco Lycoming
Oct 16-18 1973
23 SAE 740165 Lycoming’s LTS 101 Engine Design by J. Moore & E. Pease Avco Lycoming
Feb 25-Mar 1 1974
24 FAA-ADS-59 A Study of Twin-Engine Airplane Propeller Interconnection – Final Report
Jan 1966
25 Report TAR-TR-625 The Aerodynamic Loading on Streamlined Ducted Bodies by Gary R. Hough Contract# Nonr-2859(00) THERM
Dec 1962
26 Propulsion Prospects by R.H. Weir – The Aeronautical Journal of the Royal Aeronautical Society
Nov 1969
27 General Airscrew Applications to VTOL Propulsion THERM
May 16-17 1961
28 Miscellaneous Propeller Papers Various 29 Tandem Air Propellers II by E.F. Lesley Undated 30 NACA TN No. 322 The Effect of the Wings of Single
Engine Airplanes on Propulsive Efficiency as Shown by Full Scale Wind Tunnel Tests
Oct 1929
31 NACA TN No. 333 Test of an Adjustable Pitch Model Propeller at Four Blade Settings
Feb 1930
32 NACA TN No. 562 Experimental Investigation of Aircraft Propellers Exposed to Oblique Air Currents
Apr 1930
33 NACA TN No. 677 Tests of a Contra-Propeller for Aircraft Nov 1938 34 NACA TN No. 689 Tandem Air Propellers Feb 1939 35 NACA ARR No. L4E22 Wind-Tunnel Tests of Dual-
Rotating Propellers with Systematic Differences in Number of Blades, Blade Setting, and Rotational Speed of Front and Rear Propellers
May 1944
36 NACA ARR No. 4H26 An Experimental Investigation of the Thrust and Torque Produced by Propellers Used as Aerodynamic brakes
Aug 1944
37 NACA ARR No. ACR No. L5A11 The Effect of Trailing-Edge Extension Flaps on Propeller Characteristics
Jan 1945
38 NASA TN D-318 A Wind-Tunnel Investigation of Three Propellers Through an Angle-of-Attack Range from 0o to 85o
Apr 1960
203
39 NASA TN D-1774 Aerodynamic Characteristics of a Full-Scale Propeller Tested with Both Rigid and Flapping Blades and with Cyclic Pitch Control
Apr 1963
40 R. & M. No. 1377 Application of Goldstein’s Airscrew Theory to Design by C.N.H. Lock (British Air Ministry)
Nov 1930
41 R. & M. No. 1674 Tables for Use in an Improved Method of Airscrew Strip Theory Calculation by C.N.H. Lock & D. Yeatman (British Air Ministry)
Oct 22 1934
42 Report No. 675 Tests of a Hamilton Standard Four-Way, 21-Inch-Diameter Model Propeller Employing the U.S. Navy Airborne Model Testing Facility Contract# Nonr 1858(14) Princeton Univ.
Apr 1964
43 23LF Small Gas Turbine Propellers with Amendment 1 Hamilton Standard
Undated
44 WADC TR 59-421 Study of Propeller Controls for VTOL Aircraft Applications – Phase I – Determination of Aircraft Configuration and Control Requirements Contract# AF33(616)-6072
Jun 15 1959
45 Doc 81205 Variable Camber Propeller Performance Investigation Boeing Vertol
Feb 4 1966
46 NASA CR 114399 Advanced general Aviation Propeller Study Contract# NAS2-6477
Dec 21 1971
47 AR# 1023 Generalized Propeller Noise Estimating Procedure – Revision D. Hamilton Standard
Jul 12 1971
48 NASA CR 114289 Advanced General Aviation Propeller Study Contract# NAS2-5885 Hamilton Standard
Apr 1971
49 NASA CR xxx Computer Program User’s Manual for Advanced General Aviation Propeller Study Contract# NAS2-6477 Hamilton Standard
Dec 21 1971
PROPELLERS Conference on Propeller Propulsion(COPP), Apr 22-24 1980
104 1 COPP Application of Propeller Technology to General Aviation Aircraft
Nov 1980
2 COPP Review of Propeller Propulsion Progress up to the 1970’s by Charles Scolatti
C.A. 1980
3 COPP Remarks by David J. Goldsmith of Eastern Airlines C.A. 1980 4 COPP Propeller Drive System Considerations,
Requirements, Design Philosophy, Recommended R&D and Quantification of Benefits by Terry A. Lyons
C.A. 1980
5 COPP The Commercial Aircraft Designer’s View of Propeller Propulsion by Richard Foss
C.A. 1980
6 COPP A Military Aircraft Designer’s View of Propeller Propulsion by Richard Scherrer
C.A. 1980
204
7 COPP Advanced Propeller Potential by Bernard Gatzen Hamilton Standard
C.A. 1980
8 COPP Navy User’s View of Propeller Propulsion by Captain W.A. Finn
C.A. 1980
9 COPP The Commercial Aviation User’s View of Propeller Propulsion by David J. Goldsmith
C.A. 1980
10 COPP Engine Considerations by Robert Neitzel & Robert Hirschkron
C.A. 1980
11 COPP Application of Propeller Technology to General Aviation Aircraft by Cornell Slivinsky
C.A. 1980
12 COPP General Outline and Host Comments by Donald L. Nored NASA-Lewis Research Center
Apr 22-Apr24 1980
13 COPP related Clippings and Articles Various 14 COPP – Photos and Vugraphs C.A. 1980 15 COPP – Congressional Subcommittee Testimony C.A. 1980 16 The World is Round and So Are Propellers Jan 27 1981 17 NASA’s Propfan Progran – The case for Acceleration Undated 18 Propfan C-141 In-Service Demonstration Jan 15 1981 19 Turboprop Study Jan – Jun 1981 20 Lusczak ASD Activities Undated 21 Other Propeller Presentations Various 22 COPP – Miscellaneous C.A. 1980 23 Recommended Plan to Achieve Timely Technology
Readiness of Prop-Fan Propulsion & Airplane Systems Jan 23 1981
24 Report NAPTC-AED-1862 Advancement in Technology for Propellers: State of the Air
Nov 15 1967
25 SP 05A80 Advanced Turboprop Propulsion Technology Oct 1980 26 Quiet 24PF Fiberglass Covered Propeller Blade Hamilton
Standard Nov 17 1975
27 Possibilities for Progress in Gear Technology Mar 28 1968 28 SP 07A77 Prop-Fan Technology Status Report Undated 29 Hamilton Standard – Advanced Propeller Concepts C.A. 1963 30 Hamilton-Standard – Propellers for Advanced V/STOL
and STOL Aircraft C.A. 1968
31 AIAA 79-0610 Aeroacoustic Design of the Propeller by F.B. Metzger & C. Rohrbach Hamilton Standard
Mar 12-14 1979
32 SAE 780995 Prop-Fan Propulsion – Its Status and Potential
Nov 27-30 1978
33 NASA CR 159355 Turboprop Cargo Aircraft Systems Study Phase I Contract# NAS1-15708
Nov 1980
34 PDB 6101 Generalized Method of Propeller Performance Estimation Hamilton Standard
Jun 1963
35 Experimental Verification of Hamilton-Standard Method of Calculating Performance of Propellers in a Shroud
Mar 24 1961
36 Miscellaneous Design Information (Propellers) Undated 37 Propeller Performance Bibliography Jun 21 1973
205
38 Prop Fan Articles C.A. 1972
SMALL TACTICAL AERIAL MOBILITY PLATFORM (STAMP) & Lindenbaum Presentation of 1981
105 1 VTOL Overview Through 1980 C.A. 1981 2 V/STOL Concepts and Developed Aircraft – A Historical
Review by Bernard Lindenbaum - Documents Contract# N00019-78-C-0552
Mar 1981
3 V/STOL Concepts and Developed Aircraft – A Historical Review by Bernard Lindenbaum - Notes Contract# N00019-78-C-0552
Mar 1981
4 Report No. NWC TP 5853 The Alperin Jet-Diffuser Ejector (AJDE) – Development, Testing, and Performance Verification Report Contract# N00123-74-C-0243
Feb 1976
5 Jet Diffuser Ejectors – Miscellaneous Papers C.A. 1973 6 WASP II Program – STAMP – Williams Research Corp. Sep 24 1980 7 Preliminary Systems Design Engineering for a Small
Tactical Aerial Reconnaissance System – Visual (STARSV) USAAMRDL
Jun 15 1974
8 TN 4008-5 Revision 1 STAMP Operational Concepts, Mission Characteristics and Design Guidance by James G. Martz, III Naval Weapons Center
Apr 1973
9 TN 4008-6 STAMP Technical Survey, Key Parameters and Technical Concepts of Promise by Bradley D. Kowalsky & Scott W. Pitcher Naval Weapons Center
Apr 1972
10 STAMP Documents and Papers C.A. 1974 11 Report No. 1751 Feasibility Study of Small-Rocket Lift
device Contract# DA 44-177-TC-595 Aerojet-General Corp.
Feb 1960
12 Special Report No. 1820 Stability and Control Study of a Small Rocket Lift Device by P.A. Sollow Aerojet
Jul 1 1960
13 Proposal No. R-2622A The Revision and Expansion of the ASD/XR Drone/RPV Mission Analysis Study Univ. of Dayton
Apr 15 1977
14 Proposal No. R-3035 Review of V/STOL Concepts and Developed Aircraft Univ. of Dayton
Feb 23 1978
15 Report No. TR-737 Jet Lift Concepts to Improve Individual Soldier Mobility by A.H. Bohr Thiokol
Jun 3 1959
16 Report No. TR 3355-1 Rocket Jump Belt – A Proposed Experimental Program by A.H. Bohr Thiokol
Aug 1 1960
17 Document No. 74-210824 Test Report – Small Tactical Aerial Platform (STAMP) – Demonstrator Vehicle Static Tests and Tethered Flight Tests Garrett
Mar 19 1974
206
18 Document No. 74-210825 TR –Feasibility Study for Small Tactical Aerial Platform (STAMP) NWC Contract# N00123-73-C-1073 Garrett
Mar 27 1974
19 Proposal for the Development of a Lift-Fan-Stabilized STAMP Vehicle Hydra-Electric Co.
Oct 15 1973
20 Report No. 159-X-36 Preliminary Design Study of STAMP Configurations NASC Contract# N00019-73-C0519 Piasecki.
Nov 30 1973
SERIES XI: Microfilm, 1950
Box File Description Date
Records of the Prewitt Aircraft Company, Clifton Heights, PA
106 1 History of the Helicopter, Volumes 1, 2, 4, 11, 12, 13, 16 (A to C), 16 (D to Z)
Mar 10, 1950
2 Rotary Wing Aircraft Handbooks and History, Volume 1, Roll 2 History of the Helicopter from its Beginning to the year 1900
Mar 9, 1950
3 Rotary Wing Aircraft Patent Abridgement, Volume 15, 18002 to 2,491,260
Feb 1, 1950
4 Rotary Wing Aircraft History, Volumes 3, 5, 6, 7, 8, 9, 10, 14, 16, 17, 18
Apr 27, 1950
5 Rotary Wing Aircraft History, Volume 3 Apr 26, 1950 6 Rotary Wing Aircraft History, Volume 3 to Volume 18 Apr 26, 1950
SERIES XII: Film, 1938-1977
Box File Description Date
107 1 L-123 – “Spinning and Tumbling Tests of a 1/18-Scale Model of the Ryan X-13 Airplane” and “Drop Tests of a 1/18-Scale Model of the Ryan X-13 Airplane,” (NACA), 35 minutes, Silent/Black & White
Apr. 1956
2 Down-Wash Tests, Eglin AFB, FL, CH-3, HH-53, C-142A Undated 3 W/O 8875, “VJ-101 Briefing Film”, AF Flight Test Center,
Edwards AFB, CA, Color, Silent Undated
4 “CL-757 V/STOL Flying Simulator,” Lockheed, Color/Sound, 9 minutes
Apr. 23, 1965
5 “ESCAPAC,” Douglas Aircraft Comp., 10 minutes, Color/Sound
Undated
6 YAV-8B, Color, 4.5 minutes Undated
207
7 W/O 8875, “VJ-101C (X-2) Telescope Runs,” Tests: Optimization of Auto-Stabilization System in pitch, roll, and yaw,” AF Flight Test Center, Edwards AFB, CA, Color
May, Aug. 1966
8 Prod. 1563, “Scale Model Tests (Langley),” Bell Aircraft Corp.
Oct 10, 1958
9 First Flight, RSAF System 37 Feb. 8, 1967 10 W/O 8219, “STOL Demonstrations DHC-5,” Color Undated 11 JO# 785, “P-1127 (VTOL),” US Naval Missile Center,
Point Mugu, CA, Color, Silent, 35mm Jun. 15, 1967
12 W/O 8875, “DO-31 Briefing Film,” Color c.a.1966 13 “XC-4B Hummingbird II, Quarterly Progress Report No.
9, Oct. 1-Dec 31, 1968,” Lockheed-Georgia, 10 minutes Dec. 1968
14 “XC-4B Hummingbird II Quarterly Progress Report No. 3, 1 Apr. 1967-30 Jun. 1967,” Lockheed-Georgia, 8 minutes
Jun. 1967
15 “XC-4B Hummingbird II Quarterly Progress Report No. 3, 1 Apr. 1968-30 Jun. 1968,” Lockheed-Georgia,
Jun. 1968
16 “XC-4B Hummingbird II Quarterly Progress Report No. 6, 1 Jan. 1968-31 Mar. 1968,” Lockheed-Georgia, 9 minutes, 15 seconds
Mar. 1968
17 “XC-4B Hummingbird II Quarterly Progress Report No. 1, 21 Sept. 1966-21 Dec. 1966,” Lockheed-Georgia, 9 minutes
Dec. 1966
18 “XC-4B Hummingbird II Quarterly Progress Report No. 4, 1 Jul. 1967-30 Sept. 1967,” Lockheed-Georgia, 10 minutes
Sep. 1967
19 “XC-4B Hummingbird II Quarterly Progress Report No. 5, 1 Oct. 1967-31 Dec. 1967,” Lockheed-Georgia, 10 minutes
Dec. 1967
20 “XC-4B Hummingbird II Quarterly Progress Report No. 2, 22 Dec. 1966-31 Mar. 1967,” Lockheed-Georgia,
Mar. 1967
21 “XC-4B Hummingbird II Quarterly Progress Report No. 8, 1 Jul. 1968-30 Sept. 1968,” Lockheed-Georgia, 7 minutes
Sep. 1968
22 XC-4B Hummingbird II Quarterly Progress Report, Lockheed-Georgia, Undated
Undated
23 MS-401-252, “XV-4B Seat Ejection Report, Lockheed c.a.1968 24 XV-4B Ejection Seat Undated
108 1 H-43 Icing Test Shots, 10 troops in Hoist operation, Autorotation landing, Firefight demonstration
1959?
2 Bell Helicopter Company, “Master” 1965 3 “Downwash Survey Test, “ Eglin AFB, FL, Aug 21-Aug
25, 1967, Edited Version, 17 minutes, Color/Silent Aug. 1967
4 Early Attempts and Some Helicopters to mid-1950s, Historical Film Series, Shell Film
Undated
5 AVROCAR (V/STOL Aircraft) (VHS Tape Copy with 16 mm Film)
Undated
208
109 1 UH-1 Annual Report Undated 2 “H43B Huskie Progress Report,” Kaman Aircraft Corp. Undated 3 HU-1D First Flight c.a.1962 4 X-18 Wing Tilt Operation – Progress 1958 5 Sikorsky “Flying Crane Movie,” 20 min. Jul. 1959 6 “Know Your Iroquois,” Bell Helicopter Comp., 32 min.
Color/Sound Undated
7 W.O. 8232, “Avro Car Model,” Color, Approx. 20 min Mar. 1959 8 Unidentified Boeing Vertol film Dec. 1963 9 “How the XV-4A Augmented Throst System Works” Undated
110 1 “Vision Achieved,” Boeing Vertol Division, Color/Sound, 15 min.
Nov. 1966
2 Springboard for Science? Undated 3 Air Slew Missile Tests in PWT Undated 4 W.O. 698 D.C. Reel 5, Silent Color Print N.C. Undated 5 Joint Flight Test Group, AF Flight Test Center, Edwards
AFB, CA, Color 2 Oct. 1967
6 “Final Flight Test Report X-13 Jan. 1957-Jul. 1957,” Ryan Aeronautical Comp., Color/Sound, 12 min.
Jul. 1957
7 D.O. 31, V/STOL, Color Undated 8 Unidentified Undated 9 Sikorsky CH-54A, Vietnam c.a.1967 10 Unidentified 1968 11 S-64 Ship Trainer Demo, Color, 10 min. Undated 12 “Two Decades of V/STOL,” Ryan Aircraft Comp., Color,
Sound, 14 min. (Out take?) Undated
13 Unidentified Undated 14 Aerodyne in der Flugerprobung, 9 min. 35 sec. 1972 15 MP-223, “XV-4A Hummingbird,” Lockheed-Georgia
Company, Color/Sound, 12 min. Undated
16 “Rigid Rotor Concept,” Lockheed Company, Color/Sound, 7 min.
Aug. 1965
17 T58 Engine Manufacturing, General Electric Undated 18 “VERTOL V-76 Progress Report Undated 19 XV-4A Hummingbird, Camera Position Master Undated 20 X-19 Flight, Aerial Camera, Curtiss-Wright VTOL
Systems Division, Color Aug. 1965
21 “Last Half of Flight Phase Test, Test #3 & #4”, Ryan Aeronautical Company. Color, Silent,
c.a.1966
22 Unidentified Undated 23 WCBS Radio Help-ocopters, Color Apr. 1967 24 “Hueycobra,” Bell Helicopter Comp, Color/Sound, 8 min. Undated 25 “Vertical Take Off and Landing Flight 54 & 55,” Ryan
Aeronautical Comp., B/W, Silent Apr. 1957
209
26 “X-13 First Hovering Flight,” Ryan Aeronautical Comp., Color/Silent
May 1956
27 “X-13 Hook on to Cable,” Ryan Aeronautical Comp., Color/Silent
Jul. 1956
28 “Waffen system KAD Korps Aufklarungs Drohne,” Dornier PR, 10 min. 20 sec.
c.a.1973
29 Unidentified (no case) Undated
111 1 74/W-12 97010, Aerospace General Helo, Color c.a.1974 2 Unidentified Undated 3 XV5A, XC142 Undated 4 Summary of Ground and Air Tow, Sikorsky Aircraft, Air
Material Command, B&W, Silent, 18 min. Undated
5 Unidentified Undated 6 Unidentified Undated 7 Radio 88 Undated 8 HU-1A Annual Progress Report, Bell Helicopter Corp.,
Color/Sound Undated
9 Rigid Rotor Developments, Lockheed California, Color/Sound, 4 min.
Undated
10 Unidentified Undated 11 V/STOL Aircraft Developments, Air Material Command,
B&W, 27 min. Undated
112 1 W.O. 72-800, C-135 Laser Taff Test #2 Nov. 1972 2 X-142 Hover Over Patrol Box & STOL Landing (Edwards
AFB?), Color/Silent c.a.1966
3 5” Folding Prop Rotor Model Wind tunnel Test, Bell Helicopter Comp., Color/Silent, 5 min
Feb. 1970
4 XC-142A Flight #29, #2 Airplane, Color/Silent c.a.1965 5 XC-142 #929 Test, Desert Landing Attempt, AF Flight
Test Center, Color, Mar. 1966
6 SAAB Undated 7 Joint Flight Test Group, AF Flight Test Center, Color Oct. 1967 8 Distortion Patterns c.a.1968 9 Unidentified Undated 10 P41C-COA, TC-427 Undated 11 Data on Investigation of the Effects of Airframe Design on
Inlet Flow Fields by Constant Prokop, Fairchild Republic Division
Undated
12 P41C-COA, TC-427 Undated 13 Hoverbuggy, North American Aviation, Color/Silent, 1
min c.a.1964
14 Slides for Japan DEA Briefing Jul. 1966
113 1 SPR 36-70, Human Engineering Long Line Loiter, Color Undated
210
2 Drops to Small Sites Undated 3 Nichols Design Session, 8mm film Undated 4 SFR – Mother/Daughter, Color Apr. 1968 5 C-130 and L-286 Mother & Daughter Program, Lockheed
Company, 16 min. Undated
6 L-286/130 Proximity Flying, Lockheed Company, 12 min. Undated 7 Helicopter Tow Range Extension Undated 8 Aerocrane Test, Armed Forces Day Apr. 1977 9 AHS X-22A Undated 10 Kellett YO-60 & YG-1B Jump Take Off, Color Undated 11 C-3 Spot Landings, Jump Take Off Undated 12 Progress In VTOL, Report #2, Boeing VERTOL Division,
B&W, Sound, 5 min. Undated
13 The U.S. Army VZ-2 Tilt-Wing Research Aircraft, Boeing VERTOL Division, Color/Silent, 10 min.
Undated
14 XC-142, XV-5, X-19 Undated 15 Tri-Service Accidents Undated 16 Unidentified (not on reel) Undated 17 Go Patrol Excerpts Undated 18 Early GIROs Undated 19 Progress in VTOL, #3, Boeing VERTOL Division,
B&W/Sound, 8 min. Undated
20 German (Focke) Rotary Wing Kite Undated 21 Autogiro (Not on Reel) Undated 22 XR-3 (?) Undated 23 Kellett Undated 24 US AAC Autogiro Unite Graduation Exercises at Patterson
Field, Fairfield, OH plus Series of Scenes of five Kellett YG-1B Autogiros taxiing on ramp and take-off
c.a.1938
25 Unidentified Undated
114 1 XC-142 T.O. & Landing, 20 Palms, Color Mar. 1966 2 XC-142 Downwash Tests at Eglin AFB Undated 3 XC-142 #924 Multi Air Drops Oct. 1966 4 Dummy Rescue Pick-Up, XC-142A, Color/Sound, 5 min. Undated 5 XC-142A Undated 6 Stencil Kit NATC Test Undated 7 XV-4B Escape May 1968 8 Gelac (XV4B Hummingbird) Status Report XV-4B,
Lockheed –Georgia Company, Color/Sound, 4 min. Oct. 1968
9 Gelac (XV4B Hummingbird) Status Report XV-4B, Lockheed –Georgia Company, Color/Sound, 4 min.
Oct. 1968
10 XV4B Tzxi & 1st Flight, T/O & Landing, 4 min. Undated 11 Gelac (XV4B Hummingbird) Status Report XV-4B,
Lockheed –Georgia Company, Color/Sound, 4 min. Oct 1968
211
12 XC-142 Documentary, Paris Air Show, Color/Silent, 17 min.
Undated
13 XC-142A TAC Demo at Eglin Air Force Base, Color/Silent, 12 min.
Oct. 1966
14 XC-142 Category II Operational Suitability Tests, Color/Sound, 19.5 min.
Undated
15 Comparative Downwash and Simulated Forest Rescue, Color
Undated
16 Ground Damage Film, Color/Sound, 19 min. Undated 17 AVROCAR Progress Report #2, Color/Silent Undated 18 XC-142A Sand Operations at Edwards AFB, Silent Undated 19 V41A-77A Test Dec. 1974 20 Bell XF109 Mock Up & Free Flight Test in Wind Tunnel Undated
115 1 Focke-Achgelis, Large Twin Rotor, Focke-Achgelis Kite, R-6, F-5
Undated
2 Mother/Daughter, C-130 and Lockheed 286 (Unedited airto-air)
Mar. 1968
3 AFSS Tactical Usage Undated 4 Flying Lifeboat (Coast Guard) Undated 5 Film Clips (Historical), VS-300 through CH-53 (Jolly
Green) Undated
6 “Three if by Air,” 33.55 min. Undated 7 Battlefield Pegasus, Boeing Vertol Division, Color/Sound,
12 min. Mar. 1967
8 Lockheed Topped Rotor, Retractable Rotor Undated 9 XFY-1, Convair newsreel release film Jan. 1957 10 XFY-1 “POGO” Hover Test, Convair, San Diego, Color 1954 11 Kellett YO60 and YG1B Gregory Jump-Off, Color Undated 12 Rigid Roto Acrobatics, Lockheed California, Color/Sound,
9 min. Undated
13 Bell Aero D-188, Preliminary Progress Review, Bell Aircraft Corp.
Undated
14 Staff Film Report Submission, 14-41-67, Color Mar. 1967 15 X-13, Portion removed from history film and replaced with
more complete hook on sequence Undated
16 No Man Expendable, Sikorsky Aircraft, Color, 12 min. Undated 17 W-14-CL, Color/Silent Undated 18 Model 48 Undated 19 U of Maryland, XV-48 Wind tunnel Tests, Tufts & Water Undated 20 Stowed Rotor ½ Span Model, Princeton Test, Boeing
Helicopters, Color/Silent Undated
21 1966 AFA Briefing, Stabilized vs Unstablilized Tests, Douglas Aircraft, Color/Silent
1966
22 AFFDL Air Slew Missile, Hughes Model Undated 23 Aftermath of Harrier Crash Undated
212
24 Bell XV-15, Clip removed from Bell film Undated
116 1 Flight Tests of 1/5 Scale Model of the Ryan X-13 Airplane, Color/Silent, 15 min.
c.a.1961
2 “GADS” Graphic Airfield Damage Simulation), McDonnell Douglas, Color, 12 min.
1980
3 X-14 Documentary, Bell Aircraft Corp. Undated 4 Wings for the Ground Commander, Boeing VERTOL
Division, Color/Sound, 16 min. Mar. 1967
5 Rigid Rotor Revolution, Lockheed California, Color/Sound, 16 min.
Mar. 1966
6 Pan Am Bldg Roof? Undated 7 Construction by ‘Copter,’ Sikorsky Aircraft, Color/Sound,
19 min. 18 sec. Undated
8 Vought-Flying Pancake, V-173 STOL, 1942 (Navy), Prototype (XFSU-1), Flew 130 hours of testing
Undated
9 Composite XV-4B Undated 10 “Vertability,” Intro to American Helicopter Society’s first
film for industry, premiered at 23rd Annual National Forum 1967
11 Balzac Flight Test, Boeing Aircraft, Color/Silent Oct. 1965 12 Navy Accident Undated
117 1 Ryan XV-5A Progress Report Jul. 1964 2 Qualitative Assessment, 17 min. Undated 3 X-13 Used in Combat (Korea?), Also, Bell 42 Undated 4 XH-17? Undated 5 YH-40 Annual Report, Color/Sound Undated 6 Demonstration of Kellett YO-60 Autogiro, Silent Undated 7 V/STOL History Film, Non-Helicopter VTOL Aircraft Undated 8 Sikorsky S60 Sky Crane? Undated 9 X-13 Film 1955 10 XV-15 Flight Update, Bell Helicopter, 11 ½ min. Undated 11 XV-3 Summary Report, Color/Sound Undated 12 XR-3 c.a.1975
118 1 X-19, X-22, XC-142 (May be mold damaged) Undated 2 Bendix – 1 place and 5 place; XHRP-1 and Franks original
PV-1 (May be mold damaged) Undated
119 1 XH-17 Upside down, PV-3 Color; Other Miscellaneous Clips
Undated
2 The Evolution of Airlift, Color, 21 min. 40 sec. Undated 3 Propulsion for Vertical Flight, Vertical Flight Foundation
film, Color/Sound, 13 ½ min. Undated
4 H$3B Huskie Progress Report II, Kaman Aircraft Corp., Color/Sound, 20 min.
Undated
213
5 Charlies Choppers SDQP Undated 6 The Bell Helicopter (Bell Early Helicopters) Undated 7 XV-4B Hummingbird II Final, Report, Lockheed-Georgia,
Color/Sound, 19:05 min. Jun. 1969
8 Joint Flight Test Group, Color Oct. 1967 9 Pitcairn Autogiro Development Dec. 1973 10 SAAF: Viggen – fpl37 (English version of Swedish film),
17 min 1970
11 Unidentified Undated 12 Unidentified Undated
VHS Tapes 120 1 LTA 20-1 Development Summary, Program #3, 7 min.;
Walter Cronkite’s Universe “Airship Feature Interview,” 12 min.
Dec. 1981; Jun. 1982
2 Clyclo Crane, Tillanook, OR and Powered Balloon, Astoria, OR
Undated
3 Geared Flap Model Flight Films Undated 4 French – Alar Volant Choppers Undated 5 Projecting Power from the Sea, a presentation of the Navy
League of the United States in Association with Hughes Aircraft Company
Undated
6 O-Wing VTOL Undated 7 Air Force TOWS (“Hat”), Washington, D.C. (Video
Original Copy of Lindenbaum) 12 min. May 1998
8 Logging with Helicopters (From Brinkley U.S. Forest Service)
1986
9 Cessna’s Helicopter Adventure, 1 hr. 49 min Undated 10 Excerpts of V/STOL History Undated
214