SAE 2015 International Conference on Icing of Aircraft ... · the challenges involved in compliance...

Monday, June 22

Opening Plenary SessionSession Code: ICE100

Room Congress Hall

Robert J. FlemmingOrganizers -

Robert J. Flemming; Richard Lewis, AirbusModerators -

1:00 p.m.

1:20 p.m.

1:30 p.m.

1:45 p.m.

2:30 p.m.

3:00 p.m.

3:25 p.m.

3:50 p.m.

4:00 p.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

Chairmen's Welcome, Safety Tips and Conference Instructions

Welcome to the City of Prague

Welcome from Czech Aircraft Industry

Keynote Address - A/C Flight in Icing Conditions: An OverallPerspective

NASA Address

EASA Regulatory Address - Aircraft

EASA Regulatory Address - Engines

EASA Regulatory Question & Answer

BREAK - Refreshments Served on Mezzanine Level

Robert J. Flemming; Richard Lewis, Airbus

Eric Duvivier, European Aviation Safety Agency

James M. Free, National Aeronautics and SpaceAdministration

Laurent Fleury, European Aviation Safety Agency

Angus Abrams, European Aviation Safety Agency

Time Paper No. Title

SAE 2015 International Conference onIcing of Aircraft, Engines, and Structures

Technical Session Schedule

As of 06/28/2015 07:41 pm

13:00Session Time:

This presentation will look at A/C flight in Icing conditions in theoverall context of aviation safety. It will address new challengesassociated to air transport operation and regulation evolutions.Research priorities will be proposed.

This presentation will provide an overview of the changesintroduced in the new CS-E Icing regulations, and summarise theremaining key differences with the FAA regulations. Focussing onthe challenges involved in compliance with ice crystal aspects, thepresentation will address the interim EASA approach tocompliance pending the development of improved ice crystal testand analysis capabilities.

Richard Lewis, AirbusModerators -

Tuesday, June 23

Aircraft Inflight Icing - Icing Physics & Low-Order ModelSession Code: ICE107

Room Bruncvik/Premysl

This session includes a low-order model of air-driven water film over surface ice roughness, a study of ice roughened wall effect on glaze-iceprediction, and an experimental study of a supercooled drop imapct dynamics and freezing

Gene Addy, NASA John Glenn Research Center; Philip J. Alldridge, SikorskyAircraft Corp.; Ben C. Bernstein, Leading Edge Atmospherics; Gerard Duprat,Airbus; Robert J. Flemming; Richard Lewis, Airbus; Michael James Oliver; Jen-Ching Tsao, Ohio Aerospace Institute

Organizers -

Tom Currie, National Research Council Canada; William B. Wright, VantagePartners Limited

Chairpersons -

4:20 p.m.

4:45 p.m.

5:10 p.m.

5:45 p.m.

6:15 p.m.

8:30 a.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

2015-01-2078

FAA Regulatory Address - FAA 14 CFR Part 25 Rulemaking for Flightin Icing

FAA Regulatory Address - FAA 14 CFR Part 33 Rulemaking forTurbine Engine Icing

FAA Regulatory Question & Answer

Industry Perspective - Aircraft - Part 23 & 25

Industry Perspective - Engines

A Low-Order Model of the Interaction between Air-Driven WaterFilms and Sub-Grid Surface Roughness

Robert K. Hettman, Federal Aviation Administration

John Fisher, Federal Aviation Administration

Richard Lewis, Airbus; Jim R. Hoppins, Textron Aviation

Geoffrey B. Jones, Rolls Royce

Alric Rothmayer, Hui Hu, Iowa State Univ.


08:30Session Time:

On November 4, 2014, the Federal Aviation Administrationpublished a final rule to expand the environmental icing conditionsused for certification of new airplanes and engines that have beenmost affected by flight in icing. The expanded icing environmentincludes freezing drizzle and freezing rain, commonly referred toas supercooled large drops, or SLD; as well as glaciated andmixed phase icing conditions commonly referred to as ice crystals.This presentation provides an overview of the rulemaking package,the new and revised airworthiness standards, and the associatedguidance materials that may be used to show compliance.

The Federal Aviation Administration published a final rule toexpand the environmental icing conditions used for certification ofnew turbine engines for flight in icing. The expanded icingenvironment includes supercooled large drops, or SLD; as well asglaciated and mixed phase icing conditions commonly referred toas ice crystals. This presentation provides an overview of theengine icing rulemaking package, the new and revisedairworthiness standards, and the associated guidance materialsthat may be used to show compliance.

Robert J. Flemming; Richard Lewis, AirbusModerators -

Tuesday, June 23

Tuesday, June 23

Aircraft Inflight Icing - Iced Aerodynamics CFD

Aircraft Inflight Icing - NASA ARMD Icing Research Overview

Session Code:

Session Code:

ICE109

ICE105



This session includes a quasi-3D numerical evalution of icing effect on high lift configurations and a Lattice-Boltzmann analysis of 3D ice shapes ona NACA23012 airfoil.

This session presents an overview of NASA Aeronautics Research Mission Directorate (ARMD) current icing research from the AtmosphericEnvironment Safety Technology (AEST) project, and from Airframe, Engine and Rotorcraft Icing sub-projects.



Organizers -

Organizers -

Tom Currie, National Research Council Canada; William B. Wright, VantagePartners Limited

Richard Moser, Aerotex UK; Philippe Villedieu, ONERA

Chairpersons -

Chairpersons -

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

ORAL ONLY

ORAL ONLY

2015-01-2083

2015-01-2084

Ice-Roughened Walls and their Impact on Glaze-Ice Prediction

Spreading and Freezing of a Droplet Impacting Onto an InclinedCooled Surface

Parametric Evaluation of Icing Effects by a Quasi-3D Methodology forHigh-Lift Configurations

Lattice-Boltzmann Analysis of Three-Dimensional Ice Shapes on aNACA 23012 Airfoil

Planned by Aircraft and Engine Conference Planning Committee / EMB Air and Space Group


David Hanson, Michael P. Kinzel, Robert Kunz, Jose Palacios,The Pennsylvania State University

Markus Schremb, Ilia Roisman, Suad Jakirlic, CameronTropea, Technical University of Darmstadt

Daniel Silva, Thais Bortholin, J Allan Lyrio, Luis Santos,Embraer SA

Benedikt König, Ehab Fares, Exa GmbH; Andy P. Broeren,NASA John H. Glenn Research Center

Time

Time

Paper No.

Paper No.

Title

Title

10:30

13:30

Session Time:

Session Time:

Tuesday, June 23

Tuesday, June 23

Aircraft Inflight Icing - Ice Roughness Characterization & Effects

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - New Part 23 andEngine Icing Regulations

Session Code:

Session Code:

ICE106

ICE401


This session includes a study of App. C ice roughness characterization using laser scanning, two studies of detailed local flow characteristics on aNACA0012 airfoil and a flat plate with realistic ice roughness fields under different icing conditions, and a numerical modeling of local air flow overrealistic ice roughness fields from laser scanning.


Organizers -

Richard Moser, Aerotex UK; Philippe Villedieu, ONERAChairpersons -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

2015-01-2098

2015-01-2096

2015-01-2097

ORAL ONLY

NASA Aviation Safety Program¿s Atmospheric Environment SafetyTechnologies (AEST) Project¿s Contribution to Icing Research

An Overview of Airframe Icing Research at NASA

Recent Progress at NASA in Engine Icing Research

A Reevaluation of Appendix C Ice Roughness Using Laser Scanning

Boundary Layer and Heat Transfer Characterization on a Flat Platewith Realistic Ice Roughness

Convection from a Simulated NACA 0012 Airfoil with Realistic IceAccretion Roughness Variations

Computational Modeling of Flow Over Ice Shape Roughness

The papers in this session are available in SAE Technical Paper Collection, COLL-TP-00518, and alsoindividually. To purchase visit collections.sae.org



Renato Colantonio, Mary Wadel, National Aero & SpaceAdministration

Mark G. Potapczuk, NASA John Glenn Research Center

Joseph P. Veres, NASA John Glenn Research Center

Stephen T. McClain, Baylor University; Mario Vargas, RichardE. Kreeger, NASA Glenn Research Center; Jenching Tsao,Ohio Aerospace Institute

Philippe Reulet, Bertrand Aupoix, David Donjat, FrancisMicheli, ONERA

Timothy A. Shannon, Stephen T. McClain, Baylor University

Mark Potapczuk, NASA John Glenn Research Center;Jenching Tsao, Ohio Aerospace Institute


15:30Session Time:

Tuesday, June 23

Environmental Icing Meteorology and Instruments - HAIC/HIWC Overview andCharacterization (Part 1 of 2)Session Code: ICE305

Room Congress Hall

Room Congress Hall

This session includes presentations on regulatory activity for certification and for military qualification for flight in icing conditions, especially thoseassociated with ice crystal icing and supercooled large drops.

This session will provide an overview and initial findings from the High Altitude Ice Crystal (HAIC) and High Ice Water Content (HIWC) programs.

Gene Addy, NASA John Glenn Research Center; Ben C. Bernstein, Leading EdgeAtmospherics; Robert Busto, Federal Aviation Administration; Robert J. Flemming;David Johns, Transport Canada; Richard Lewis, Airbus; Jeanne G. Mason,Boeing Commercial Airplanes; Jen-Ching Tsao, Ohio Aerospace Institute

Gene Addy, NASA John Glenn Research Center; Ben C. Bernstein, Leading EdgeAtmospherics; Robert J. Flemming; Christine LeBot, Meteo-France; RichardLewis, Airbus; Vince LoPresto, United Technologies Aerospace; Jeanne G.Mason, Boeing Commercial Airplanes; Jen-Ching Tsao, Ohio Aerospace Institute

Organizers -

Organizers -

Vince LoPresto, United Technologies Aerospace; Robert W. Ray, Ray Engineering

Matthew Grzych, Boeing; Richard Lewis, Airbus

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

2015-01-2075

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

FAA Certification Standards for Part 23 Aircraft

Development of ASTM Standard for Certification of Part 23 IceProtection Systems ¿ Industry View

Response to FAA and EASA Plenary Presentation for Small Part 23Aircraft

FAA Icing Certification Standards for Fixed Wing Unmanned AircraftSystems

HAIC/HIWC International Field Campaign Overview & PreliminaryOutcomes


Paul Pellicano, Federal Aviation Administration

Dennis Regnier, CAV Aerospace Inc.

Jim R. Hoppins, Textron Aviation

Douglas Bryant, Federal Aviation Administration

Alice Grandin, Airbus; Thomas Ratvasky, NASA John GlennResearch Center; Alfons Schwarzenboeck, CNRS LaMP; J.Walter Strapp, Met Analytics; Fabien Dezitter, Airbus;Dominique Duchanoy, Jean-Francois Bourdinot, CNRS Safire;Julien Delanoe, CNRS Latmos; Rodney Potts, Alain Protat,BoM; Lyle Lilie, Science Engineering Associates Inc.; AlexeiKorolev, Environment Canada; Sandra Turner,ATMOSPHERE, Systèmes & Services

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

08:30

10:30

Session Time:

Session Time:

Tuesday, June 23

Environmental Icing Meteorology and Instruments - HAIC/HIWC Overview andCharacterization (Part 2 of 2)Session Code: ICE305

Room Congress Hall

This session provides an overview and initial findings from the HAIC/HIWC programs.


Organizers -

Alfons Schwarzenboeck, CNRS; J. Walter Strapp, Met Analytics Inc.Chairpersons -

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

ORAL ONLY

2015-01-2087

ORAL ONLY

2015-01-2086

Preliminary Assessment of Appendix D/P Total Water Content fromIn-Situ Measurements of Deep Convective Clouds in the HAIC-HIWCDarwin-2014 Flight Campaign

HAIC/HIWC Field Campaign - Specific Findings on PSD Microphysicsin High IWC Regions from In Situ Measurements: Median MassDiameters, Particle Size Distribution Characteristics and Ice CrystalShapes

Flight Deck Observations During Flight in High Ice Water ContentConditions

Studies of Cloud Characteristics Related to Jet Engine Ice CrystalIcing Utilizing Infrared Satellite Imagery



J. Walter Strapp, Met Analytics Inc.; Alfons Schwarzenboeck,CNRS; Julien Delanoe, LATMOS-UVSQ-CNRS; FabienDezitter, Airbus; Christopher Dumont, Federal AviationAdministration; Alice Grandin, Airbus; Alexei Korolev,Environnement Canada; Lyle Lilie, Science EngineeringAssociates Inc.; Rodney Potts, Bureau of Meteorology; AlainProtat, Australian Bureau of Meteorology; Thomas Ratvasky,NASA John Glenn Research Center; James Riley, FederalAviation Administration

Delphine Leroy, Emmanuel Fontaine, Alfons Schwarzenboeck,LaMP-CNRS/UBP; J. Walter Strapp, Met Analytics Inc.; LyleLilie, Science Engineering Associates Inc.; Julien Delanoe,LATMOS-CNRS/UVSQ; Alain Protat, Centre for AustralianWeather & Climate; Fabien Dezitter, Airbus Operation SAS;Alice Grandin, Airbus

Thomas Ratvasky, NASA John Glenn Research Center;Dominique Duchanoy, Jean-Francois Bourdinot, CNRS;Steven Harrah, NASA Langley Research Center; J. WalterStrapp, Met Analytics, Inc.; Alfons Schwarzenboeck, CNRS-LaMP; Fabien Dezitter, Alice Grandin, Airbus UK

Matthew Grzych, Boeing; Terrance Tritz, Jeanne Mason,Melissa Bravin, Anna Sharpsten, Boeing CommercialAirplanes


13:30Session Time:

Tuesday, June 23

Tuesday, June 23

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Supercooled LargeDrop Icing Tests

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Ice Crystal ParticleImpact in Turbine Engines

Session Code:

Session Code:

ICE410

ICE405

Room Congress Hall

Room Gallery

This session includes presentations on recent supercooled large drop (SLD) test programs.

This session includes presentations on recent developments in the prediction of the effects of ice crystal impacts on turbine.



Organizers -

Organizers -

Walter Affonso, Embraer-Empresa Brasileira Aero SA; James McNamara, NavmarApplied Science Corp.

Thomas E. Dwier, Textron Aviation; Jeanne G. Mason, Boeing CommercialAirplanes

Chairpersons -

Chairpersons -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

3:30 p.m.

2015-01-2092

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

Development of a Supercooled Large Droplet Environment within theNRC Altitude Icing Wind Tunnel

Developing an Ice Protection System to Deal with the RecentlyDefined Supercooled Large Droplet (SLD) Environment

SLD Considerations for General Aviation Aircraft

SLD Icing Wind Tunnel Testing of a General Aviation Aircraft WingSection

On Impact of Spherical Ice Particles on Thin Liquid Films duringGlaciated Icing


David M. Orchard, Catherine Clark, Myron Oleskiw, NationalResearch Council Canada

Jerry L. Jordan, CAV Aerospace Inc.

Jim R. Hoppins, Textron Aviation

Garrett Homan, Cirrus Aircraft

Daniel Martin Kintea, Ilia Roisman, Cameron Tropea,Technische Universität Darmstadt

Time

Time

Paper No.

Paper No.

Title

Title

15:30

15:30

Session Time:

Session Time:

Tuesday, June 23

Tuesday, June 23

Deicing and Anti-icing of Structures, Ground Operations in Icing Conditions - RunwayDeicing

Deicing and Anti-icing of Structures, Ground Operations in Icing Conditions - AircraftGround Deicing

Session Code:

Session Code:

ICE201

ICE202

Room Libuse

Room Libuse

This session includes papers for a wide range of topics from the protection of wind turbines from the effects of ice accretion, the deicing of ships andground and structures, the methods of deicing of aircraft prior to departures, the effects of ground fog at cold temperatures, the prevention andclearing of ice from runways, and regulations for the use of deicing fluids and chemicals. Icing papers for topics that do not fit in the other threesessions are invited to submit in this session.

Gene Addy, NASA John Glenn Research Center; Ben C. Bernstein, Leading EdgeAtmospherics; Robert J. Flemming; Richard Lewis, Airbus; Jeanne G. Mason,Boeing Commercial Airplanes; Jen-Ching Tsao, Ohio Aerospace Institute

Organizers -

Caroline Laforte, Anti-Icing Materials Intl. Laboratory; Alun Williams, Airbus SASChairpersons -

4:00 p.m.

4:30 p.m.

5:00 p.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

ORAL ONLY

2015-01-2099

ORAL ONLY

2015-01-2076

2015-01-2077

2015-01-2082

Inlet Guide Vane Ice Impact Fragmentation Testing

Ice Particle Impacts on a Flat Plate

Ice Particle Collision with a Dry Rigid Substrate and Its Breakup

Anti-Icing Comparative Performance Skid Test for Runway Deicers

Carbon Brake Catalytic Oxidation

Computational and Experimental Investigation of Ice ParticleAccretion in a Generic Pack Discharge Duct



Yiqiang Han, Jared Soltis, Jose Palacios, Pennsylvania StateUniversity

Mario Vargas, Charles Ruggeri, Peter Struk, Mike Pereira,Duane Revilock, Richard Kreeger, NASA Glenn ResearchCenter

Ilia Roisman, Darmstadt University of Technology; TobiasHauk, Elmar Bonaccurso, Airbus Group Innovations; CameronTropea, Technical Univ. of Darmstadt

Caroline Laforte, Anti-Icing Materials Intl. Laboratory; NealWesley, LNT Solutions; Marc Mario Tremblay, Anti-IcingMaterials Intl. Laboratory

Alun Williams, Airbus SAS; Michael Arriaga, Boeing Co

Andreas Tramposch, Wolfgang Hassler, Reinhard F.A. Puffing,FH JOANNEUM GmbH Graz

ORAL ONLY


08:30

10:30

Session Time:

Session Time:

Tuesday, June 23

Tuesday, June 23

Deicing and Anti-icing of Structures, Ground Operations in Icing Conditions - Wind TurbineIcing, Ground Safety, and a New Icing Test Facility

Aircraft Inflight Icing - Rotorcraft Ice Shedding Analysis

Session Code: ICE203

Room Libuse

This session covers the ground deicing topics assocaited with runway surfaces. Included are presentations on runway deicers, the damge thatrunway deicers can cause to aircraft brakes, and the use of microwaves to safely deice runway surfaces.

This session includes a presentation on the growing field of wind tunrbine icing and a presentation on icing accifents that have occurred in canada.Also included is a presentation on an EASA wind tunnel test project for the effects of anti-icing fluids on the performance of horizontal stabiliser duringaircraft take-off, called the DIFT project.

Gene Addy, NASA John Glenn Research Center; Ben C. Bernstein, Leading EdgeAtmospherics; Robert J. Flemming; Richard Lewis, Airbus; Jeanne G. Mason,Boeing Commercial Airplanes; Jen-Ching Tsao, Ohio Aerospace Institute

Gene Addy, NASA John Glenn Research Center; Robert J. Flemming; RichardLewis, Airbus; Jeanne G. Mason, Boeing Commercial Airplanes; Jen-Ching Tsao,Ohio Aerospace Institute

Organizers -

Organizers -

Caroline Laforte, Anti-Icing Materials Intl. Laboratory; Alun Williams, Airbus SAS

Caroline Laforte, Anti-Icing Materials Intl. Laboratory; Alun Williams, Airbus SAS

Chairpersons -

Chairpersons -

11:00 a.m.

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

ORAL ONLY

2015-01-2081

ORAL ONLY

ORAL ONLY

2015-01-2160

Capabilities of the New Icing Wind Tunnel Vienna

Developing a Novel Ice Protection System for Wind Turbine BladesUsing Vibrations of Both Short and Long Wavelengths

"DIFT" Research Project: A Wind Tunnel Evaluation of the Effect ofAnti-icing Fluids on the Performance of Horizontal Stabiliser duringAircraft Take-off

TC/FAA Propulsion Icing Wind Tunnel Research Simulating Ice PelletConditions

Effects of Prolonged Exposure to UV and Water on Super-Hydrophobic Surfaces at Ambient and Icing Conditions



Hermann Ferschitz, Otto Bucek, Michael Wannemacher, RTA

Hossein Habibi, Brunel Innovation Centre (BIC); GrahamEdwards, TWI Ltd.; Liang Cheng, Haitao Zheng, BrunelInnovation Centre (BIC); Adam Marks, TWI Ltd.; VassiliosKappatos, Cem Selcuk, Tat-Hean Gan, Brunel InnovationCentre (BIC)

Alberto Fernandez, EASA

Marco Ruggi, APS Aviation Inc.

Alidad Amirfazli, York Univ.

Time

Time

Paper No.

Paper No.

Title

Title

13:30Session Time:

Tuesday, June 23

Aircraft Inflight Icing - Droplet Concentration & Impingement (Part 1 of 2)

Session Code:

Session Code:

ICE102

ICE108

Room Neklan/Vlasta

Room Neklan/Vlasta

This session includes analytical modeling of rotor blade ice shedding, shed ice size prediction and ice release from a rotating propeller.

This session includes a validation study of icing cloud concentration factor prediction, and a numerical study of Pitot tube placement using optimizedgrids.

Gene Addy, NASA John Glenn Research Center; Philip J. Alldridge, SikorskyAircraft Corp.; Ben C. Bernstein, Leading Edge Atmospherics; Gerard Duprat,Airbus; Robert J. Flemming; Richard Lewis, Airbus; Michael Oliver, Nasa GlennResearch Center; Jen-Ching Tsao, Ohio Aerospace Institute


Organizers -

Organizers -

Philip J. Alldridge, Sikorsky Aircraft Corp.; Mario Vargas, NASA Glenn ResearchCenter

Philip J. Alldridge, Sikorsky Aircraft Corp.; Mario Vargas, NASA Glenn ResearchCenter

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

2015-01-2080

ORAL ONLY

2015-01-2079

2015-01-2085

ORAL ONLY

2015-01-2120

Additional Considerations for Analytical Modeling of Rotor Blade Ice

Rotor Blade Shed Ice Length Prediction

Analysis of Ice Release from a Rotating Propeller

Validation of Predicted Icing Cloud Depletion and Over-Concentration Factors

Numerical Analysis for the Placement of a Pitot Tube Using OptimizedGrids

Ice Adhesion Performance of Superhydrophobic Coatings inAerospace Icing Conditions


Roger J. Aubert, Bell Helicopter Textron

Jared Soltis, Jose Palacios, Pennsylvania State University

Colin Hatch, Jason Moller, Eleftherios Kalochristianakis, IanRoberts, AeroTex UK LLP

James Brown, Airbus Operations

Isik Ozcer, Patrick Lagacé, David Switchenko, Guido Baruzzi,Cristhian Aliaga, ANSYS; John Dow, DOW International LLC;Wagdi Habashi, McGill University

Yong Han Yeong, Eric Loth, Univ. of Virginia; Jack Sokhey,Rolls-Royce North America; Alexis Lambourne, Rolls RoycePlc

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

08:30

10:30

Session Time:

Session Time:

Tuesday, June 23

Tuesday, June 23

Aircraft Inflight Icing - Droplet Concentration & Impingement (Part 2 of 2)

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - NASA PSL Ice CrystalTest Facility

Session Code:

Session Code:

ICE108

ICE409

Room Neklan/Vlasta

Room Neklan/Vlasta

This session includes a numerical study of water drop impingement on a 3D engine inlet and a numerical investigation on shedding of engine fan iceaccretion and a generalized drop collection efficiency correlation for an airfoil

This session includes presentations on recent developments for and tests in NASA's PSL ice crystal test facility.



Organizers -

Organizers -

Dave Dischinger, Honeywell Aerospace; Peter M. Struk, NASA Glenn ResearchCenter

Dave Dischinger, Honeywell Aerospace; Peter M. Struk, NASA Glenn ResearchCenter

Chairpersons -

Chairpersons -

1:30 p.m.

2:00 p.m.

3:30 p.m.

2015-01-2091

2015-01-2090

ORAL ONLY

Numerical Investigation of Ice Shedding Associated with Engine FanIcing

Ice Accretion Prediction on Engine Nacelles in Liquid Phase Clouds

PSL Icing Facility Update



Ryosuke Hayashi, Makoto Yamamoto, Tokyo University ofScience

Serkan Ozgen, Middle East Technical University; Volkan Tatar,Turkish Engine Industries, Inc.; Nermin Ugur, Middle EastTechnical University; Ilhan Gorgulu, Turkish Engine Industries,Inc.

Queito P. Thomas, Thomas Griffin, NASA Glenn ResearchCenter

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

13:30

15:30

Session Time:

Session Time:

Wednesday, June 24

Wednesday, June 24

Aircraft Inflight Icing - Icing Simulation Model Tool Development

Aircraft Inflight Icing - Icing CFD (Part 1 of 2)

Session Code:

Session Code:

ICE110

ICE111



This session includes a numerical improvement of 2D ice accretion simulation capability of ONERA2D, a study on ice adhesion and a reduced ordermodeling approach to explore the 14 CFR 25/29 Appendix C icing envelope.

This session includes a CFD evaluation of ice accretion scaling methods using the ONERA2D icing code, , a comparison of natural flight test resultswith CFD simulations using FENSAP-ICE, and an overview of the A350XWB icing certification program.

Gene Addy, NASA John Glenn Research Center; Philip J. Alldridge, SikorskyAircraft Corp.; Ben C. Bernstein, Leading Edge Atmospherics; Gerard Duprat,Airbus; Robert J. Flemming; Robert J. Flemming; Richard Lewis, Airbus; MichaelJames Oliver; Jen-Ching Tsao, Ohio Aerospace Institute


Organizers -

Organizers -

Dan Fuleki, National Research Council Canada; Eric Loth, Univ. of Virginia

Dan Fuleki, National Research Council Canada; Eric Loth, Univ. of Virginia

Chairpersons -

Chairpersons -

4:00 p.m.

4:30 p.m.

5:00 p.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

ORAL ONLY

2015-01-2156

ORAL ONLY

2015-01-2103

ORAL ONLY

2015-01-2164

Update on NASA¿s Propulsion Systems Lab Ice Crystal CloudCharacterization

Ice Crystal Icing Engine Testing in the NASA Glenn ResearchCenter's Propulsion Systems Laboratory: Altitude Investigation

NASA Experimental Plans for Second Ice Crystal Icing Test with aHeavily Instrumented Engine

Improvement of Ice Accretion Prediction Capability of the ONERA 2DIcing Code

A Reduced Order Modeling Approach for Exploring Appendix C

Icing Modelling with Level-Set Approach



Judith Foss Van Zante, NASA John Glenn Research Center

Michael Oliver, NASA Glenn Research Center

Ashlie B. Flegel, NASA Glenn Research Center

Christian Bartels, Julien Cliquet, Carlos Bautista, Airbus

Zhao Zhan, Wagdi Habashi, Marco Fossati, McGill Univ.

Dorian Pena, Yannick Hoarau, Strasbourg University; EricLaurendeau, Ecole Polytechnique Montreal

ORAL ONLY


08:30

10:30

Session Time:

Session Time:

Wednesday, June 24

Wednesday, June 24

Aircraft Inflight Icing - NASA/FAA/ONERA Swept-wing Icing & Aerodynamics (Part 1 of 2)

Aircraft Inflight Icing - NASA/FAA/ONERA Swept-wing Icing & Aerodynamics (Part 2 of 2)

Session Code:

Session Code:

ICE104

ICE104



This session includes an overall research project overview and current status , a 3D swept-wing hybrid model design and a detached eddy simulation(DES) of the model in the NASA Icing Research Tunnel (IRT).


Organizers -

Thomas H. Bond, Federal Aviation Adminstration; Mark G. Potapczuk, NASA JohnGlenn Research Center

Chairpersons -

10:30 a.m.

11:00 a.m.

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2015-01-2111

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

2015-01-2122

A350XWB Icing Certification Overview

Comparison of Natural Flight Test Results with CFD simulation usingFENSAP-ICE

Numerical Study of Scaling Rules for Ice Accretion Tests

NASA/FAA/ONERA Swept-Wing Icing and Aerodynamics: Summaryof Research and Current Status

Design of Wind Tunnel Models for Full-Scale Swept-Wing IceAccretion

Detached Eddy Simulation on a Swept Hybrid Model in the IRT



Marie-Laure Toulouse, Richard Lewis, Airbus

Yana Indrulenayte, PAO "Tupolev"; Wagdi Habashi, MarcoFossati, McGill Univ; Guido Baruzzi, Newmerical TechnologiesInc

Philippe VILLEDIEU, Pierre Trontin, Charlotte BAYEUX,ONERA

Andy Broeren, NASA Glenn Research Center

Gustavo Eidji Camarinha Fujiwara, University of Washington;Brian Woodard, Univ. of Illinois at Urbana; Michael Bragg,University of Washington

Cameron Butler, Eric Loth, University of Virginia

Time

Time

Paper No.

Paper No.

Title

Title

13:30

15:30

Session Time:

Session Time:

Wednesday, June 24

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Supercooled LargeDrop Icing PhysicsSession Code: ICE411

Room Congress Hall

This session includes a 3D ice accretion modeling on this hybrid model, a full-span ice shape generation method, a velocity scaling study on swept-wing ice shape, and initial results of low Reynolds number iced aerodynamic performance of the sub-scaled hybrid model.

This session includes presentations on recent developments in the determination of the physics involved in the prediction of supercooled large drop(SLD) icing.



Organizers -

Organizers -

Thomas H. Bond, Federal Aviation Adminstration; Mark G. Potapczuk, NASA JohnGlenn Research Center

Biagio M. Esposito, CIRA Scpa; Jim R. Hoppins, Textron Aviation

Chairpersons -

Chairpersons -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

8:30 a.m.

9:00 a.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

2015-01-2101

ORAL ONLY

Method to Generate Full-Span Ice Shape on Swept Wing Using IcingTunnel Data

Initial Low-Reynolds Number Iced Aerodynamic Performance forCRM Wing

3D Modeling of Ice Accretion with Application to Swept Wing Test-Cases

Velocity Effect on Swept-Wing Ice Accretion for ScalingConsideration

Impact of Supercooled Liquid Drops onto Cold Solid Substrates

Experimental Investigation and Numerical Modelling of SLD ImpactPhenomena


Sam Lee, Vantage Partners, LLC

Brian Woodard, Univ of Illinois at Urbana-Champaign; JeffreyDiebold, University of Illinois; Andy P. Broeren, NASA John H.Glenn Research Center; Sam Lee, Vantage Partners, Inc.;Mark Potapczuk, NASA John Glenn Research Center; MichaelBragg, University of Washington

Emmanuel Radenac, Pierre Trontin, Helene Gaible, HerveBezard, Philippe Villedieu, ONERA

Jen-Ching Tsao, Ohio Aerospace Institute

Hai Li, Ilia Roisman, Cameron Tropea, Technical Univ. ofDarmstadt

Philippe Villedieu, Pierre Trontin, Pierre Berthoumieu, ONERA

Time

Time

Paper No.

Paper No.

Title

Title

08:30Session Time:

Wednesday, June 24

Wednesday, June 24

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - ComputationalModeling of Supercooled Large Drop Phenomena

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Supercooled LargeDrop Icing Studies

Session Code:

Session Code:

ICE412

ICE413

Room Congress Hall

Room Congress Hall

This session includes presentations on recent developments in the use of computational fluid dynamics (CFD) for the prediction of the effects of largedrop (SLD) icing conditions.

This session includes additional presentations on recent developments for the prediction of the effects of supercooled large drop (SLD) icingconditions.



Organizers -

Organizers -

Biagio M. Esposito, CIRA Scpa; Jim R. Hoppins, Textron Aviation

Steven L. Morris, Engineering Systems Inc.; David L. Rigby, Vantage PartnersLimited

Chairpersons -

Chairpersons -

9:30 a.m.

10:30 a.m.

11:00 a.m.

2015-01-2100

2015-01-2108

ORAL ONLY

Investigation of the Splashing Phenomenon of Large Droplets forAviation Safety

A Combined Post-processing Method for SLD Modeling

Three-dimensional Eulerian Modeling of Secondary Droplet Flows



Yongsheng Lian, Yisen Guo, University of Louisville

Julien Cliquet, Christian Bartels, Carlos Bautista, Airbus

David R. Bilodeau, Wagdi Habashi, McGill University; GuidoBaruzzi, Isik A. Ozcer, Newmerical Technologies International;John P. Dow, Sr., Dow International L.L.C.; Marco Fossati,McGill University

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

10:30

13:30

Session Time:

Session Time:

Wednesday, June 24

Aircraft Inflight Icing - Thermal IPS AnalysisSession Code: ICE113

Room Congress Hall

This session includes an experimental study of altitude effect on thermal IPS performance, an analysis of thermal ice protection of restraining grids onaircraft, an unsteady thermal simulation of aircraft wing IPS integrated in metallic or composite structures, and an update on recent advances in theGlennIce icing model.


Organizers -

Stephen T. McClain, Baylor Univ.; Mario Vargas, NASA Glenn Research CenterChairpersons -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

2015-01-2118

2015-01-2119

2015-01-2117

ORAL ONLY

2015-01-2094

2015-01-2093

2015-01-2095

Interaction of Supercooled Large Droplets with Aerodynamic Profile

Modeling of Droplet Deformation and Breakup in the SupercooledLarge Droplet Regime

Comparative Investigation on Effect of Droplet Deformation Modelson SLD Icing

Altitude Effects on Thermal Ice Protection System Performance: AStudy of an Alternative Simulation Approach

Recent Advances in the LEWICE Icing Model

Unsteady Thermal Simulations of Wing Ice Protection SystemsIntegrated in Metallic or Composite Structures

Thermal Ice Protection of Restraining Grids in the EnvironmentalControl System of Passenger Aircraft




Sergey Alekseyenko, Dnipropetrovsk National University;Michael Sinapius, Martin Schulz, Technische UniversitätBraunschweig; Oleksandr Prykhodko, Dnipropetrovsk NationalUniversity

Shinan Chang, Chao Wang, Mengyao Leng, Beijing Univ. ofAeronautics & Astronautics

Miki Shimura, Makoto Yamamoto, Tokyo University of Science

Gene Addy, NASA John Glenn Research Center; William B.Wright, Vantage Partners, LLC; David Orchard, MyronOleskiw, National Research Council Canada

William B. Wright, Vantage Partners Limited; Peter Struk,NASA John Glenn Research Center; Tadas Bartkus, OhioAerospace Institute; Gene Addy, NASA John Glenn ResearchCenter

Maxime Henno, SONACA sa

Wolfgang Hassler, Reinhard F.A. Puffing, Andreas Tramposch,FH JOANNEUM GmbH Graz


15:30Session Time:

Wednesday, June 24

Wednesday, June 24

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Ice Particle Melting inTurbine Engines

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Ice Particle Accretionand Boundary Conditions in Turbine Engines

Session Code:

Session Code:

ICE406

ICE407

Room Gallery

Room Gallery

This session includes presentations on recent developments in the observation methods and prediction of ice crystal melting in turbine engines.

This session includes presentations on the prediction of ice particle accretion and the boundary conditions for ice crystals predictions for turbineengines.



Organizers -

Organizers -

Alice Grandin, Airbus UK; Helene Mazet, Snecma

Alice Grandin, Airbus UK; Helene Mazet, Snecma

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

ORAL ONLY

2015-01-2107

ORAL ONLY

High Speed Visualization of Partial Melting in Ice Particles

Simulation of Ice Particle Melting in the NRCC RATFac Mixed-PhaseIcing Tunnel

Development of a Shape-Dependent Melting Model for Irregular IceParticles Based On Melting Experiments in an Acoustic Levitator



Sihong Yan, Jose Palacios, Penn State Univ.-University Park;Richard Kreeger, NASA John Glenn Research Center; ChiongTan, General Electric

Tom Currie, Dan Fuleki, Craig Davison, National ResearchCouncil Canada

Elmar Bonaccurso, Tobias Hauk, Airbus Group Innovations;Ilia Roisman, Cameron Tropea, Technical Univ of Darmstadt;Philippe Villedieu, Pierre Trontin, ONERA

Time

Time

Paper No.

Paper No.

Title

Title

08:30

10:30

Session Time:

Session Time:

Wednesday, June 24

Wednesday, June 24

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Ice Crystal Modeling(Part 1 of 5)


Session Code:

Session Code:

ICE408

ICE408

Room Gallery

Room Gallery

This session includes presentations on recent developments in ice crystal simulation and modeling.



Gene Addy, NASA John Glenn Research Center; Ben C. Bernstein, Leading Edge

Organizers -

Organizers -

Shengfang Liao, United Technologies Pratt and Whitney; Wolfgang A. Sandel,Honeywell Aerospace

Chairpersons -

10:30 a.m.

11:00 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2015-01-2116

2015-01-2115

ORAL ONLY

ORAL ONLY

ORAL ONLY

Ice Accretion Measurements on an Airfoil and Wedge in Mixed-PhaseConditions

Surface Energy Influence on Supercooled Water Crystallization: AComputational Study

Simulation of Ice Crystal Accretion using ONERA 3D Icing Suite

Ice Crystal Accretion Modeling within ONERA¿s Icing Tools

Modeling of the Accretion and Shedding Behavior of Ice Layers onWarm Surfaces



Peter Struk, NASA John Glenn Research Center; TadasBartkus, Jen-Ching Tsao, Ohio Aerospace Institute; TomCurrie, Dan Fuleki, National Research Council Canada

Antonio Criscione, TAKATA AG, EMEA New DevicesEngineering; Suad Jakirlic, Technical Univ. of Darmstadt;Zeljko Tukovic, University of Zagreb; Ilia Roisman, CameronTropea, Technical Univ. of Darmstadt

Jean-Mathieu Senoner, Pierre Trontin, Valentin Biasi,Emmanuel Radenac, Philippe Villredieu, ONERA

Pierre Trontin, Jean-Mathieu Senoner, Philippe Villedieu,ONERA

Daniel Martin Kintea, Ilia Roisman, Cameron Tropea,Technische Universität Darmstadt


13:30

15:30

Session Time:

Session Time:

Wednesday, June 24

Aircraft Inflight Icing - IPS, Including Rotorcraft Ice Protection SystemsSession Code: ICE112

Room Libuse

This session includes a numerical study of the electrothermal deicing process on a helicopter rotor blade, an experimental study of icing effect on amechanical deicing system based on natural frequency, and a study of open loop anti-icing control of rotor blade heaters.

Atmospherics; Robert Busto, Federal Aviation Administration; Robert J. Flemming;David Johns, Transport Canada; Richard Lewis, Airbus; Jeanne G. Mason,Boeing Commercial Airplanes; Jen-Ching Tsao, Ohio Aerospace Institute


Organizers -

Shengfang Liao, United Technologies Pratt and Whitney; Wolfgang A. Sandel,Honeywell Aerospace

Stephane Catris, Airbus Helicopters Inc.; Emmanuel Radenac, ONERA

Chairpersons -

Chairpersons -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

8:30 a.m.

9:00 a.m.

2015-01-2133

2015-01-2132

2015-01-2131

ORAL ONLY

2015-01-2102

ORAL ONLY

Performance Modeling of Honeywell Turbofan Engine Tested with IceCrystal Ingestion in the NASA Propulsion System Laboratory

Three Dimensional Simulation of Flow in an Axial Low PressureCompressor at Engine Icing Operating Points

Ice Particle Analysis of the Honeywell ALF502 Engine Booster

HAIC Achievements at M24

Numerical Investigation of the Electrothermal De-Icing Process of aRotor Blade

Open Loop Anti-ice Control of Rotorblade Heaters



Joseph P. Veres, Scott M. Jones, Philip C. E. Jorgenson,NASA John Glenn Research Center

David L. Rigby, Vantage Partners Limited; Joseph Veres, ColinBidwell, NASA John Glenn Research Center

Colin Bidwell, NASA John Glenn Research Center; DavidRigby, Vantage Partners Limited

Fabien Dezitter, Alice Grandin, Airbus; Christiane Voigt, DLR;Philippe Villedieu, ONERA; Franck Hervy, DGA CEPR; Jean-Louis Brenguier, Météo-France; Gilles Zalamansky, DassaultAviation

Guilin Lei, Wei Dong, Jianjun Zhu, Mei Zheng, Shanghai JiaoTong University

Richard Carpino, James Mullen, UTC Aerospace Systems;Roger J. Aubert, Bell Helicopter Textron

Time

Time

Paper No.

Paper No.

Title

Title

08:30Session Time:

Wednesday, June 24

Wednesday, June 24

Aircraft Inflight Icing - Rotorcraft Icing Numerical Simulation

Aircraft Inflight Icing - Inflight IPS Analysis

Session Code:

Session Code:

ICE103

ICE114

Room Libuse

Room Libuse

This session includes numerical simulation of rotor blade icing, rotor blade ice shedding and ice adhesion performance of super hydrophilic coatings inicing conditions.

This session includes a 3D numerical study of bleed air IPS parametric analysis, an update on development and evaluation of an integrated inflightIPS - The JEDI ACE project, and a summary report on certification inflight natural icing test results for validating the PZL Mielec M28 bleed air IPSCFD.



Organizers -

Organizers -

Stephane Catris, Airbus Helicopters Inc.; Emmanuel Radenac, ONERA

Roger J. Aubert, Bell Helicopter Textron; Brian D. Matheis, UTC AerospaceSystems

Chairpersons -

Chairpersons -

10:30 a.m.

11:00 a.m.

11:30 a.m.

1:30 p.m.

ORAL ONLY

2015-01-2121

2015-01-2088

2015-01-2109

Ice Accretion Effects on Fully-Articulated Rotors in Forward Flight

Numerical Simulation of Helicopter Blade Ice Shedding using aBilinear Cohesive Zone Model

Progress in Rotorcraft Icing Computational Tool Development

3D Computational Methodology for Bleed Air Ice Protection SystemParametric Analysis



Daniel Kelly, Marco Fossati, McGill Univ.; Giuseppe Quaranta,Pierangelo Masarati, Politecnico di Milano; Wagdi Habashi,McGill Univ.

Yong Chen, Liang Fu, Shanghai Jiao Tong Univ

Richard E. Kreeger, NASA John Glenn Research Center;Lakshmi Sankar, Georgia Institute of Technology; RobertNarducci, Boeing Co.; Robert Kunz, Penn State University

Rodrigo Domingos, Daniel Silva, Embraer

Time

Time

Paper No.

Paper No.

Title

Title

10:30

13:30

Session Time:

Session Time:

Wednesday, June 24

Wednesday, June 24

Aircraft Inflight Icing - Rotorcraft Icing Test

Environmental Icing Meteorology and Instruments - In-situ Icing/SLD Detection (Part 1 of 2)

Session Code:

Session Code:

ICE101

ICE304

Room Libuse

This session includes the experimental simulations of ice accretion, 2D ice shape scaling evaluation from rotorcraft blade icing tests, icedaerodynamics on 2D rotor blades and full-vehicle configurations, and rotorcraft icing certification using Helicopter Inflight Icing System (HISS) testresults.


Organizers -

Roger J. Aubert, Bell Helicopter Textron; Brian D. Matheis, UTC AerospaceSystems

Chairpersons -

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:30 p.m.

5:00 p.m.

ORAL ONLY

2015-01-2110

2015-01-2128

2015-01-2129

2015-01-2127

Development and Evaluation of Integrated In-flight Ice ProtectionSystems ¿ The JediAce Project

Certification Flight Tests in Natural Icing of the PZL Mielec M28Commuter Turboprop Airplane

Use of HISS Test Results for Rotorcraft Civil Certification

2D Ice Shape Scaling for Helicopter Blade Profiles in Icing WindTunnel

2D Polar Assessment in Icing Wind Tunnel for iced Helicopter BladeProfiles




Nadine Rehfeld, Andreas Brinkmann, Gerhard Pauly,Fraunhofer IFAM; Benoit Berton, Dassault Aviation SA; TaroTanaka, Fuji Heavy Industries Ltd; Shigeo Kimura, KanagawaInstitute of Technology; Hirotaka Sakaue, Katsuaki Morita,Japan Aerospace Exploration Agency; Francesc Diaz,Magdalena Aguiló, Airán Ródenas Seguí, Javier Martínez,Universitat Rovira i Virgili

Jozef Brzeczek, Janusz Pietruszka, Polskie Zaklady LotniczeSp. z o.o.; Robert J. Flemming; Ben C. Bernstein, LeadingEdge Atmospherics

Enrico Bellussi, Agusta-Westland

Andrea Munzing, Stephane Catris, Airbus Helicopters Inc.

Andrea Munzing, Airbus Helicopters Inc.; Franck Hervy, DGACEPR; Stephane Catris, Airbus Helicopters Inc.


15:30Session Time:

Wednesday, June 24

Environmental Icing Meteorology and Instruments - In-situ Icing/SLD Detection (Part 2 of 2)Session Code: ICE304

Room Neklan/Vlasta

Room Neklan/Vlasta

This session describes new instruments under development for icing conditions aloft, including supercooled large drop (SLD) icing conditions.

This session describes new instruments under development for icing conditions aloft, including supercooled large drop (SLD) icing conditions.



Organizers -

Organizers -

Erik Langhofer, Boeing Commercial Airplanes; Manuel Thorez, Zodiac Aerospace

Ismail Gultepe; Thomas Stephen Rowe Richards, GKN Aerospace SPG

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

ORAL ONLY

2015-01-2105

2015-01-2106

2015-01-2112

ORAL ONLY

2015-01-2113

New Optical Technologies for PRIMARY and ADVISORY Ice DetectionSystems

Primary Ice Detection Certification Under the New FAA and EASARegulations

Analysis of Flight Test Results of the Optical Ice Detector

Wireless and Flexible Ice Detection on Aircraft

A New Technique for Automated Freezing Drizzle Detection and itsImplications on Prior Freezing Drizzle-Based Climatological Studies

Freezing Fog and Drizzle Observations



Francois LaRue, Zodiac Aerospace

Darren Glenn Jackson, UTC Aerospace Systems

Mark Ray, Kaare Anderson, UTC Aerospace Systems

Thomas Schlegl, Michael Moser, Eologix Sensor TechnologyGmbH; Hubert Zangl, Alpen-Adria-Universität Klagenfurt

Scott Landolt, Marcia Politovich, National Center forAtmospheric Research; Jennifer Black, NCAR; Kent Goodrich,Andrew Schwartz, Andrew Gaydos, Daniel Adriaansen,National Center for Atmospheric Research

Ismail Gultepe, Environment Canada; Michael Pavolonis,NOAA/NESDIS; Binbin Zhou, NOAA; Randolph Ware,Radiometrics; Robert Rabin, NOAA NSSL/CIMMS; WilliamBurrows, Jason Milbrandt, Louis Garand, Environment Canada

Time

Time

Paper No.

Paper No.

Title

Title

08:30

10:30

Session Time:

Session Time:

Wednesday, June 24

Wednesday, June 24

Environmental Icing Meteorology and Instruments - HAIC/HIWC Nowcasting and RemoteSensing (Part 1 of 2)

Environmental Icing Meteorology and Instruments - HAIC/HIWC Nowcasting and RemoteSensing (Part 2 of 2)

Session Code:

Session Code:

ICE306

ICE306

Room Neklan/Vlasta

Room Neklan/Vlasta

This session explores the emerging remote detection and nowcasting capabilities for HAIC/HIWC aloft.

This session explores the emerging remote detection and nowcasting capabilities for HAIC/HIWC aloft.

Gene Addy, NASA John Glenn Research Center; Ben C. Bernstein, Leading EdgeAtmospherics; Robert J. Flemming; Richard Lewis, Airbus; Vince LoPresto, UnitedTechnologies Aerospace; Jeanne G. Mason, Boeing Commercial Airplanes; Jen-Ching Tsao, Ohio Aerospace Institute

Gene Addy, NASA John Glenn Research Center; Ben C. Bernstein, Leading EdgeAtmospherics; Robert J. Flemming; Richard Lewis, Airbus; Vince LoPresto, UnitedTechnologies Aerospace; Jeanne G. Mason, Boeing Commercial Airplanes; Jen-

Organizers -

Organizers -

Melissa Bravin, The Boeing Company; William Smith, NASA Langley ResearchCenter

Chairpersons -

1:30 p.m.

2:00 p.m.

2:30 p.m.

2015-01-2123

ORAL ONLY

2015-01-2124

Overview of the HAIC ¿Space-borne Observation and Nowcasting ofHigh Ice Water Content Regions¿ Sub-Project and Mid-Term Results

Detection of Ice Crystal Engine Icing Conditions with the Algorithmfor Prediction of High Ice Water Content Areas (ALPHA): Overviewand Validation with Research Aircraft Data

The Use of RDT Nowcasting Tool for Detecting Convective AreasAssociated with High Ice Water Content during HAIC/HIWC FieldCampaign


Eric Defer, CNRS-LERMA; Jean-Louis Brenguier, Meteo-France; Jos De Laat, KNMI; Julien Delanoe, CNRS-LATMOS;Fabien Dezitter, Airbus; Michael Faivre, CNRS-LERMA;Amanda Gounou, Meteo-France; Alice Grandin, Airbus;Anthony Guignard, CNRS-LATMOS; Jan Fokke Meirink,KNMI; Jean-Marc Moisselin, Meteo-France; Frederic Parol,CNRS-LOA; Alain Protat, BoM; Claudine Vanbauce, CNRS-LOA

Jennifer Black, NCAR; George McCabe, National Center forAtmospheric Research; J. Walter Strapp, Met Analytics Inc.;Rabindra Palikonda, Louis Nguyen, NASA Langley ResearchCenter; Rodney Potts, Bureau of Meteorology; Julie Haggerty,NCAR

Amanda Gounou, Jean-Marc Moisselin, Frédéric Autones,Dominique Levaillant, Jean-Louis Brenguier, Météo-France;Eric Défer, Michael Faivre, CNRS; Alice Grandin, FabienDezitter, Airbus; Sandra Turner, ATMOSPHERE, Systèmes &Services


13:30

15:30

Session Time:

Session Time:

Thursday, June 25

Aircraft In-flight Icing - New Icing Test Facilities, Advanced Icing Test Capabilities, and anIcing Facility Capability Update (Part 1 of 4)Session Code: ICE118


This session includes a report on the capability of the new Icing Wind Tunnel Vienna, a report on the development of the UTC Aerospace Systems(UTAS) Advanced Icing Wind Tunnel, and a report on improvement to GKN IWT for glaciated and mixed phase icing conditions.

Ching Tsao, Ohio Aerospace Institute


Organizers -

Eric Defer, CNRS; Amanda Gounou

Daniel C. Knezevici, GE Aviation; Judith Foss Van Zante, NASA John GlennResearch Center

Chairpersons -

Chairpersons -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

2015-01-2130

Inferring High Ice Water Content from the Geostationary SatelliteImager SEVIRI in Support of Aviation and the 2015 HAIC FieldCampaign

On the Origin of High Altitude High Ice Water Content Regions inOceanic Deep Convection

Detection of Cloud Water/Ice Contents in Convective Systems ¿Implications for Aircraft In Service Events

An Investigation into Location and Convective Lifecycle Trends in anIce Crystal Icing Engine Event Database


Jos De Laat, KMNI; Amanda Gounou, Jean-Marc Moisselin,Meteo-France; Julien Delanoe, LATMOS-UVSQ-CNRS;Anthony Guignard, LATMOS - Institut Pierre-SimonLAPLACE; Jan Fokke Meirink, KNMI

Alexei V. Korolev, Environment Canada; AlfonsSchwarzenboeck, CNRS; Andrew Ackerman, NASA GoddardInstitute for Space Studies; Julien Delanoe, CNRS; FabienDezitter, Airbus Operations SAS; Christopher Dumont, FederalAviation Administration; Ann Fridlind, NASA Goddard Institutefor Space Studies; Alice Grandin, Airbus; Lyle Lilie, ScienceEngineering Associates Inc; Rodney Potts, Alain Protat, BoM;Adam Varble, University of Utah; J. Walter Strapp, MetAnalytics Inc.; Edward Zipser, University of Utah

Christiane Voigt, German Aerospace Center DLR; Ralf Weigel,Sergej Molleker, Johannes Gutenberg-Universität Mainz;Fabien Dezitter, Airbus Operations SAS; Stephan Borrmann,Johannes Gutenberg-Universität Mainz; Alice Grandin, Airbus;Tina Jurkat, German Aerospace Center DLR; ManfredWendisch, Universität Leipzig; Hans Schlager, FabianHeidelberg, German Aerospace Center DLR

Melissa Bravin, Boeing Commercial Airplanes; J. WalterStrapp, Met Analytics Inc.; Jeanne Mason, Boeing CommercialAirplanes


08:30Session Time:

Thursday, June 25

Thursday, June 25

Aircraft In-flight Icing - New Icing Test Facilities, Advanced Icing Test Capabilities, and anIcing Facility Capability Update (Part 2 of 4)Session Code: ICE118


This session includes a report on the GLACIER Icing Facility operation lessons learned for the past 5 years, a report on DLR deicing facility and icingdetection development, a study of Interferometric Laser Imaging for the cloud calibration of a newly built von Karman Institute for Fluid Dynamics (VKI)icing wind tunnel.


Organizers -

Daniel C. Knezevici, GE Aviation; Judith Foss Van Zante, NASA John GlennResearch Center

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

2015-01-2144

2015-01-2143

2015-01-2145

Preliminary Calibration of the Icing Wind Tunnel Braunschweig withRespect to Mixed Phase and Glaciated Icing Conditions

Design and Calibration of a New High-Speed Insert for the NRCAltitude Icing Wind Tunnel

An Assessment of the SEA Multi-Element Sensor for Liquid WaterContent Calibration of the IRT

The GLACIER Icing Facility-Lessons Learnt in Five Years ofOperation

Icing Wind Tunnel and Detection of the Formation of Icing by HeatCristallization

Conversion of the VKI Cold Wind Tunnel CWT-1 into an Icing WindTunnel Including Diagnostics by ILIDS



Arne Baumert, Technische Universität Braunschweig; StephanBansmer, Technische Universitat Braunschweig

Catherine Clark, David Orchard, National Research CouncilCanada

Laura E. Steen, Robert Ide, Sierra Lobo Inc.; Judith VanZante, NASA John Glenn Research Center

James MacLeod, National Research Council of Canada;Michael Clarke, Rolls-Royce plc; Doug Marsh, MDS AeroSupport

Christian Mendig, DLR German Aerospace Center

Sara Gonzalez Ruiz, Gertjan Glabeke, Jeroen Vanbeeck, VonKarman Institute for Fluid Dynamics

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

10:30Session Time:

Thursday, June 25

Aircraft In-flight Icing - New Icing Test Facilities, Advanced Icing Test Capabilities, and anIcing Facility Capability Update (Part 3 of 4)

Aircraft In-flight Icing - New Icing Test Facilities, Advanced Icing Test Capabilities, and anIcing Facility Capability Update (Part 4 of 4)

Session Code:

Session Code:

ICE118

ICE118



This session includes a report on ice shape mapping by means of 4D scans, an experimental study of effects of high water content on icing tunnel airdata parameters, and an application of an high speed imaging probe in the calibration of NRC-AIWT glaciated and mixed phase cloud.

This session includes reports on an assessment of the SEA multi-element sensor for LWC calibration of the NASA Icing Research Tunnel (IRT), thedevelopment of mixed phase and glaciated environments within the NRC AIWT, the calibration of the IWT Braunschweig for mixed phase andglaciated icing conditions, and a new high-speed insert for the NRC AIWT.



Organizers -

Organizers -

Sam Lee, Vantage Partners Limited; Pierre Trontin, ONERA

Sam Lee, Vantage Partners Limited; Pierre Trontin, ONERA

Chairpersons -

Chairpersons -

1:30 p.m.

2:00 p.m.

3:30 p.m.

4:00 p.m.

2015-01-2151

ORAL ONLY

ORAL ONLY

2015-01-2135

Ice Shape Mapping by Means of 4D-Scans

Application of High Speed Imaging (HSI) Probe in theCharacterization of NRC-AIWT Glaciated and Mixed-Phase Clouds

Ice Adhesion Strength Modeling Based on Surface MorphologyVariations

Evaluation of Different Ice Adhesion Tests for Mechanical DeicingSystems


Reinhard F.A. Puffing, Wolfgang Hassler, Andreas Tramposch,FH JOANNEUM GmbH Graz; Marian Peciar, Slovak Universityof Technology

Biagio M. Esposito, CIRA Scpa; Alexei V. Korolev,Environment Canada; William D. Bachalo, ArtiumTechnologies Inc.

Taylor Knuth, Jose Palacios, Penn State Univ-University Park;Richard Kreeger, NASA John Glenn Research Center; FrankPalmieri, Joseph Smith, Christopher Wohl, NASA LangleyResearch Center

Martin Schulz, Michael Sinapius, Technische UniversitätBraunschweig

Time

Time

Paper No.

Paper No.

Title

Title

13:30

15:30

Session Time:

Session Time:

Thursday, June 25

Thursday, June 25

Environmental Icing Meteorology and Instruments - HAIC/HIWC Instruments and TunnelTests (Part 1 of 2)

Environmental Icing Meteorology and Instruments - HAIC/HIWC Instruments and TunnelTests (Part 2 of 2)

Session Code:

Session Code:

ICE307

ICE307

Room Congress Hall

Room Congress Hall

This session describes the development of new HAIC/HIWC instrumentation and testing of these instruments in wind tunnels.

This session describes the development of new HAIC/HIWC instrumentation and testing of these instruments in wind tunnels.



Organizers -

Organizers -

Biagio M. Esposito, CIRA Scpa; Francois LaRue, Zodiac Aerospace

Darren Glenn Jackson, UTC Aerospace Systems; Peter M. Struk, NASA GlennResearch Center

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

ORAL ONLY

ORAL ONLY

2015-01-2125

A Method to Interpret Mixed-Phase Measurements using the SEAMulti-Wire Probe in Select Icing Test Facilities

Isokinetic TWC Evaporator Probe Development and PerformanceTesting for the HAIC-HIWC Darwin 2014 Field Campaign

Technique for Ice Crystal Particle Size Measurements and Results forthe National Research Council of Canada Altitude Ice Crystal TestSystem



Peter Struk, NASA John Glenn Research Center; TadasBartkus, Jen-Ching Tsao, Ohio Aerospace Institute

Lyle Lilie, Science Engineering Associates Inc.; J. WalterStrapp, Met Analytics, Inc.; Thomas Ratvasky, NASA JohnGlenn Research Center; Craig Davison, National ResearchCouncil Canada

Dan Fuleki, Jennifer L.Y. Chalmers, Brian Galeote, NationalResearch Council Canada

Time

Time

Paper No.

Paper No.

Title

Title

08:30

10:30

Session Time:

Session Time:

Thursday, June 25

Thursday, June 25

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Revisions to IcingStandards

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Ice Crystal TestFacilities

Session Code:

Session Code:

ICE402

ICE404

Room Congress Hall

This session includes presentations on the development of new icing standards.


Organizers -

Jim R. Hoppins, Textron Aviation; Jen-Ching Tsao, Ohio Aerospace InstituteChairpersons -

10:30 a.m.

11:00 a.m.

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2015-01-2134

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

Development and Application of an Impedance-Based Instrument forMeasuring the Liquid Fraction and Thickness of Ice CrystalAccretions

Instrumentation Evaluation and Selection to Support Wind TunnelCalibrations with Respect to Changes on 14 CFR part 33 AppendixD/P Regulation within the HAIC Project

Wind Tunnel Investigations on Size and Concentration Measurementsof Ice Crystals and Measurements of Phase Composition of CloudsUsing the Newly Developed HSI Probe

EUROCAE Working Group 95: Changes to Ice Detector Requirements

EUROCAE Working Group 89: Changes to Pitot and Pitot-staticProbe Requirements

Effects of High Water Content on Icing Tunnel Air Data Parameters



Tom Currie, Dan Fuleki, National Research Council Canada

Biagio M. Esposito, CIRA Scpa; David Hammond, CranfieldUniv.; William Bachalo, Artium Technologies Inc.; HugoPervier, Cranfield Univ.

William Bachalo, Artium Technologies Inc.; Biagio M. Esposito,CIRA Scpa; J. Walter Strapp, Met Analytics; Alexei Korolev,Environment Canada

Vince LoPresto, United Technologies Aerospace; FrancoisLaRue, Zodiac Aerospace

Vince LoPresto, United Technologies Aerospace; RichardLewis, Airbus

Brian Matheis, Mac Whalen, UTC Aerospace Systems


13:30Session Time:

Thursday, June 25

Icing Regulations, Ice Crystals, and Supercooled Large Drops (SLD) - Ice Crystal Modeling(Part 3 of 5)Session Code: ICE408

Room Congress Hall

Room Gallery

This session includes presentations on recent ice crystal engine tests and the facilities for these tests.




Organizers -

Organizers -

Ashlie B. Flegel, Queito P. Thomas, NASA Glenn Research Center

Gerard Duprat, Airbus; James MacLeod

Chairpersons -

Chairpersons -

3:30 p.m.

4:00 p.m.

4:30 p.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

ORAL ONLY

2015-01-2154

ORAL ONLY

2015-01-2140

2015-01-2139

2015-01-2138

Development of the UTC Aerospace Systems Advanced Icing WindTunnel

Improvement of an Altitude Test Facility Capability in Glaciated IcingConditions at DGA Aero-engine Testing

Development of Mixed Phase and Ice Crystal Environments within theNRC Altitude Icing Wind Tunnel

Modeling of Particle Impingement in Presence of Ice Crystals

Computational Method for Ice Crystal Trajectories in a TurbofanCompressor

Modelling of Non-Spherical Particle Evolution for Ice CrystalsSimulation with an Eulerian Approach


Brian Matheis, Don Weber, Mac Whalen, UTC AerospaceSystems

Franck Hervy, Severine Maguis, François Virion, DGA EssaisPropulseurs; Biagio Esposito, CIRA Scpa; Hugo Pervier,Cranfield Univ.

David M. Orchard, Catherine Clark, Myron Oleskiw, NationalResearch Council Canada

Emiliano Iuliano, CIRA Scpa

E.J. Grift, Delft University of Technology; E. Norde, E.T.A. Vander Weide, H.W.M. Hoeijmakers, University of Twente

E. Iuliano, CIRA Scpa; E. Montreuil, ONERA; E. Norde, E.T.A.Van der Weide, H.W.M. Hoeijmakers, University of Twente

Time

Time

Paper No.

Paper No.

Title

Title

15:30

08:30

Session Time:

Session Time:

Thursday, June 25

Thursday, June 25



Session Code:

Session Code:

ICE408

ICE408

Room Gallery

Room Gallery





Organizers -

Organizers -

Gerard Duprat, Airbus; James MacLeod

Tobias Hauk, Airbus Group; Serkan Ozgen, Middle East Technical University

Chairpersons -

Chairpersons -

11:00 a.m.

11:30 a.m.

1:30 p.m.

2015-01-2141

2015-01-2155

2015-01-2148

Lagrangian Trajectory Simulation of Rotating Regular Shaped IceParticles

Development of a Coupled Air and Particle Thermal Model for EngineIcing Test Facilities

Prediction of Ice Crystal Accretion with TAICE




Markus Widhalm, German Aerospace Center

Tadas P. Bartkus, Ohio Aerospace Institute; Peter Struk,NASA John Glenn Research Center; Jen-Ching Tsao, OhioAerospace Institute

Erdem Ayan, Turkish Aerospace Industries Inc.; SerkanOzgen, Middle East Technical University; Canibek Murat,Erhan Tarhan, Turkish Aerospace Industries Inc.

Time

Time

Paper No.

Paper No.

Title

Title

10:30

13:30

Session Time:

Session Time:

Thursday, June 25

Thursday, June 25

Aircraft Inflight Icing - IPS Design & Advanced Technologies

Aircraft Inflight Icing - Hybrid IPS & Application

Session Code:

Session Code:

ICE115

ICE116

Room Libuse

Room Libuse

This session includes a study on the development of a fluid based IPS for UAV/UAS applications, a report on the development of a jet pump IPS forthe A400M transporter, and an evaluation study of different ice adhesion tests for new mechanical deicing systems design.

This session includes a status report on initial results from a hybrid electro thermal/mechanical simulation tool, the development of an ultra-sensitivephotonic ice sensors for inflight IPS - JEDI ACE project, and a 3D CFD comparison of two nacelle IPS.


Gene Addy, NASA John Glenn Research Center; Philip J. Alldridge, SikorskyAircraft Corp.; Ben C. Bernstein, Leading Edge Atmospherics; Gerard Duprat,

Organizers -

Organizers -

Gene Addy, NASA John Glenn Research Center; Leslie McVey, GE AviationChairpersons -

2:00 p.m.

2:30 p.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

2015-01-2146

2015-01-2147

ORAL ONLY

2015-01-2136

ORAL ONLY

Ice Crystal Ingestion in a Turbofan Engine

Improvements of the PLANET System for Real-Time Satellite DataTransmission During the HAIC-HIWC Darwin Field Campaign

The Development of Fluid Based Ice Protection Systems for use inUAV Applications

Innovative Jet Pump Ice Protection System for A400M

Development and Testing of In-Flight Ice Protection Systems basedon Semi Conductive Coatings




Matthew Feulner, Shengfang Liao, Becky Rose, Xuejun Liu,Pratt & Whitney

Sandra Turner, Jean-Marc Gaubert, Remy Gallois, ThibaultDacla, Ingrid Mullie, ATMOSPHERE, Systèmes & Services;Aurelien Bourdon, SAFIRE (CNRS/Météo-France/CNES);Fabien Dezitter, Alice Grandin, Airbus; Alain Protat, RodneyPotts, Bureau of Meteorology R&D; Alfons Schwarzenboeck,LaMP - CNRS/UBP; J. Walter Strapp, Met Analytics

Alexander John Baty, CAV Aerospace, Ltd.

Francisco José Redondo, Airbus

Markus Villinger, Villinger R&D


08:30

10:30

Session Time:

Session Time:

Thursday, June 25

Aircraft Inflight Icing - Low Surface Energy Coating (Part 1 of 2)Session Code: ICE117

Room Libuse

This session includes a review of icephobic coatings performance, the development of ice-relaese silicone film adhesives, a JAEA progress summaryon the development and evaluation of icephobic coatings - the JEDI ACE project, and the development of a new IPS for aircraft integrated with anti-icing coating - the JEDI ACE project.

Airbus; Robert J. Flemming; Richard Lewis, Airbus; Michael James Oliver; Jen-Ching Tsao, Ohio Aerospace Institute


Organizers -

Gene Addy, NASA John Glenn Research Center; Leslie McVey, GE Aviation

Richard E. Kreeger, NASA John Glenn Research Center; Jose Palacios, PennState University

Chairpersons -

Chairpersons -

10:30 a.m.

11:00 a.m.

11:30 a.m.

1:30 p.m.

2:00 p.m.

2015-01-2142

ORAL ONLY

ORAL ONLY

2015-01-2149

2015-01-2150

Initial Results from a Hybrid Electro-Thermal Electro-MechanicalSimulation Tool (HETEMS)

Ultra-sensitive Photonic Flush-mounted Real-time Sensors for In-flight Ice Protection Systems

3D CFD Comparison of Two Nacelle Ice Protection Systems

A Review of Icephobic Coating Performances over the Last Decade

Development and Evaluation of Icephobic Coatings ¿ ProgressSummary of Japan Aerospace Exploration Agency within the JEDI-ACE Project


Colin Hatch, Roger Gent, Richard Moser, AeroTex UK

Airan Rodenas, Javier Martínez, Magdalena Aguiló, FrancescDiaz, Universitat Rovira i Virgili; Miquel Traveria, CESDA;Shigeo Kimura, Kanawaga Institute of Technology; TaroTanaka, Fuji Heavy Industries Ltd; Benoit Berton, DassaultAviation SA; Gerhard Pauly, Nadine Rehfeld, Fraunhofer IFAM

Aleksei P. Paduchev, AVIADVIGATEL; Guido Baruzzi, WagdiHabashi, Newmerical Technologies Inc.

Caroline Laforte, Caroline Blackburn, Jean Perron, Anti-IcingMaterials Intl. Laboratory

Katsuaki Morita, Hirotaka Sakaue, Japan AerospaceExploration Agency; Taro Tanaka, Takeshi Yoshida, FujiHeavy Industries Ltd; Nadine Rehfeld, Andreas Brinkmann,Katrin Lummer, Gerhard Pauly, Fraunhofer IFAM

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

13:30Session Time:

Thursday, June 25

Thursday, June 25

Aircraft Inflight Icing - Low Surface Energy Coating (Part 2 of 2)

Environmental Icing Meteorology and Instruments - Icing Products and Data Inputs

Session Code:

Session Code:

ICE117

ICE301

Room Libuse

This session includes a wind tunnel study of water runback on hydrophobic/hydrophilic surfaces of a cylinder, a numerical study of dynamic effects ofsurface wettability on wind-driven drops, an experimental study of ice adhesion strength of superhydrophobic coatings from highspeed drop impact, astudy on effects prolonged ultraviolet and water exposure on superhydrophobic surfaces at icing conditions, and the development of asuperhydrophobic and icephobic films for efficient deicing.


Organizers -

Richard E. Kreeger, NASA John Glenn Research Center; Jose Palacios, PennState University

Chairpersons -

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

ORAL ONLY

2015-01-2159

2015-01-2158

2015-01-2157

Development of Innovative Ice Protection System of AircraftIntegrating the Anti-icing Coating

Energy Efficient De-Icing by Superhydrophobic and IcephobicPolyurethane Films Created by Microstructuringand Plasma-Coating

Runback Water Behavior on Hydro-phobic/philic Surfaces of CircularCylinder Placed in Flow Field

Dynamic Effects of Surface Wettability on Wind Driven Droplet




Taro Tanaka, Fuji Heavy Industries, Ltd.; Katsuaki Morita,Hirotaka Sakaue, Japan Aerospace Exploration Agency;Shigeo Kimura, Kanazawa Institute of Technology; NadineRehfeld, Fraunhofer IFAM; Benoit Berton, Dassault AviationSA; Francesc Diaz, Universitat Rovira I Virgili

Philipp Grimmer, Swarupini Ganesan, University of Stuttgart;Michael Haupt, Jakob Barz, Christian Oehr, Fraunhofer IGB;Thomas Hirth, University of Stuttgart

Tatsuma Hyugaji, Shigeo Kimura, Haruka Endo, MitsuguHasegawa, Kanagawa Institute of Technology; HirotakaSakaue, Katsuaki Morita, Japan Aerospace ExplorationAgency; Yoichi Yamagishi, Kanagawa Institute of Technology;Nadine Rehfeld, Fraunhofer IFAM; Benoit Berton, DassaultAviation; Francesc Diaz, Universitat Rovira I Virgili; TarouTanaka, Fuji Heavy Industries Ltd.

Mengyao Leng, Shinan Chang, Yuanyuan Zhao, Beijing Univ.of Aeronautics & Astronautics


15:30Session Time:

Thursday, June 25

Thursday, June 25

Environmental Icing Meteorology and Instruments - Icing Observations, Products andVerification

Environmental Icing Meteorology and Instruments - Remote Sensing of Icing/SLDConditions Aloft

Session Code:

Session Code:

ICE302

ICE303

Room Neklan/Vlasta

Room Neklan/Vlasta

This session describes recent developments in the diagnosis and forecasting of icing conditions aloft.

This session will discuss icing observations and their use for validation and verification of icing products.



Organizers -

Organizers -

Ben C. Bernstein, Leading Edge Atmospherics; Frank Kalinka, DeutscherWetterdienst

Daniel R. Adriaansen, National Center for Atmospheric Research; Katharina Roloff

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

ORAL ONLY

2015-01-2137

ORAL ONLY

ORAL ONLY

ORAL ONLY

Diagnosing Aircraft Icing Potential from Satellite Cloud Retrievals

Advancements in Combining Datasets for In-Flight Icing Diagnoses

Global Forecasts of Aircraft Inflight Icing Conditions with ADWICE

Use of In-flight Measurement Data Base for Icing Tool Verification

Two Different Scenarios of Icing Conditions During the Winter of 2015in France



William Smith, Patrick Minnis, NASA Langley ResearchCenter; Cecilia Fleeger, Douglas Spangenberg, ScienceSystems and Applications Inc.

Daniel R. Adriaansen, Paul Prestopnik, George McCabe,Marcia Politovich, National Center for Atmospheric Research

Frank Kalinka, Deutscher Wetterdienst

Christine LeBot, Olivier Jaron, Meteo-France

Olivier Jaron, Christine LeBot, Meteo-France

Time

Time

Paper No.

Paper No.

Title

Title

08:30

10:30

Session Time:

Session Time:

Thursday, June 25

Aircraft Inflight Icing - Icing CFD (Part 2 of 2)Session Code: ICE111

Room Neklan/Vlasta

Room Neklan/Vlasta

This session examines the use of ground-based remote sensing systems for inflight icing, including supercooled large drop (SLD) icing.

This session includes an ice accretion prediction on engine nacelles in both liquid and solid phase, a bpoundary layer transition effect model study forice protected airfoils, an icing modeling with Level-Set approach, and a multi-step icing calculations using the latest NSMB3D-ICE icing code.



Organizers -

Organizers -

Stephanie DiVito, Federal Aviation Administration; Olivier Jaron, Meteo-France

Yongsheng Lian, Univ. of Louisville; Mario Vargas, NASA Glenn Research Center

Chairpersons -

Chairpersons -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

2015-01-2152

2015-01-2153

ORAL ONLY

2015-01-2162

2015-01-2163

Aircraft In Situ Validation of Hydrometeors and Icing ConditionsInferred by Ground-based NEXRAD Polarimetric Radar

Initial Results from Radiometer and Polarimetric Radar-based IcingAlgorithms Compared to In-situ Data

Preliminary Findings of Inflight Icing Field Test to support IcingRemote Sensing Technology Assessment

Progress towards a 3D Numerical Simulation of Ice Accretion on aSwept Wing using the Morphogenetic Approach

CFD and Boundary Layer Models with Laminar-Turbulent Transitionaround Airfoils and a Rough Cylinder: Results Validation


Earle Williams, Michael F. Donovan, David J. Smalley, RobertG. Hallowell, Elaine P. Griffin, Kenta T. Hood, Betty J. Bennett,Massachusetts Institute of Technology; Mengistu Wolde,National Research Council of Canada; Alexei V. Korolev,Environment Canada

David Serke, NCAR; Michael King, Andrew Reehorst, NASAJohn Glenn Research Center

Michael King, Andrew Reehorst, NASA John Glenn ResearchCenter; David Serke, NCAR

Krzysztof Szilder, National Research Council Canada; EdwardLozowski, University of Alberta

Caio Fuzaro Rafael, Federal University of ABC; Diogo MendesPio, Guilherme A. Lima da Silva, ATS4i Aerothermal Solutionsfor Industry

Time

Time

Paper No.

Paper No.

Title

Title

13:30

15:30

Session Time:

Session Time:

4:30 p.m. 2015-01-2161 Multi-time Step Icing Calculations Using a 3D Multi-block StructuredMesh Generation Procedure



Kazem Hasanzadeh, Ecole Polytechnique Montreal; DorianPena, Yannick Hoarau, Strasbourg University; EricLaurendeau, Ecole Polytechnique Montreal

SAE 2015 International Conference on Icing of Aircraft ... · the challenges involved in compliance...

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