A predictive controller for the Mach number in a transonic wind tunnel

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Transcript of A predictive controller for the Mach number in a transonic wind tunnel

Page 1: A predictive controller for the Mach number in a transonic wind tunnel
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AD-754-098, Body Aerodynamics at Subsonic, Transonic & Supersonic Mach Numbers, Moore, 1972

AD-754-098, Body Aerodynamics at Subsonic, Transonic & Supersonic Mach Numbers, Moore, 1972

A Comparison of the Measured and Computed Skin Friction Distribution on ...€¦ · the National Transonic Facility at NASA Langley and in the 11 Ft Transonic Wind Tunnel at NASA

A Comparison of the Measured and Computed Skin Friction Distribution on ...€¦ · the National Transonic Facility at NASA Langley and in the 11 Ft Transonic Wind Tunnel at NASA

Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds

Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds

Calibration of the 11-By 11-Foot Transonic Wind Tunnel at ...

Calibration of the 11-By 11-Foot Transonic Wind Tunnel at ...

DESIGN AND CONSTRUCTION OF A MACH 2 WIND TUNNEL FOR …

DESIGN AND CONSTRUCTION OF A MACH 2 WIND TUNNEL FOR …

Conversion of Purdue’s Mach-4 Ludwieg Tube to a Transonic ...aae520/wilhelm-transonic-finalrpt-dec04.pdf · Conversion of Purdue’s Mach-4 Ludwieg Tube to a Transonic Educational

Conversion of Purdue’s Mach-4 Ludwieg Tube to a Transonic ...aae520/wilhelm-transonic-finalrpt-dec04.pdf · Conversion of Purdue’s Mach-4 Ludwieg Tube to a Transonic Educational

A Shock Tube Driven Transonic Wind Tunnel...A Shock Tube Driven Transonic Wind Tunnel R&D Journal of the South African Institution of Mechanical Engineering 2013, 29, 1-10

A Shock Tube Driven Transonic Wind Tunnel...A Shock Tube Driven Transonic Wind Tunnel R&D Journal of the South African Institution of Mechanical Engineering 2013, 29, 1-10

The Design and Construction of a 20” x 20” Mach 2.0 Blowdown Wind Tunnel … · 2020. 9. 28. · The Design and Construction of a 20” x 20” Mach 2.0 Blowdown Wind Tunnel to

The Design and Construction of a 20” x 20” Mach 2.0 Blowdown Wind Tunnel … · 2020. 9. 28. · The Design and Construction of a 20” x 20” Mach 2.0 Blowdown Wind Tunnel to

Wind Tunnel Testing Guide - NASA...2019/03/20  · Speed Schlieren, BOS, PLIF, Oil Flow 31-Inch Mach 10 Air Tunnel Mach 10 NASA LaRC 0.5 to 2.2 x 106 per ft 31” H x 31” W 150 to

Wind Tunnel Testing Guide - NASA...2019/03/20  · Speed Schlieren, BOS, PLIF, Oil Flow 31-Inch Mach 10 Air Tunnel Mach 10 NASA LaRC 0.5 to 2.2 x 106 per ft 31” H x 31” W 150 to

AEROELASTICITY OF A LAMINAR WING · 2.4 Wind tunnel The tests were performed in the Transonic Wind Tunnel Goettingen (TWG), operated by the foundation German-Dutch Wind Tunnels (DNW).

AEROELASTICITY OF A LAMINAR WING · 2.4 Wind tunnel The tests were performed in the Transonic Wind Tunnel Goettingen (TWG), operated by the foundation German-Dutch Wind Tunnels (DNW).

USING TRANSONIC SMALL DISTURBANCE THEORY FOR … › ... › 19900010731.pdf · using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel

USING TRANSONIC SMALL DISTURBANCE THEORY FOR … › ... › 19900010731.pdf · using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel

An Investigation of Transonic Resonance in a Mach … · An Investigation of Transonic Resonance in a Mach 2.2 Round Convergent-Divergent Nozzle ... compressible flow solvers, ...

An Investigation of Transonic Resonance in a Mach … · An Investigation of Transonic Resonance in a Mach 2.2 Round Convergent-Divergent Nozzle ... compressible flow solvers, ...

QUASI-ONE-DIMENSIONAL VISCOUS/INVISCID INTERACTING …€¦ · QUASI-ONE-DIMENSIONAL VISCOUS/INVISCID INTERACTING INTERNAL FLOWS AT SUBSONIC, TRANSONIC, AND SUPERSONIC MACH NUMBERS

QUASI-ONE-DIMENSIONAL VISCOUS/INVISCID INTERACTING …€¦ · QUASI-ONE-DIMENSIONAL VISCOUS/INVISCID INTERACTING INTERNAL FLOWS AT SUBSONIC, TRANSONIC, AND SUPERSONIC MACH NUMBERS

Development of Flow over Blunt-Nosed Slender Bodies at Transonic … · Development of Flow over Blunt-Nosed Slender Bodies at Transonic Mach Numbers ... understanding of complex

Development of Flow over Blunt-Nosed Slender Bodies at Transonic … · Development of Flow over Blunt-Nosed Slender Bodies at Transonic Mach Numbers ... understanding of complex

FINITE ELEMENT ANALYSIS OF A NASA NATIONAL TRANSONIC … · 2013-08-30 · FINITE ELEMENT ANALYSIS OF A NASA NATIONAL TRANSONIC FACILITY WIND TUNNEL BALANCE Michael C. Lindell NASA

FINITE ELEMENT ANALYSIS OF A NASA NATIONAL TRANSONIC … · 2013-08-30 · FINITE ELEMENT ANALYSIS OF A NASA NATIONAL TRANSONIC FACILITY WIND TUNNEL BALANCE Michael C. Lindell NASA

Instability Measurements in the Boeing/AFOSR Mach-6 Quiet ...aae519/BAM6QT-Mach-6-tunnel/tunnel... · Instability Measurements in the Boeing/AFOSR Mach-6 ... The Rotating cone has

Instability Measurements in the Boeing/AFOSR Mach-6 Quiet ...aae519/BAM6QT-Mach-6-tunnel/tunnel... · Instability Measurements in the Boeing/AFOSR Mach-6 ... The Rotating cone has

João Batista P. Falcão Filho* Historical review and future ... · Historical review and future perspectives for Pilot Transonic Wind Tunnel of IAE Abstract: The Pilot Transonic

João Batista P. Falcão Filho* Historical review and future ... · Historical review and future perspectives for Pilot Transonic Wind Tunnel of IAE Abstract: The Pilot Transonic

This document is provided by JAXA. · (2) Transonic wind tunnel (2m x 2m), (3) Supersonic wind tunnel (1m x 1m) and(4) Hypersonic wind tunnel (0. 5m. Φ and 1.25mΦ). Figure 4 shows

This document is provided by JAXA. · (2) Transonic wind tunnel (2m x 2m), (3) Supersonic wind tunnel (1m x 1m) and(4) Hypersonic wind tunnel (0. 5m. Φ and 1.25mΦ). Figure 4 shows

Transonic Dynamics Tunnel Aeroelastic Testing in Support ... · PDF fileJOURNALOFAIRCRAFT Vol. 40, No. 5, September– October 2003 Transonic Dynamics Tunnel Aeroelastic Testing in

Transonic Dynamics Tunnel Aeroelastic Testing in Support ... · PDF fileJOURNALOFAIRCRAFT Vol. 40, No. 5, September– October 2003 Transonic Dynamics Tunnel Aeroelastic Testing in

CFD Investigation of the Transonic Flow- field for a ... · supersonic Mach number range. The wind tunnel is not a suitable experimental tool as this will generate accelerated section.

CFD Investigation of the Transonic Flow- field for a ... · supersonic Mach number range. The wind tunnel is not a suitable experimental tool as this will generate accelerated section.