Hypersonic Wind Tunnels

105 books
The flying wind tunnelR. B. Norris

The flying wind tunnel

R. B. Norris

1989No page data
A summary of design techniques for axisymmetric hypersonic wind tunnelsYing-Nien Yu
⏱ 1h 28m

A summary of design techniques for axisymmetric hypersonic wind tunnels

Ying-Nien Yu

195888 pp.
The development of a hypersonic wind tunnelD. H. Henshaw

The development of a hypersonic wind tunnel

D. H. Henshaw

1950No page data
I.A.I. hypersonic wind tunnelL. Y. Jacobi

I.A.I. hypersonic wind tunnel

L. Y. Jacobi

1987No page data
Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnelsCharles G. Miller
⏱ 1h 30m

Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels

Charles G. Miller

198190 pp.
Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditionsWilliam A. Wood

Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions

William A. Wood

1999No page data
Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnelJale F. Akyurtlu

Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel

Jale F. Akyurtlu

1991No page data
Into the windJ. Lawrence Lee

Into the wind

J. Lawrence Lee

2012No page data
Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulationLawrence D. Huebner
⏱ 46m

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation

Lawrence D. Huebner

199346 pp.
The performance of the VKI Longshot hypersonic wind tunnelG. Simeonides
⏱ 35m

The performance of the VKI Longshot hypersonic wind tunnel

G. Simeonides

198735 pp.
The VKI hypersonic wind tunnels and associated measurement techniquesG. Simeonides

The VKI hypersonic wind tunnels and associated measurement techniques

G. Simeonides

1990No page data
Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flowsRobert L. McKenzie

Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows

Robert L. McKenzie

1992No page data
A System to measure flow moisture content in hypersonic wind tunnelsJames W. West

A System to measure flow moisture content in hypersonic wind tunnels

James W. West

1992No page data
Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnelsGregory M. Buck

Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels

Gregory M. Buck

1995No page data
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6Scott Douglas Holland

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Scott Douglas Holland

1994No page data
Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzleHarris M. Schurmeier
⏱ 2h 36m

Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle

Harris M. Schurmeier

1959156 pp.
A comparison of hypersonic wind tunnel data obtained by static and free oscillation techniquesK. F. Stetson

A comparison of hypersonic wind tunnel data obtained by static and free oscillation techniques

K. F. Stetson

1977No page data
Development of a high accuracy angular measurement system for Langley Research Center hypersonic wind tunnel facilitiesBrett Newman

Development of a high accuracy angular measurement system for Langley Research Center hypersonic wind tunnel facilities

Brett Newman

2003No page data
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6Scott D. Holland

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Scott D. Holland

1994No page data
Air condensation effects measured in the R.A.E. 7 in. x 7 in. hypersonic wind tunnelJohn Frank William Crane
⏱ 38m

Air condensation effects measured in the R.A.E. 7 in. x 7 in. hypersonic wind tunnel

John Frank William Crane

196838 pp.
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