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Hypersonic wind tunnels
Aerodynamics, Hypersonic 11
Hypersonic planes 5
Hypersonic speed 5
Testing 5
Aerodynamic load 4
Blowdown wind tunnels 4
Design and construction 4
Wind tunnel testing 4
Wind tunnel tests 4
Aerodynamics 3
Cylinders 3
Heat 3
Heat transfer 3
Measurement 3
Pressure 3
Shock tunnels 3
Test facilities 3
Transmission 3
Aerodynamic control surfaces 2
Aerodynamic heating 2
Aerothermodynamics 2
Airplanes 2
Appropriations and expenditures 2
Calibration 2
Computer simulation 2
Condensation 2
Engine tests 2
Flow distribution 2
Gas analysis 2

Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. by Kaufman, Louis G.

Pressure measurement for Mach 8 flows over expansion corners and ramps on an internally cooled model. by Kaufman, Louis G.

A spectrographic analysis of a 1-foot hypersonic-arc-tunnel airstream using an electron beam probe / by Sebacher, Daniel I.

Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / by Hollis, Brian R. (Brian Ray)

Advanced experimental techniques for study of hypervelocity flight; [papers.

Theories and technologies of hypervelocity shock tunnels by Jiang, Z. (Zonglin), Chue, Randy S. M., 1957-

Advances in hypervelocity techniques : proceedings /

Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF₄ Tunnel by Thompson, R. A.

Investigation of pressure distributions over planar, twisted, and cambered wings in a hypersonic wind tunnel / by Hopkins, H. B.

Rapid fabrication of flat plate cavity phosphor thermography test models for shuttle return-to-flight aero-heating

Experimental methods of hypersonics / by Lukasiewicz, J.

Langley 8-ft. HTT Test 139 gas analyses / by Sprinkle, Danny R., Davis, Patricia P.

Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel final report for NAG-1-767 / by Akyurtlu, Jale F.

Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel status report, October 31, 1991 / by Akyurtlu, Jale F.

Aerodynamic characteristics at Mach number 0.2 of a wing-body concept for a hypersonic research airplane / by Dillon, James L.

A preliminary theoretical study of the expansion tube : a new device for producing high-enthalpy short-duration hypersonic gas flows / by Trimpi, Robert L.

An assessment of laser velocimetry in hypersonic flow final report.

Enhancing U.S. competitiveness : NASA hypersonics research and wind tunnel programs : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on S...

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation by Huebner, Lawrence D.

Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31̊ angle of attack and Mach 20 in helium / by Ashby, George C.

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Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. by Kaufman, Louis G.

Pressure measurement for Mach 8 flows over expansion corners and ramps on an internally cooled model. by Kaufman, Louis G.

A spectrographic analysis of a 1-foot hypersonic-arc-tunnel airstream using an electron beam probe / by Sebacher, Daniel I.

Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / by Hollis, Brian R. (Brian Ray)

Advanced experimental techniques for study of hypervelocity flight; [papers.

Theories and technologies of hypervelocity shock tunnels by Jiang, Z. (Zonglin), Chue, Randy S. M., 1957-

Advances in hypervelocity techniques : proceedings /

Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF₄ Tunnel by Thompson, R. A.

Investigation of pressure distributions over planar, twisted, and cambered wings in a hypersonic wind tunnel / by Hopkins, H. B.

Rapid fabrication of flat plate cavity phosphor thermography test models for shuttle return-to-flight aero-heating

Experimental methods of hypersonics / by Lukasiewicz, J.

Langley 8-ft. HTT Test 139 gas analyses / by Sprinkle, Danny R., Davis, Patricia P.

Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel final report for NAG-1-767 / by Akyurtlu, Jale F.

Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel status report, October 31, 1991 / by Akyurtlu, Jale F.

Aerodynamic characteristics at Mach number 0.2 of a wing-body concept for a hypersonic research airplane / by Dillon, James L.

A preliminary theoretical study of the expansion tube : a new device for producing high-enthalpy short-duration hypersonic gas flows / by Trimpi, Robert L.

An assessment of laser velocimetry in hypersonic flow final report.

Enhancing U.S. competitiveness : NASA hypersonics research and wind tunnel programs : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on S...

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation by Huebner, Lawrence D.

Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31̊ angle of attack and Mach 20 in helium / by Ashby, George C.

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