Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility

Langley 8-ft. HTT test 139 gas analyses

Danny R. Sprinkle

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

Charles G. Miller

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

Lawrence D. Huebner

Aeronautical facilities catalogue

Frank E. Peñaranda

Enhancing U.S. competitiveness

United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation.

Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium

George C. Ashby

A short time response stagnation temperature probe

R. A. East

Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel

S. Venkateswaran

Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms

Nathan S. Jacobson

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

Jale F. Akyurtlu