Hypersonic tunnels require solution of problems associated with high stagnation temperatures and pressures and more critical dimensional tolerances; solutions employed by Jet Propulsion Laboratory of Calif Inst Technology are outlined based on both supersonic and hypersonic tunnel design and operational experience. (received Mar 1960)
Design and operation of continuous-flow hypersonic wind tunnel using two-dimensional nozzle
AGARDograph
AGARDograph ; n 38
1959
156 pages
Article (Journal)
English
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Hypersonic wind tunnel nozzle study
AIAA | 1992
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AIAA | 2005
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