To simulate high heating rates encountered in hypersonic flow, exhaust gases from rocket are used to power supersonic tunnel producing gas temperature of 4500 R; calibration pressure data indicate reproducibility of test conditions; physical, transport, and 1-dimensional aerodynamic data for combustion products of ammonia and oxygen included.
Mach 4 rocket-powered supersonic tunnel using ammonia-oxygen as working fluid
NACA -- Tech Note
1958
53 pages
Article (Journal)
English
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Jet-powered car reaches Mach 0.94 - Goal is first supersonic auto
Online Contents | 1997