Use of nitrous oxide for obtaining high stagnation enthalpies in shock tunnels.
CRAIG, R. R., ORTWERTH, P. J. /USAF, SYSTEMS COMMAND, RESEARCH AND TECHNOLOGY DIV., AERO PROPULSION LAB., RAMJET E
AIAA Journal ; 5 , 12 ; 2271-2274
1967-01-01
4 pages
Article (Journal)
Electronic Resource
English
Hypersonic merged stagnation shock layers
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