Reynolds number and cowl position effects for a generic sidewall compression scramjet inlet at Mach 10 - A computational and experimentalinvestigation
17th Aerospace Ground Testing Conference ; 1992 ; Nashville , TN , U.S.A.
1992-01-01
Conference paper
Electronic Resource
English
Shock tunnel studies on cowl-ramp shock interactions in a generic scramjet inlet
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|Effects of Reynolds Number on Scramjet Inlet Peformance
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