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
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effects of Sidewall Compression and Relaminarization in a Scramjet Inlet
Online Contents | 2013
|Effects of Reynolds Number on Scramjet Inlet Peformance
British Library Conference Proceedings | 2002
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