Computational and experimental investigation of a 2-D scramjet inlet at Mach numbers from 10 to 25
5th International Aerospace Planes and Hypersonics Technologies Conference ; 1993 ; Munich , Germany
1993-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Computational and Experimental Investigation of A 2-D Scramjet Inlet at Mach Numbers From 10 to 25
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