Combined numerical and experimental investigation of a 2-D scramjet inlet at Mach numbers from 10 to 25
International Aerospace Planes and Hypersonics Technologies ; 1995 ; Chattanooga , TN , U.S.A.
1995-01-01
Conference paper
Electronic Resource
English
Computational and Experimental Investigation of A 2-D Scramjet Inlet at Mach Numbers From 10 to 25
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