Computational and Experimental Investigation of A 2-D Scramjet Inlet at Mach Numbers From 10 to 25
5th International conference, Aerospace planes and hypersonics technologies ; 1993 ; Munich; Germany
1993-01-01
AIAA-93-5043
Separate paper nos AIAA-93-5000 to AIAA-93-5169 with gaps
Conference paper
English
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