NASA NACA-RM-E50D05-1950
Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1.8 and 2.9
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NASA NACA-RM-E50D05-1950
Standard No.
NASA NACA-RM-E50D05-1950
Release Date
1950
Published By
National Aeronautics and Space Administration (NASA)
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