Free-flight performance of 16-inch-diameter supersonic ram-jet units I : four units designed for combustion-chamber-inlet Mach number of 0.12 at free-stream Mach number of 1.6 (units A-2, A-3, A-4, and A-5)

Carlton, William W Messing, Wesley E
naca-rm-e9f22
September 22, 1949


No Abstract Available

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