Effect of yaw and angle of attack pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71

Comenzo, Raymond J Mackley, Ernest A
naca-rm-l54g22
September 10, 1954


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-l54g22.pdf