Wind-tunnel investigation of the effects of lip geometry on drag and pressure recovery of a normal-shock nose inlet on a body of revolution at Mach numbers of 1.41 and 1.81

Robins, A Warner
naca-rm-l57k08
February 03, 1958


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1958/naca-rm-l57k08.pdf