Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel

Love, Eugene S Coletti, Donald E Bromm, August F , Jr
naca-rm-l52h21
October 17, 1952


No Abstract Available

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