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