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

Author:	Love, Eugene S.
Additional Authors:	Bromm, August F., Coletti, Donald E.
Year:	1952
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L52H21
Series:	National Advisory Committee for Aeronautics research memorandum ;
Report Number:	L52H21
Subjects:	Reynolds number
	Drag (Aerodynamics)
	Aerodynamics, Supersonic
	Body of revolution
	Base flow (Aerodynamics)
Link:	https://hdl.handle.net/2027/mdp.39015086465062