Forces and pitching moments on an aspect-ratio-3.1 wing-body combination at Mach numbers from 2.5 to 3.5 and sublimation studies of the effect of single-elements roughness on the boundary-layer flow

Author:	Hopkins, Edward J.
Additional Authors:	Keating, Stephen J., Jr.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A58E21a
Link:	https://digital.library.unt.edu/ark:/67531/metadc64256/