Effects of boundary-layer control on the longitudinal characteristics of a 45 degrees swept-forward wing-fuselage combination

Author:	McCormack, Gerald M.
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A9K02a
Link:	https://digital.library.unt.edu/ark:/67531/metadc58338/