Aerodynamic characteristics at Mach number of 4.06 of a typical supersonic airplane model using body and vertical-tail wedges to improve directional stability

Author:	Dunning, Robert W
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57I10
Link:	https://digital.library.unt.edu/ark:/67531/metadc63668/