Wing-on and wing-off longitudinal characteristics of an airplane configuration having an thin unswept tapered wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4

Author:	Gillis, Clarence L.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50K16
Link:	https://digital.library.unt.edu/ark:/67531/metadc58657/