Lift, drag, and longitudinal stability at Mach numbers from 1.4 to 2.3 of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

Author:	Gillespie, Warren, Jr.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55I12
Link:	https://digital.library.unt.edu/ark:/67531/metadc61589/