Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-Sided Fuselage: Lift, Drag, Longitudinal Stability, Lateral Force, and Jet Effects at Mach Numbers Between 1.0 and 2.3

Author:	Peck, Robert F.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55L29
Link:	https://digital.library.unt.edu/ark:/67531/metadc62413/