Supersonic-area-rule design and rocket-propelled flight investigation of a zero-lift straight-wing-body-nacelle configuration between Mach numbers 0.8 and 1.53

Author:	Hoffman, Sherwood
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56B27
Link:	https://digital.library.unt.edu/ark:/67531/metadc62301/