Free-flight investigation of jet effect on the low-lift drag and longitudinal trim of a supersonic interceptor-type airplane configuration with an overhanging tail boom at Mach numbers from 1.09 to 1.34

Author:	Blanchard, Willard S., Jr.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57G11
Link:	https://digital.library.unt.edu/ark:/67531/metadc63606/