Effect of leading-edge chord-extensions on the aerodynamic characteristics of a 45 degree sweptback wing-fuselage combination at Mach numbers of 0.40 to 1.03

Author:	West, F. E., Jr.
Additional Authors:	Martz, Gladys S.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53B02
Link:	https://digital.library.unt.edu/ark:/67531/metadc59557/