Effects of leading-edge slats on the aerodynamic characteristics of a 45 degree sweepback wing-fuselage configuration at Mach numbers of 0.4 to 1.03

Author:	Runckel, Jack F.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53F23
Link:	https://digital.library.unt.edu/ark:/67531/metadc59785/