The Effects of an Inverse-Taper Leading-Edge Flap on the Aerodynamic Characteristics in Pitch of a Wing-Body Combination Having an Aspect Ratio of 3 to 45 Degrees of Sweepback at Mach Numbers to 0.92

Author:	Demele, Fred A.
Year:	1958
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4366
Link:	https://digital.library.unt.edu/ark:/67531/metadc57450/