The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90, by Fred A. Demele et al.

Title:	The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90
Author:	Demele, Fred A.
Author:	Ames Research Center
Note:	National Aeronautics and Space Administration, 1959

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Subject:	Aerodynamic loads
Subject:	Aspect ratio
Subject:	Camber
Subject:	Deflection
Subject:	Leading edge flaps
Subject:	Mach number
Subject:	Pressure effects
Subject:	Sweptback wings
Subject:	Twisting
Subject:	Wind tunnel tests
Subject:	Wing loading
Subject:	Wing profiles
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