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Effects of a Leading-edge Slat and a Trailing-edge Split Flap on the Aerodynamic Characteristics of a Wing-fuselage Combination Having a Nearly Triangular Wing of Aspect Ratio 2.9 at Mach Numbers from 0.60 to 0.92

Fred A Demele

Abstract

Report presenting an investigation to determine the effectiveness of a leading-edge slat and a trailing-edge split flap in improving the high subsonic speed aerodynamic characteristics of a model of a wing-fuselage combination with a nearly triangular wing. Results regarding the effects of Reynolds number, effects of slats, and effects of flaps are provided.

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Available abstract

Key concepts: Fuselage, Wing, Trailing edge, Aerodynamics, Leading edge, Wing twist, Reynolds number, Wing configuration