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Lift and Pitching Derivatives of Thin Sweptback Tapered Wings with Streamwise Tips and Subsonic Leading Edges at Supersonic Speeds

Frank S Malvestuto, Dorothy M. Hoover

Abstract

Note presenting the lift-due-to-pitching derivative and the damping-in-pitch derivative, which were derived for a series of thin sweptback tapered wings with streamwise tips and subsonic leading edges. The effects of camber and thickness were not considered.

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Key concepts: Supersonic speed, Camber (aerodynamics), Lift (data mining), Swept wing, Angle of attack, Vortex lift, Wing, Mechanics