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Effect of twist and camber on the low-speed aerodynamic characteristics of a powered close-coupled wing-canard configuration

John W. Paulson, Jeffrey L. Thomas

Abstract

A series of wind-tunnel tests were conducted in a V/STOL tunnel to determine the low-speed longitudinal aerodynamic characteristics of a powered close-coupled wing/canard fighter configuration. The data was obtained for a high angle-of-attack maneuvering configuration and a takeoff and landing configuration. The data presented in tabulated form are intended for reference purposes.

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Available abstract

Key concepts: Camber (aerodynamics), Wing, Aerodynamics, Takeoff, Aerospace engineering, Wind tunnel, Angle of attack, Wing configuration