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.
Effect of Twist and Camber on the Low-Speed Aerodynamic Characteristics of a Powered Close-Coupled Wing-Canard Configuration
1978
159 pages
Report
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English