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
1978-05-01
Report
No indication
English