Calculations based on linearized supersonic flow theory and on additional assumption that Mach cones yaw with wing.
Effect of thickness on lateral force and yawing moment of sideslipping Delta wing at supersonic speeds
Nat Advisory Committee Aeronautics -- Tech Note
1949
24 pages
Report
Englisch
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Engineering Index Backfile | 1950
|Effects of yawing thin pointed wings at supersonic speeds
Engineering Index Backfile | 1947
|