Investigation in connection with program to compute stability derivatives of certain specific aircraft and missiles; paper divided into three parts; curved flight path, zero rate of change of sideslip; straight flight path, rate of change of sideslip equals rate of yaw; rate of change of sideslip and yaw.
Dynamic derivatives in yaw and sideslip of thin wings at supersonic speeds
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 23 , n 4 ; p 357-367
1956
11 pages
Article (Journal)
English
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Rolling and yawing moments for swept-back wings in sideslip at supersonic speeds
Engineering Index Backfile | 1951
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