Rigidly forced oscillatory dynamic stability method for measuring pitch and yaw damping derivatives in wind tunnels at transonic and supersonic speeds
The significance of nonlinear damping trends determined for current aircraft configurations
1966-09-01
Miscellaneous
No indication
English
Transonic Aircraft Configurations
AIAA | 2012
|CURRENT TRENDS in AIRCRAFT POWER PLANTS
SAE Technical Papers | 1944
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