Unsteady-lift functions for wings of finite aspect ratio have been calculated by correcting the aerodynamic inertia and the angle of attack of the infinite wing. The calculations are based on the operational method.
The unsteady lift of a wing of finite aspect ratio
1940-01-01
Miscellaneous
No indication
English
Unsteady lift of wing of finite aspect ratio
Engineering Index Backfile | 1940
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