The following contains information on the air forces on a wing produced by it's pitching at a finite rate of angular velocity. The condition of smooth flow at the region of the trailing edge is maintained. The wing then experiences the same lift as if moving with the momentary velocity of the rear edge.
Note on the air forces on a wing caused by pitching.
1925-03-01
Sonstige
Keine Angabe
Englisch
Note on the air forces on a wing caused by pitching
SLUB | 1925
|Wing pitching moment coefficient
Engineering Index Backfile | 1945
|Tema Archiv | 1985
|AIAA | 1985
|Wing Pitching Moment Coefficient
Emerald Group Publishing | 1945
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