Effect of Wing Loading and Altitude on Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Free- Flight Tunnel
1943
23 pages
Report
No indication
English
Aerodynamics , Aeronautics , Wings , Roll , Aircraft , Aerodynamic stability , Free flight , Dynamic loads , Altitude , Control , Wind tunnel tests , Ati-7836 , Ati collection
Engineering Index Backfile | 1943
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