Theoretical Investigation of the Effect of the Lateral Oscillations of an Airplane of an Automatic Control Sensitive to Yawing Accelerations
1950
37 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Aerodynamic stability , Acceleration , Yaw , Automatic , Oscillation , Theory , Control , Ati-72333 , Ati collection
Engineering Index Backfile | 1950
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