Investigation of Effects of Extreme Structural Flexibility of Flight Vehicles with Feedback Control System Stabilization
1965
142 pages
Report
Keine Angabe
Englisch
Aircraft , Feedback control system , Flexibility , Flight vehicle , Stabilization , Aerodynamics , Body , Canard , Characteristics , Control , Dynamic , Feedback , Flight , Loading , Missile , Slender , Structural , Surface , System , Tail , Vehicle
Experimental Investigation of Wing Flexibility Effects in Flapping Flight
British Library Conference Proceedings | 2008
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