Control of helicopter rotor blade dynamic stall and hub vibration loads by multiple trailing edge flaps
Hang kong xue bao ; 34 , 5 ; 1083-1091
2013
Aufsatz (Zeitschrift)
Chinesisch
Helicopter Blade Loads Control via Multiple Trailing-Edge Flaps
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AIAA | 2004
|Swashplateless Helicopter Rotor with Trailing-Edge Flaps
Online Contents | 2004
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|Helicopter Vibration Reduction with Trailing Edge Flaps
British Library Conference Proceedings | 1995
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