Analysis of helicopter vibratory hub loads alleviation by cyclic trailing-edge blade flap actuation
The aeronautical journal ; 113 , 1146
2009
Article (Journal)
Unknown
Flexbeam hinge for helicopter blade active trailing edge flap
European Patent Office | 2016
|ALLEVIATION OF ROTOR BLADE DYNAMIC STALL VIA TRAILING EDGE FLAP FLOW CONTROL
British Library Conference Proceedings | 2003
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