Structural Design of an Active Trailing-Edge Flap Blade for Helicopter Vibration Control
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Structural Design of an Active Trailing-Edge Flap Blade for Helicopter Vibration Control
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