Magnetostrictively Actuated Control Flaps Vibration Reduction in Helicopter Rotors - Design Considerations for Implementation
Israel annual conference; 36th, Aerospace sciences ; 1996 ; Tel Aviv; Israel
01.01.1996
12 pages
Also held in Haifa, Israel
Aufsatz (Konferenz)
Englisch
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Optimal Placement of Piezoelectric Actuated Trailing-Edge Flaps for Helicopter Vibration Control
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