AIAA-2001-1433 Trailing Edge Flap Control Methodology for Vibration Reduction of Helicopter with Dissimilar Blades
42nd, Structures, structural dynamics, and materials conference ; 2001 ; Seattle, WA
01.01.2001
11 pages
Aufsatz (Konferenz)
Englisch
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AIAA-2001-1675 Aeroelastic Stability of Smart Trailing-Edge Flap Helicopter Rotors
British Library Conference Proceedings | 2001
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