Stabilization of Helicopter Blades with Severed Pitch Links Using Trailing-Edge Flaps

by Roberto Celi

Published in Journal of Guidance Control and Dynamics by American Institute of Aeronautics and Astronautics (AIAA).

2003 Volume 26, p585-592

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Year 2003
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DOI 10.2514/2.5086

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ISSN-L: 0731-5090

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Stabilization of Helicopter Blades with Severed Pitch Links Using Trailing-Edge Flaps release_agm3m2dynbejlo6cohfgtdzq4q