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Published in 2018 at "Journal of The American Helicopter Society"
DOI: 10.4050/jahs.63.025001
Abstract: Based on blade element/momentum theory the aerodynamic impact on rotor controls and blade flapping caused by a straight line vortex penetrating orthogonally the plane of a rotor disk is solved using a realistic swirl velocity…
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Keywords:
controls blade;
rotor controls;
rotor;
flapping caused ... See more keywords