Vibration and Performance Analyses Using Individual Blade Pitch Controls for Lift-Offset Rotors
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DOI: 10.1155/2019/9589415
Abstract: This work attempts to reduce the hub vibratory loads of a lift-offset rotor using IBC (individual blade pitch control) in high-speed forward flight. As a lift-offset rotor for the present study, the rigid coaxial rotor… read more here.
Keywords: vibration; individual blade; rotor; performance ... See more keywords