Response calculation method for the rotor blade with arbitrary rigid motions

被引:0
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作者
Wang, Hao-Wen [1 ]
Han, Dong [1 ]
Gao, Zheng [1 ]
机构
[1] National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
关键词
Helicopter rotors;
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页码:46 / 50
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