Response calculation method for the rotor blade with arbitrary rigid motions

被引：0
|
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
来源：
Zhendong Gongcheng Xuebao/Journal of Vibration Engineering | 2006年 / 19卷 / 01期
关键词：
Helicopter rotors;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
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页码：46 / 50
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