Torsional vibration analysis for a helicopter tail drive system

被引:0
|
作者
Xu, Zhao-Tang [1 ]
Zhu, Ru-Peng [1 ]
机构
[1] College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2007年 / 28卷 / 02期
关键词
Helicopters;
D O I
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中图分类号
学科分类号
摘要
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页码:425 / 431
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