Efficient method for helicopter rotor transient aerodynamic response

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作者：
National Key Laboratory of Rotorcraft Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China [1 ]
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来源：
Yingyong Lixue Xuebao/Chinese Journal of Applied Mechanics | 2006年 / 23卷 / 01期
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页码：154 / 158
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