Helicopter / engine coupled system modeling and dynamic response analysis

被引:0
|
作者
Wei, Yuan [1 ]
Chen, Renliang [1 ]
机构
[1] National Key Laboratory of Helicopter Aeromechanics, Nanjing University of Aeronautics and Astronautics), Nanjing,210016, China
来源
Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology | 2024年 / 56卷 / 12期
关键词
D O I
10.11918/202312066
中图分类号
学科分类号
摘要
引用
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页码:1 / 9
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