| 对直升机动力学的现状与发展的分析 |
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| 引用本文： | 杨超,宋寿峰.对直升机动力学的现状与发展的分析[J].北京航空航天大学学报,1995,21(2):46-52. |
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| 作者姓名： | 杨超 宋寿峰 |
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| 作者单位： | 北京航空航天大学飞行器设计与应用力学系 |
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| 摘 要： | 对以旋翼动力学和飞行动力学为主体的直升机动力学研究进展回顾。主要讨论与飞行力学有关的旋翼气动力模型，旋翼结构动力学、气动弹性力学、飞行动力学模型与控制以及飞行操纵与品质等方面的进展，分析它们的现状，供有关直升机研究人员参考。
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| 关 键 词： | 直升机 旋翼 空气动力学 飞行力学 飞行品质 |
THE ANALYSIS ABOUT CURRENT SITUATION AND DEVELOPMENT OF HELICOPTER DYNAMICS |
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| Yang Chao, Song Shoufeng.THE ANALYSIS ABOUT CURRENT SITUATION AND DEVELOPMENT OF HELICOPTER DYNAMICS[J].Journal of Beijing University of Aeronautics and Astronautics,1995,21(2):46-52. |
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| Authors: | Yang Chao Song Shoufeng |
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| Abstract: | The rotor dynamics and flight dynamics, as the main content of helicopter dynamics, are reviewed. It discusses the current situation and development of aerodynamics. structure mechanics. aeroelasticity of rotor. and mathematical model. control, qualities for flight dynamics. It is useful in a certain sense for the research people. |
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| Keywords: | helicopters: rotor aerodynamics: flight mechanics flight quality aeroelastic dynamics |
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