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扑翼飞行的绕流升力与阻流升力及其估算

王孝义 董银萍 邱支振 汪辉兴 陈富强

王孝义, 董银萍, 邱支振, 汪辉兴, 陈富强. 扑翼飞行的绕流升力与阻流升力及其估算[J]. 机械科学与技术, 2017, 36(7): 1136-1142. doi: 10.13433/j.cnki.1003-8728.2017.0725
引用本文: 王孝义, 董银萍, 邱支振, 汪辉兴, 陈富强. 扑翼飞行的绕流升力与阻流升力及其估算[J]. 机械科学与技术, 2017, 36(7): 1136-1142. doi: 10.13433/j.cnki.1003-8728.2017.0725
Wang Xiaoyi, Dong Yinping, Qiu Zhizhen, Wang Huixing, Chen Fuqiang. Lift Estimation of Flow around Wing and Flow Dragging Wing in Flapping Wing Flight[J]. Mechanical Science and Technology for Aerospace Engineering, 2017, 36(7): 1136-1142. doi: 10.13433/j.cnki.1003-8728.2017.0725
Citation: Wang Xiaoyi, Dong Yinping, Qiu Zhizhen, Wang Huixing, Chen Fuqiang. Lift Estimation of Flow around Wing and Flow Dragging Wing in Flapping Wing Flight[J]. Mechanical Science and Technology for Aerospace Engineering, 2017, 36(7): 1136-1142. doi: 10.13433/j.cnki.1003-8728.2017.0725

扑翼飞行的绕流升力与阻流升力及其估算

doi: 10.13433/j.cnki.1003-8728.2017.0725
基金项目: 

国家自然科学基金项目(51375014)资助

详细信息
    作者简介:

    王孝义(1970-),教授,博士,研究方向为仿生机械、数字化设计与制造,wangxy@ahut.edu.cn

Lift Estimation of Flow around Wing and Flow Dragging Wing in Flapping Wing Flight

  • 摘要: 针对扑翼飞行比固定翼飞行气动特性更为复杂、升力计算更加困难问题,从绕流物体的基本气动特性出发,将飞行升力分成绕流升力与阻流升力。分析了扑翼飞行模式下绕流升力与阻流升力作用特点,解释了动物飞行中绕流升力与阻流升力的变化规律。在此基础上,建立了扑翼飞行运动模型,推导出扑翼最大绕流升力与阻流升力理论估算模型。实验算例表明,分类升力估算方法是可行的,绕流升力与阻流升力占比与扑翼实际飞行规律趋势一致。
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出版历程
  • 收稿日期:  2016-01-28
  • 刊出日期:  2017-07-05

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