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三维仿生悬停扑翼的时间非对称扑动气动特性

朱建阳 蒋林 雷斌

朱建阳, 蒋林, 雷斌. 三维仿生悬停扑翼的时间非对称扑动气动特性[J]. 航空动力学报, 2017, 32(4): 858-864. doi: 10.13224/j.cnki.jasp.2017.04.0010
引用本文: 朱建阳, 蒋林, 雷斌. 三维仿生悬停扑翼的时间非对称扑动气动特性[J]. 航空动力学报, 2017, 32(4): 858-864. doi: 10.13224/j.cnki.jasp.2017.04.0010
Aerodynamic performance of time asymmetric flapping of a three-dimensional flapping hovering bionic wing[J]. Journal of Aerospace Power, 2017, 32(4): 858-864. doi: 10.13224/j.cnki.jasp.2017.04.0010
Citation: Aerodynamic performance of time asymmetric flapping of a three-dimensional flapping hovering bionic wing[J]. Journal of Aerospace Power, 2017, 32(4): 858-864. doi: 10.13224/j.cnki.jasp.2017.04.0010

三维仿生悬停扑翼的时间非对称扑动气动特性

doi: 10.13224/j.cnki.jasp.2017.04.0010
基金项目: 国家自然科学基金(51505347)

Aerodynamic performance of time asymmetric flapping of a three-dimensional flapping hovering bionic wing

  • 摘要: 基于对现有黄蜂飞行观察实验的分析,建立了不同下扑和上挥时间非对称扑动悬停扑翼运动轨迹模型,并采用数值求解三维层流Navier-Stokes(N-S)方程的方法,研究了采用不同下扑和上挥时间比的仿生悬停扑翼气动特性.结果表明采用适当的时间非对称扑动可以增强悬停扑翼的气动性能.进一步通过对不同时间非对称扑动扑翼流场分析得出,采用时间非对称扑动不但可以增强使扑翼产生高升力的旋转环流机制,而且还可以增强扑翼表面涡流和展向流的强度,从而使扑翼具有更好的气动性能.

     

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出版历程
  • 收稿日期:  2015-09-12
  • 刊出日期:  2017-04-28

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