班学, 何国毅, 张波. 蜻蜓褶皱翼气动效能数值研究[J]. 南昌航空大学学报(自然科学版), 2014, 28(2): 70-73,79. DOI: 10.3969/j.issn.1001-4926.2014.02.012
引用本文: 班学, 何国毅, 张波. 蜻蜓褶皱翼气动效能数值研究[J]. 南昌航空大学学报(自然科学版), 2014, 28(2): 70-73,79. DOI: 10.3969/j.issn.1001-4926.2014.02.012
ZHANG Bin-bin, HU Shui-lian, FENG Chang-jie. Numerical Study of the Aerodynamic Performance of the Dragonfly Wing Sections in Gliding flight[J]. Journal of nanchang hangkong university(Natural science edition), 2014, 28(2): 70-73,79. DOI: 10.3969/j.issn.1001-4926.2014.02.012
Citation: ZHANG Bin-bin, HU Shui-lian, FENG Chang-jie. Numerical Study of the Aerodynamic Performance of the Dragonfly Wing Sections in Gliding flight[J]. Journal of nanchang hangkong university(Natural science edition), 2014, 28(2): 70-73,79. DOI: 10.3969/j.issn.1001-4926.2014.02.012

蜻蜓褶皱翼气动效能数值研究

Numerical Study of the Aerodynamic Performance of the Dragonfly Wing Sections in Gliding flight

  • 摘要: 蜻蜓具有优异的飞行技能,这与它的翅膀结构密切相关。通过利用数值模拟方法研究了蜻蜓前翅沿展向5个截面翼型位置气动力和流场结构后,发现:在滑翔时,蜻蜓翅膀沿展向翅根处的翼型会产生正升力,且沿展向逐渐减小,在翅尖处翼型会产生小的负升力,使翅膀延展向不发生翘曲变形;且由于翅膀皱褶处驻留涡的作用,具有较大的失速迎角,这都保证了蜻蜓飞行的稳定性。

     

    Abstract: Dragonfly is considered a high performance flyer in nature because of its wing structures. A computational fluid-dynamics-based study of a pleated wing section has been performed at low Reynolds numbers corresponding to the gliding flight of the dragonfly. The simulations demonstrate that the pleated wing produces high lift at wing roots, along the spanwise of the wing sections, the lift decreased gradually, until it becomes a small negative value at the wing tips, the phenomenon make the wing not bend along spanwise. In the cavities of the pleated wing, the resident vortexes make the wing have large stall angle. These ensure the stability of the dragonfly gliding flight.

     

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