基于透气结构的海鸥仿生翼型气动特性

Aerodynamic characteristics of seagull bionic airfoil based on breathable structure

  • 摘要: 羽毛是鸟类飞行的关键部件,是构成鸟翼外形的核心元素,其自身透气特性也是影响鸟翼气动特性的重要因素。本文将羽毛简化为多孔介质,将多孔介质覆盖在海鸥仿生翼型表面来模拟透气结构,应用多孔介质的渗流理论,通过CFD方法探究此仿生结构对翼型气动特性的影响。结果表明:多孔介质对翼型的气动性能有显著影响,从壁面压力分布、摩擦阻力分布以及空间速度分布等方面的影响机制分析来看,在多孔介质作用下,翼型失速迎角增加5°,最大升力系数提高8.2%;多孔介质的几何分布参数对翼型气动特性也有显著影响,随着分布起始点前移,失速迎角增大,翼型线性段的升力系数降低;随着厚度增大,翼型线性段升力系数降低,翼型阻力增加,其中多孔区域阻力显著增大;透气特征参数对翼型气动特性的影响较为显著,随着达西数增大,多孔翼型的升力系数小幅增加,其阻力在小迎角范围内降低,在失速段增加。各向异性对翼型升力影响较小,主要影响翼型阻力,且翼型表面摩擦阻力分布和多孔区域的阻力主要由x方向的渗透率决定。本文半覆盖多孔翼型所采用的分布方式和透气特性及其研究结论可为仿生翼型的设计研究提供一定参考。

     

    Abstract: Feathers, as the key component for avian flight, are the core elements constituting the shape of bird wings, and their breathable characteristics significantly influence the aerodynamic properties of bird wings. In this study, feathers were simplified as a breathable structure on the wing surface, and porous medium was applied to the surface of a seagull bionic airfoil to simulate this breathable structure. By utilizing the seepage theory of porous media and employing the Computational Fluid Dynamics (CFD) method, the impact of this biomimetic structure on the aerodynamic characteristics of the airfoil was investigated. The results indicate that, porous medium has a significant impact on the aerodynamic performance of airfoils, and the influence mechanism is analyzed from aspects such as wall pressure distributions, friction drag distributions, and spatial velocity distributions. Under the influence of porous medium, the stall angle of attack of the airfoil increases by 5°, and the maximum lift coefficient is improved by 8.2%. The distribution parameters of porous medium can also significantly affect the aerodynamic characteristics of the airfoil. As the starting point of porous region moves forward, the stall angle of attack increases, while the lift coefficient in the linear segment of the airfoil decreases. As the thickness of porous medium increases, the lift coefficient of the airfoil's linear section decreases, while the drag of the airfoil increases, with a significant increase in the drag of the porous region. The influence of permeable characteristic parameters on the aerodynamic characteristics of the airfoil is significant. As the Darcy number increases, the lift coefficient of the porous airfoil slightly increases, and the drag decreases within a small range of angles of attack but increases in the stall segment. Anisotropy has a minor effect on the lift of the airfoil, but mainly affects its drag. The surface friction drag distributions on the airfoil and in the porous region are primarily determined by permeability in the x-direction. The distribution mode, air permeability characteristics and research conclusions of the semi-covered porous airfoil adopted in this paper can provide certain references for the design and research of bionic airfoils.

     

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