主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
透气特征参数对翼型气动特性的影响
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作者:
作者单位:

1.西北工业大学;2.西北工业大学 航空学院

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中图分类号:

V211

基金项目:

翼型、叶栅空气动力学国家级重点实验室基金


Influence of permeability characteristics on the aerodynamic characteristics of airfoils
Author:
Affiliation:

Northwestern Polytechnical University

Fund Project:

Foundation of National Key Laboratory of Airfoil and Cascade Aerodynamics

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    摘要:

    羽毛在鸟类飞行活动中发挥着重要作用,多孔介质材料可用于模拟鸟类羽毛的透气特性,基于Darcy-Brinkman-Forchheimer 模型开展透气特性参数对翼型气动特性影响的研究。以NACA0012 翼型为研究对象,将多孔材料覆盖在翼型表面来模拟鸟翼覆羽,通过CFD 方法探究透气特征参数对翼型气动特性的影响。结果表明:半覆盖多孔翼型能够显著提升翼型的气动性能,尤其能明显改善翼型的失速特性,失速迎角增加2°,最大升力系数提高16.2%;透气特征参数达西数和孔隙率对翼型气动特性有显著影响,翼型的气动性能随着达西数的增大而变差,随着孔隙率的增大而提高;各向异性对翼型气动特性有显著影响,其中y 方向渗透率大的各向异性多孔翼型气动特性最优,与鸟翼覆羽结构也是一致的。

    Abstract:

    Porous media materials, due to their unique pore structure, can be used to simulate the permeability characteristics of bird wing feathers. This article takes the NACA0012 airfoil as the research object, covers the surface of the airfoil with porous materials to simulate bird wing feathers, applies the theory of porous media, and explores the influence of permeability parameters on the aerodynamic characteristics of the airfoil through CFD method.The results show that: 1) The semi covered porous airfoil can significantly improve the aerodynamic performance of the airfoil, especially the stall characteristics of the airfoil. The stall angle of attack increases by 2°, and the maximum lift coefficient increases by 16.2%; 2) The permeability characteristic parameters Darcy""s number and porosity have a significant impact on the aerodynamic characteristics of the airfoil. The aerodynamic performance of the airfoil deteriorates with the increase of Darcy""s number and improves with the increase of porosity; 3) Anisotropy has a significant impact on the aerodynamic characteristics of airfoils, among which the anisotropic porous airfoil with high permeability in the y-direction has the best aerodynamic characteristics, which is consistent with the bird wing feather structure. The surface covered porous medium airfoil scheme and its research conclusions adopted in this article can provide a reference for the design and research of bionic airfoil.

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历史
  • 收稿日期:2024-08-19
  • 最后修改日期:2024-11-10
  • 录用日期:2024-11-19
  • 在线发布日期: 2025-07-14
  • 出版日期: