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中文核心期刊

仿鸟类翅膀羽毛多孔介质的雷诺数效应

REYNOLDS NUMBER EFFECTS ON A BIRD-FEATHER-INSPIRED POROUS-MEDIA

  • 摘要: 鸟类羽毛具有透气性, 羽毛的层状覆盖特征决定了羽毛透气性呈现出各向异性的多孔介质特点, 这种多孔介质特性对鸟类翅膀的气动特性带来什么样的影响是本文研究工作的基本动机. 本文构造了一种仿鸟类羽毛的各向异性多孔介质翼型, 反映鸟类羽毛的宏观各向异性特征, 通过隐式大涡模拟方法, 通过对比不同雷诺数工况下翼型表面压力分布、速度场结构及分离行为, 研究了不同雷诺数下多孔介质对翼型气动特性的影响机制. 研究结果表明, 在雷诺数范围(Re = 6 × 104 ~ 4 × 105)内, 一定迎角下翼型前缘的附面层分离涡可以部分渗入多孔介质内部, 避免了分离涡向下游发展形成更大范围的分离区, 降低了翼型的阻力和阻力脉动; 但是, 在更低的雷诺数(Re = 4 × 104 ~ 5 × 104)条件下, 翼型表面流动状态发生剧变, 多孔介质的低速流动反而增强了分离涡的形成和发展, 恶化了翼型的气动性能. 研究结果表明, 仿鸟类羽毛的各向异性多孔介质结构在特定雷诺数范围内能够有效调控翼型流动特性, 为理解鸟类羽毛结构在气动性能提升中的作用提供了新的认识.

     

    Abstract: Bird feathers are inherently permeable, and their layered overlapping arrangement gives rise to anisotropic permeability characteristics. From a macroscopic perspective, a feathered wing surface can therefore be regarded as an anisotropic porous medium. Understanding how such porous-media characteristics influence the aerodynamic performance of bird wings constitutes the fundamental motivation of the present study. In this work, a bird-feather-inspired anisotropic porous-media airfoil is constructed to represent the dominant macroscopic anisotropy associated with real feather assemblies. A Monotone Integrated Large Eddy Simulation (MILES) approach is employed to investigate the aerodynamic behavior of the porous airfoil under different Reynolds number conditions. By comparing surface pressure distributions, velocity field structures, and flow separation characteristics at various Reynolds numbers, the mechanisms by which porous media affect airfoil aerodynamics are systematically examined. The results show that within a Reynolds number range of Re = 6 × 104 ~ 4 × 105, and at a fixed attack angle, the leading-edge separation vortex can partially penetrate into the porous medium. This penetration suppresses the downstream growth of the separation vortex and prevents the formation of a large-scale separated region, thereby reducing the aerodynamic drag and drag fluctuations of the airfoil. In contrast, at lower Reynolds numbers (Re = 4 × 104 ~ 5 × 104) a pronounced change in the surface flow state is observed. Under these conditions, the low-velocity flow within the porous medium enhances the formation and development of separation vortices, leading to a deterioration of aerodynamic performance. These findings indicate that bird-feather-inspired anisotropic porous-media structures are capable of effectively modulating airfoil flow characteristics within a specific Reynolds number range. The results provide new insights into the aerodynamic role of feather structures and contribute to a deeper understanding of how feather-like porous media can influence aerodynamic performance.

     

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