穿孔二维飞翼的流动机制和空气动力学性能
Dou Wang1, Shuai Hao2, Dengyu Wu3
1Central South University, 932 South Lushan Road, Yuelu District, Changsha, Hunan Province, 410083, CHINA.
Bioinspiration & biomimetics
|January 16, 2026
概括
羽毛间隙改善了鸟类的飞行空气动力学. 数字模拟显示,气形板上向下打开的孔径显著提高了起重和效率,为微型车辆设计提供了洞察力.
科学领域:
- 空气动力学 航空动力学
- 流体力学 流体力学 流体力学
- 生物启发工程 生物启发工程
背景情况:
- 鸟类的羽毛间隙在飞行时提高了空气动力学性能.
- 了解这种现象背后的流动机制对于生物灵感设计至关重要.
研究的目的:
- 为了数值地研究平板气翼上的杆孔的流动机制.
- 分析穿孔位置,尺寸和打开角度对空气动力学性能的影响.
主要方法:
- 使用二维沉浸边界格子博尔兹曼方法进行流动模拟.
- 模拟了一个零厚平板气形翼,具有模仿羽毛间隙的链穿孔.
- 系统地改变穿孔参数:位置,尺寸和最大开口角.
主要成果:
- 向上穿孔增加了前沿压力差;向下穿孔减少了它.
- 链产生的旋流部分抵消了压力差异的影响.
- 具有最佳参数 (位置,尺寸,角度) 的向下穿孔显著改善了提升和提升效率.
- 向上穿孔在特定条件下 (位置,大小,角度) 显示出有限的性能提升.
结论:
- 往下穿孔通常优于向上的穿孔,在气形中提高起重和效率.
- 研究结果为优化微翼车辆的穿孔设计提供了洞察力.
- 需要对自动推进和3D流动相互作用进行进一步的研究.
相关概念视频
Steady, Laminar Flow Between Parallel Plates
797
Understanding steady, laminar flow between parallel plates is essential for analyzing and designing flow in narrow rectangular channels, commonly found in various water conveyance and drainage systems. The Navier-Stokes equations govern fluid motion and are generally challenging to solve due to their nonlinearity. However, simplifications are possible in certain cases, like the steady laminar flow between parallel plates. For this scenario, we assume steady, incompressible, laminar flow.
797
General External Flow Characteristics
523
The study of external flow is essential for creating structures and objects that interact efficiently and safely with moving fluids, such as air or water. When a body is immersed in a flowing fluid, it experiences two primary forces: drag, which opposes motion along the flow direction, and lift, which acts perpendicular to the flow. The shape, size, and orientation of the object influence these forces.Streamlined and Blunt Bodies in External FlowObjects in fluid flow are classified as...
523
Lift
475
Lift is a fundamental aerodynamic force that acts perpendicular to the direction of airflow. It plays a central role in achieving and sustaining flight and in stabilizing various vehicles. Lift primarily originates from pressure differences created across surfaces, such as an airfoil. A lower pressure region forms above the wing, while a higher pressure region forms below it, generating an upward force. This differential results from the shape and orientation of the airfoil, enabling the wing...
475
Drag
378
Drag is a resistive force opposing an object’s motion through a fluid, resulting from surface pressure and shear forces. It comprises two components: a perpendicular one from pressure and a tangential one from shear stress. Accurate drag calculations use pressure and wall shear stress distributions, often determined through Computational Fluid Dynamics (CFD) or wind tunnel testing. The drag coefficient, a dimensionless measure, depends on factors like shape, Reynolds number, Mach number,...
378
Free Jet
549
Free jets describe the flow of liquid exiting a reservoir through an opening into the atmosphere without resistance. The velocity (v) of the liquid jet is derived using Bernoulli's principle and expressed as:
549
Couette Flow
956
Couette flow represents the flow of fluid between two parallel plates, with one plate fixed and the other moving with a constant velocity. This configuration allows for a simplified analysis using the Navier-Stokes equations, which govern fluid motion under conditions of viscosity and incompressibility. For Couette flow, the assumptions include a steady, laminar, incompressible flow with a zero-pressure gradient in the flow direction. This flow type is beneficial for understanding shear-driven...
956


