GrabCAD 模型信息
Inverted Aerofoil Spoiler with Louvered End Plates · 模型 59248
©️2023 This aerodynamic component is an inverted aerofoil designed to generate significant downforce by creating a pressure differential between its upper and lower surfaces. The design utilizes a negative angle of attack and the Venturi effect to produce a high-velocity, low-pressure region underneath the wing, effectively pushing the vehicle toward the ground for improved traction. To enhance efficiency, it features side end plates to minimize drag-inducing vortices, further optimized with elliptical louvers that mix internal and external air pressures to maintain a stable aerodynamic profile.
- 格式
- Rendering、SOLIDWORKS
- 分类
- Aerospace、Automotive、Machine design
- 标签
- wing design、formula student、fluid dynamics、iut_aus、downforce、aerofoil、spoiler、aerodynamics
- 数据更新
- 2026-10-01T13:42:42Z
