方程式SAE空气动力学系统的建模、分析与设计

Isaac Van Baren, A. Milligan, S. Ashcraft, S. Rosser, Xiuling Wang
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引用次数: 0

摘要

该项目开发了一项研究方法,通过实施轻量化、高效的空气动力学设计来增加大学SAE方程式赛车的下压力。该团队计划通过底盘来提高性能,减少车辆的单圈时间,从而在处理弯道时提供更好的车轮牵引力和稳定性。完成后,空气动力学组件将使PNW车队能够更有效地参加2020年春季的FSAE设计竞赛。在减少阻力的同时,底盘还提供了引导车辆底盘下方空气的能力,从而为系统增加了“人工重量”。在底盘两侧之间建立了一个高强度的压力梯度,在身体下方发现了一个低负压区域。这种设计是基于流体动力学原理,特别是通过使用喷嘴和扩散器的文丘里效应。在这种方式下,车辆在转弯时可以获得较重汽车的好处,同时保持较轻汽车更高的直线加速度。本报告描述了在底盘设计中使用仿真软件,以及制造方法。在文献检索中获得的结果的复制中,进行了二维基准案例。随后,利用CFD和FEA/FEM技术对底盘模型进行了优化,得到了一个准备制造的部件。建立了一个操作程序,概述了其组装的复杂步骤。最后,它为未来的空气动力学团队提供了一个坚实的基础,可以在此基础上进行改进。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling, Analysis and Design of the Formula SAE Aerodynamics System
This project developed a study on methods to increase downforce on the university’s Formula SAE vehicle by implementing a lightweight, efficient aerodynamic design. The team planned to improve the performance and reduce lap times of the vehicle with an undertray, which grants better wheel traction and stability while handling corners. Upon completion, the aerodynamic component would have allowed the PNW Motorsports team to more effectively compete at the FSAE design competition in the spring of 2020. While reducing drag, an undertray provides the capability to direct the air beneath the vehicle chassis in a way which adds “artificial weight” to the system. A pressure gradient of high magnitude is established between the two sides of the undertray, with a low negative pressure region found beneath the body. This design is based upon the principles of fluid dynamics, in particular the venturi effect through the use of nozzles and diffusers. In this fashion, the vehicle can receive the benefits of a heavier car around corners while maintaining the higher straight-line acceleration of a lighter car. This report describes the use of simulation software in the design of an undertray, as well as the approach to manufacture it. Two-dimensional benchmark cases were performed in the replication of results obtained in a literature search. Subsequently, the undertray model was optimized with CFD and FEA/FEM techniques to obtain a component that was prepared for manufacturing. An operating procedure was established to outline the complicated steps of its assembly. Finally, it provides future aerodynamics teams with a solid foundation upon which improvements can be made.
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