Design of a 2D Ahmed Body Rear Surface to Optimize Drag and Downforce Using Multi-objective Genetic Algorithm

R. Aranha, Anton Alconl, Kais Abdulmawjood, Martin Angelin-Chaab
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Abstract

In the design of race cars or airplanes the aerodynamics, such as its rear surface, is important to achieve the best performance possible. The objective of this paper was to optimize the rear surface design of a two-dimensional body (2D) to reduce drag and lift (to improve downforce) utilizing a metaheuristic optimization program. Drag and lift shape optimization can be solved using a multi-objective algorithm in which the primary objectives were to minimize the drag and the lift (to improve the downforce). To develop the program, the test shape used was an Ahmed Body box that was fixed without any tilt (0 degrees relative to the horizontal axis), where the rear surface was defined as five (5) equally spaced points for shape optimization. Alteration of the 5 points were constrained to change within 400mm in the positive or negative direction from the reference vertical axis. To achieve optimization, the program was designed to optimize the shape using an Evolutionary Algorithm (EA) - the Elitist Non-Dominated Sorting Genetic Algorithm (NSGA - II). The following parameters were fixed during initialization of the program: number of points for the rear surface, flow velocity, max allowed result. The program began optimization, by generating random candidate surface shapes. Then those candidate solutions were smoothed by the B-Spline function, utilizing applied CFD through the use of OpenFOAM. The program then compared the results and generated new candidate shapes to be tested until 40 generations (for each Reynolds number generated) were produced and the pareto progress was tracked for candidate solution comparison. This resulted in optimized shapes that are similar to experimentally tested and proven shapes that are shaped like a diffuser (as expected) that demonstrated the validity of the program.
基于多目标遗传算法的二维艾哈迈德车身后表面阻力和下压力优化设计
在赛车或飞机的设计中,空气动力学,比如它的后表面,对于实现最佳性能是很重要的。本文的目的是利用元启发式优化程序优化二维车身(2D)的后表面设计,以减少阻力和升力(以提高下压力)。阻力和升力形状优化可以使用多目标算法来解决,其中主要目标是最小化阻力和升力(以提高下压力)。为了开发该程序,使用的测试形状是一个固定的Ahmed Body box,没有任何倾斜(相对于水平轴0度),其中后表面被定义为五(5)个等间距的点,以进行形状优化。5个点的变化被限制在距离参考垂直轴正负方向400mm以内。为了实现优化,程序设计使用进化算法(EA) -精英非支配排序遗传算法(NSGA - II)来优化形状。在程序初始化期间固定了以下参数:后表面点数,流速,最大允许结果。程序开始优化,通过生成随机的候选表面形状。然后利用应用CFD软件OpenFOAM对候选解进行b样条函数平滑处理。然后,该程序比较结果并生成新的候选形状进行测试,直到生成40代(生成的每个雷诺数),并跟踪pareto进度以进行候选解决方案比较。这导致优化的形状与实验测试和证明的形状相似,形状像扩散器(如预期的那样),证明了程序的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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