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High-order detached-eddy simulation of external aerodynamics over an SAE notchback model

机译:基于SAE缺口模型的外部空气动力学的高阶分离涡模拟

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摘要

This research explores the modification and implementation of a Detached-Eddy Simulation (DES) in a high-order compressible solver and its application to automotive aerodynamics. This was conducted on a 20 degrees SAE Reference Notchback Model with a Reynolds number of 2.23 x 10(5). This DES algorithm implemented within FLAMENCO, which is finite-volume research code operating over multi-block meshes, was used for all the simulations. The primary objectives were to capture unsteady flow features, separated coherent structures and also relax the meshing requirements to improve accessibility to turbulence-resolving methods for realistic configurations. This also aims to better understand the separated flow physics, especially around the base surfaces of the car. Simulations for three mesh refinement levels were compared to wind-tunnel measurements. Even on relatively coarse meshes (similar to 7m cells) for DES, time-averaged Cp was obtained with maximum errors of < 8%.
机译:这项研究探索了高阶可压缩求解器中的分离涡流仿真(DES)的修改和实现及其在汽车空气动力学中的应用。这是在雷诺数为2.23 x 10(5)的20度SAE参考缺口模型上进行的。在FLAMENCO中实现的DES算法是在多块网格上运行的有限体积研究代码,用于所有仿真。主要目的是捕获不稳定的流动特征,分离的相干结构,还放宽了网格划分要求,以提高针对实际配置的湍流解析方法的可访问性。这也旨在更好地了解分离的流动物理原理,尤其是在汽车底面周围。将三个网格细化级别的仿真与风洞测量进行了比较。即使在相对较粗的DES网格(类似于7m单元)上,也获得了时间平均Cp,最大误差小于8%。

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  • 来源
    《The Aeronautical Journal》 |2017年第1243期|1342-1367|共26页
  • 作者

    Islam A.; Thornber B.;

  • 作者单位

    Univ Sydney Darlington, Sch Aerosp Mech & Mechatron Engn, Sydney, NSW 2006, Australia;

    Univ Sydney Darlington, Sch Aerosp Mech & Mechatron Engn, Sydney, NSW 2006, Australia;

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  • 正文语种 eng
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