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Large eddy simulation of the flow around bluff body with drag reduction device.

机译:用减阻装置对阻流体周围的流动进行大涡模拟。

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摘要

This thesis focuses on the use of LES to simulate the flow around elliptical bluff body with blunt trailing edge fitted with open base cavity. The main objective of this study is to determine the effects of the cavity on the drag of the body. A secondary but important objective is to demonstrate that LES can provide accurate representation of the flow around this bluff body. Moreover, LES results can complement the available experimental results in order to provide a much better understanding of the flow. The simulations were carried out at a Reynolds number of 2.6x104 based on the height of the body using Spalart-Allmaras RANS model while the LES were performed using Smagorinsky dynamic model. A grid-independence test was conducted using three grids which contain 0.85M, 1.3M and 1.7M cells, respectively. This test shows that the results are grid-independent. The LES results predicted the mean flow field in the near wake with good accuracy as compared to the experimental mean flow field obtained. The base pressure results show that the base pressure coefficient for the base model was around -0.56, which agrees well with the experimental results .By attaching the cavity, the base pressure has increased. The increase in base pressure coefficient was around 44% using 1/3 h cavity and this agrees well with the experimental measurements. The RANS predicted drag coefficient of 0.56 for the base model and 0.471 for the cavity model. This represents a difference of 8% for the base model and 34% for the cavity model when compared with experiment drag coefficients (0.61 for the base model and 0.35 for the cavity model). For the LES, the drag coefficient of the base model was around 0.65 (6.5% difference) and using the cavity, the drag coefficient was reduced to around 0.37 (5.74% difference).;Details of the mean velocity components have been compared with experimental data at various locations in the wake region of the flow. Observation on the comparison between LES and RANS shows that LES predicted the mean flow field more accurately than RANS particularly downstream the recirculation regions. The length of the recirculation region was over predicted by RANS compared to LES. The prediction of this length by LES was in excellent agreement with experimental measurement.
机译:本文着重于利用LES模拟椭圆钝体的流动,该钝体后缘装有开放式基腔。这项研究的主要目的是确定空腔对人体阻力的影响。第二个但重要的目标是证明LES可以准确表示该钝体周围的流动。此外,LES结果可以补充可用的实验结果,以便更好地了解流程。使用Spalart-Allmaras RANS模型,根据车身高度在2.6x104的雷诺数下进行了仿真,而使用Smagorinsky动力学模型进行了LES。使用三个分别包含0.85M,1.3M和1.7M单元的网格进行了网格独立性测试。该测试表明结果与网格无关。与获得的实验平均流场相比,LES结果预测了近尾流中的平均流场,具有很高的精度。基础压力结果表明,基础模型的基础压力系数约为-0.56,与实验结果吻合良好。通过附着型腔,基础压力有所提高。使用1/3小时的腔体,基本压力系数的增加约为44%,这与实验测量结果非常吻合。 RANS预测的阻力系数对于基本模型为0.56,对于空腔模型为0.471。与实验阻力系数(基础模型为0.61,空腔模型为0.35)相比,基本模型的误差为8%,空腔模型的误差为34%。对于LES,基本模型的阻力系数约为0.65(相差6.5%),使用腔体,阻力系数减小至0.37(相差5.74%)。流尾流区域中各个位置的数据。对LES和RANS的比较观察表明,LES比RANS更准确地预测了平均流场,特别是在再循环区域的下游。与LES相比,RANS预测了再循环区域的长度。 LES对这一长度的预测与实验测量非常吻合。

著录项

  • 作者

    Al-Anazi, Khalid Qaied.;

  • 作者单位

    King Fahd University of Petroleum and Minerals (Saudi Arabia).;

  • 授予单位 King Fahd University of Petroleum and Minerals (Saudi Arabia).;
  • 学科 Engineering Aerospace.
  • 学位 M.S.
  • 年度 2010
  • 页码 109 p.
  • 总页数 109
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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