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Investigations on the Flow Fields of Hypersonic Flow Past the Wall-Mounted Square Cylinder with Various Heights

机译:高超声速流过壁挂式方形圆柱体的流场研究

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Combined with the large eddy simulation (LES), a 3rd-order WENO scheme and the adaptive mesh refinement (AMR) technique, the hypersonic compressible flow (Ma = 5) past wall-mounted square cylinders with different heights is simulated numerically. Our results reveal that with the variation of cylinder heights, the pressure distributions of the flat plane in front of the cylinder are similar and have multiple peaks. The different flow patterns of the flow field around the cylinders are shown and discussed in detail. Our calculated results are in good agreement with corresponding experimental data which can provide important data for related research.
机译:结合大涡模拟(LES),三阶WENO方案和自适应网格细化(AMR)技术,对通过不同高度的壁挂式方筒的高超声速可压缩流(Ma = 5)进行了数值模拟。我们的结果表明,随着气缸高度的变化,气缸前面的平面压力分布是相似的,并且具有多个峰值。示出并详细讨论了围绕圆柱体的流场的不同流型。我们的计算结果与相应的实验数据吻合良好,可以为相关研究提供重要的数据。

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