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Interaction of Three-Dimensional Protuberances with a Supersonic Turbulent Boundary Layer

机译:三维隆起与超音速湍流边界层的相互作用

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摘要

A comprehensive computational fluid dynamics study of the surface-pressure fluctuations induced by a cylindrical protuberance in a supersonic turbulent boundary layer is presented. The effects of two important parameters on the surface-pressure fluctuations are investigated: protuberance height to boundary-layer thickness and surface curvature. The turbulent boundary layer is modeled using a hybrid Reynolds-averaged Navier-Stokes and large-eddy-simulation approach known as detached-eddy simulation. At first extensive comparisons to experimental data for the surface-pressure coefficient and the unsteady surface-pressure coefficient were performed. Results from our computational-fluid-dynamics computations compared well to the experimental data in the wake region downstream of the protuberance and in the vicinity of the protuberance at other locations. Increasing the protuberance height relative to the boundary-layer thickness resulted in higher sound-pressure levels on the surface. In addition, the surface-pressure fluctuation showed more coherence in the spanwise direction ahead of the protuberance and immediately downstream of it Increasing the surface curvature lowered the sound-pressure levels on the surface and resulted in stretched coherent structures in the spanwise direction. Convection velocities of the turbulent structures increased away from the protuberance and were in agreement with published literature.
机译:提出了在超声速湍流边界层中由圆柱突起引起的表面压力波动的综合计算流体动力学研究。研究了两个重要参数对表面压力波动的影响:凸起高度对边界层厚度和表面曲率的影响。湍流边界层是使用混合雷诺平均Navier-Stokes和大涡流仿真方法(称为分离涡流仿真)建模的。首先,对表面压力系数和非稳态表面压力系数与实验数据进行了广泛的比较。我们的计算流体动力学计算结果与突起下游的尾流区域以及其他位置的突起附近的实验数据进行了很好的比较。相对于边界层厚度增加隆起高度导致表面上更高的声压级。另外,表面压力波动在隆起之前在翼展方向上显示出更多的连贯性,并且紧接在其下游。表面曲率的增加降低了表面上的声压级,并导致在翼展方向上的拉伸的相干结构。湍流结构的对流速度远离隆起,并且与已发表的文献一致。

著录项

  • 来源
    《AIAA Journal》 |2013年第7期|1657-1666|共10页
  • 作者单位

    External Environments, currently Blue Origin in Kent, WA 98032,NASA Marshall Space Flight Center, Huntsville, Alabama 35811;

    Mechanical and Aerospace Engineering,University of Alabama in Huntsville, Huntsville, Alabama 35899;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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