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Receptivity to free-stream disturbance waves for blunt cone axial symmetry hypersonic boundary layer

机译:钝锥轴向对称高超声速边界层对自由流扰动波的接收

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摘要

Based on high-order compact upwind scheme, a high-order shock-fitting finite difference scheme is studied to simulate the generation of boundary layer disturbance waves due to free-stream waves. Both steady and unsteady ow solutions of the receptivity problem are obtained by resolving the full Navier-Stokes equations. The interactions of bow-shock and free-stream disturbance are researched. Direct numerical simulation (DNS) of receptivity to free-stream disturbances for blunt cone hypersonic boundary layers is performed.
机译:基于高阶紧凑迎风方案,研究了一种高阶激波拟合有限差分方案,以模拟自由流波引起的边界层扰动波的产生。通过解析完整的Navier-Stokes方程,可以得到接受度问题的稳态和非稳态流动解。研究了船首冲击与自由流扰动的相互作用。对钝锥高超声速边界层的自由流扰动进行了直接数值模拟(DNS)。

著录项

  • 来源
    《》|2007年|P.1-4|共4页
  • 会议地点 Shanghai(CN)
  • 作者单位

    LNM, Institute of Mechanics, CAS, Beijing 100080, China;

    China Academy of Aerospace Aerodynamics, Beijing 100074, China;

    LNM, Institute of Mechanics, CAS, Beijing 100080, China;

    LNM, Institute of Mechanics, CAS, Beijing 100080, China;

    LNM, Institute of Mecha;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 流体力学;
  • 关键词

    receptivity; shock-fitting; compact upwind scheme; DNS; blunt cone;

    机译:接受度;减震;紧凑迎风方案; DNS;钝锥;

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