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Incipient Separation in Laminar Ramp-Induced Shock-Wave/Boundary-Layer Interactions

机译:层流引起的激波/边界层相互作用中的初始分离

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摘要

Incipient separation in laminar, ramp-induced shock-wave/boundary-layer interactions is examined using numerical solutions of the triple-deck equations and the full set of governing equations for compressible flows. Validation of the numerical methods is presented and the results are compared. A new comparison between solutions to the triple-deck equations and the compressible Navier-Stokes equations is presented. It was found that the triple-deck trends qualitatively match the trends produced by numerical solutions to the compressible Navier-Stokes equations. An expression for true incipient separation is derived and the trends are discussed.
机译:使用三层方程组和可压缩流的完整控制方程组的数值解,研究层流,斜波引起的激波/边界层相互作用中的初始分离。提出了数值方法的验证并比较了结果。提出了三层甲板方程和可压缩Navier-Stokes方程解的新比较。发现三层趋势定性地匹配了可压缩Navier-Stokes方程数值解所产生的趋势。得出了真正的初始分离的表达式,并讨论了趋势。

著录项

  • 来源
    《AIAA Journal》 |2018年第2期|524-531|共8页
  • 作者单位

    Univ Texas Arlington, Aerodynam Res Ctr, Arlington, TX 76019 USA|Univ Texas Arlington, Dept Mech & Aerosp Engn, Computat Fluid Dynam Lab, Arlington, TX 76019 USA;

    Univ Texas Arlington, Dept Mech & Aerosp Engn, Computat Fluid Dynam Lab, Arlington, TX 76019 USA;

    Univ Texas Arlington, Aerodynam Res Ctr, Dept Mech & Aerosp Engn, Arlington, TX 76019 USA;

  • 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
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