超音速混合层向湍流的过渡

Mohamed Si Ameur, Jean-Pierre Chollet
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引用次数: 0

摘要

数值模拟用于研究刚性壁之间空间发展的可压缩混合层向湍流的过渡。快流和慢流是超音速的,马赫数分别为M1=4.5和M2=1.6。采用高阶Godunov格式分段抛物法,用Roe的近似Riemann解算器求解二维可压缩流的全Navier-Stokes方程。目的是研究从线性不稳定状态到湍流的过渡,并与Tam和Hu的线性稳定性分析进行比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Transition à la turbulence d'une couche de mélange supersonique

Numerical simulations are used to study the transition to turbulence of a spatially developed compressible mixing layer between rigid walls. The fast and slow flows are supersonic with Mach numbers M1 = 4.5 and M2= 1.6 respectively. The full Navier-Stokes equations are solved for a 2D compressible flow with a high order Godunov 's scheme piecewise parabolic method (PPM) with the approximate Riemann solver of Roe. The purpose is to study the transition to turbulence from the linear regime of instability, with comparison to the linear stability analysis of Tam and Hu.

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