Linear stability of a compressible flow in a channel

IF 0.8
M Deka, G Tomar, V Kumaran
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Abstract

Summary Modal instabilities in a compressible flow through a channel at high Reynolds numbers are studied for three-dimensional (3D) perturbations. In addition to the Tollmien–Schlichting (TS) mode, there exist compressible modes in a channel flow that do not have a counterpart in the incompressible limit. The stability characteristics of these compressible modes, obtained through numerical calculations, are compared with boundary layer and Couette flows that have been previously studied. The dominant compressible instabilities in a channel flow are shown to be viscous in nature, in contrast to compressible boundary layer modes. For general compressible bounded-domain flows, a necessary condition for the existence of neutral modes in the inviscid limit is obtained, and this criterion is used to determine critical Mach numbers below which the compressible modes remain stable. This criterion also delineates a range of wave-angles which could go unstable at a specified Mach number. Asymptotic analysis is carried out for the lower and upper branches of the stability curve in the limit of high Reynolds number for both the T-S and the compressible modes. A common set of relations are identified for the scaling exponents, and the leading order eigenvalues for the unstable modes are obtained through an adjoint-based procedure. The asymptotic analysis shows that the stability boundaries for 3D perturbations at high Reynolds numbers can be calculated from the strain rate and the temperature of the base flow at the wall.
通道中可压缩流的线性稳定性
摘要 针对三维(3D)扰动,研究了高雷诺数条件下流经通道的可压缩流的模态不稳定性。除 Tollmien-Schlichting (TS) 模式外,通道流中还存在不可压缩极限中没有对应模式的可压缩模式。通过数值计算获得的这些可压缩模式的稳定性特征与之前研究过的边界层和库埃特流进行了比较。与可压缩边界层模式相比,通道流中的主要可压缩不稳定性在本质上是粘性的。对于一般的可压缩界域流,得到了在不粘性极限中存在中性模式的必要条件,并利用这一标准确定了临界马赫数,在此马赫数以下,可压缩模式保持稳定。这一标准还划定了在特定马赫数下可能不稳定的波角范围。对 T-S 和可压缩模式在高雷诺数极限下的稳定性曲线的下分支和上分支进行了渐近分析。为缩放指数确定了一组共同的关系,并通过基于邻接的程序获得了不稳定模式的前阶特征值。渐近分析表明,高雷诺数下三维扰动的稳定边界可以通过应变率和壁面基流的温度计算出来。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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