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Nonlinear development of subsonic modes on compressible mixing layers: a unified strongly nonlinear critical-layer theory

Published online by Cambridge University Press:  16 October 2008

CLIFFORD A. SPARKS  and
XUESONG WU
CLIFFORD A. SPARKS
Affiliation:
Department of Mathematics, Imperial College London, 180 Queens Gate, London SW7 2AZ, UK
XUESONG WU
Affiliation:
Department of Mathematics, Imperial College London, 180 Queens Gate, London SW7 2AZ, UK
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Abstract

This paper is concerned with the nonlinear instability of compressible mixing layers in the regime of small to moderate values of Mach number M, in which subsonic modes play a dominant role. At high Reynolds numbers of practical interest, previous studies have shown that the dominant nonlinear effect controlling the evolution of an instability wave comes from the so-called critical layer. In the incompressible limit (M = 0), the critical-layer dynamics are strongly nonlinear, with the nonlinearity being associated with the logarithmic singularity of the velocity fluctuation (Goldstein & Leib, J. Fluid Mech. vol. 191, 1988, p. 481). In contrast, in the fully compressible regime (M = O(1)), nonlinearity is associated with a simple-pole singularity in the temperature fluctuation and enters in a weakly nonlinear fashion (Goldstein & Leib, J. Fluid Mech. vol. 207, 1989, p. 73). In this paper, we first consider a weakly compressible regime, corresponding to the distinguished scaling M = O(ε1/4), for which the strongly nonlinear structure persists but is affected by compressibility at leading order (where ε ≪ 1 measures the magnitude of the instability mode). A strongly nonlinear system governing the development of the vorticity and temperature perturbation is derived. It is further noted that the strength of the pole singularity is controlled by T′c, the mean temperature gradient at the critical level, and for typical base-flow profiles T′c is small even when M = O(1). By treating T′c as an independent parameter of O(ε1/2), we construct a composite strongly nonlinear theory, from which the weakly nonlinear result for M = O(1) can be derived as an appropriate limiting case. Thus the strongly nonlinear formulation is uniformly valid for O(1) Mach numbers. Numerical solutions show that this theory captures the vortex roll-up process, which remains the most prominent feature of compressible mixing-layer transition. The theory offers an effective tool for investigating the nonlinear instability of mixing layers at high Reynolds numbers.

Type
Papers
Information
Journal of Fluid Mechanics , Volume 614 , 10 November 2008 , pp. 105 - 144
Copyright
Copyright © Cambridge University Press 2008

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