Compressible mixing layer: linear theory and direct simulation
Sandham, N.D. and Reynolds, W.C. (1990) Compressible mixing layer: linear theory and direct simulation AIAA Journal, 28, (4), pp. 618624.
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Description/Abstract
Results from linear stability analysis are presented for a wide variety of mixing layers, including lowspeed layers with variable density and high Mach number mixing layers. The linear amplification predicts correctly the experimentally observed trends in growth rate that are due to velocity ratio, density ratio, and Mach number, provided that the spatial theory is used and the mean flow is a computed solution of the compressible boundarylayer equations. It is found that threedimensional modes are dominant in the highspeed mixing layer above a convective Mach number of 0.6, and a simple relationship is proposed that approximately describes the orientation of these waves. Direct numerical simulations of the compressible NavierStokes equations are used to show the reduced growth rate that is due to increasing Mach number. From consideration of the compressible vorticity equation, it is found that the dominant physics controlling the nonlinear rollup of vortices in the highspeed mixing layer is contained in an elementary form in the linear eigenfunctions. It is concluded that the linear theory can be very useful for investigating the physics of free shear layers and predicting the growth rate of the developed plane mixing layer
Item Type:  Article  

ISSNs:  00011452 (print) 

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ePrint ID:  72048  
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Date Deposited:  18 Jan 2010  
Last Modified:  18 Apr 2017 20:58  
Further Information:  Google Scholar  
URI:  http://eprints.soton.ac.uk/id/eprint/72048 
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