Numerical Simulation of the Supersonic Planar Mixing Layer

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Abstract:

Large eddy simulation (LES) has been used to simulate both non-reacting and reacting supersonic planar mixing layers at convective Mach number Mc=0.3. The different eddy characteristics of two cases have been visualized and discussed based on our calculated results, and the differences of mixing layer structures have also been shown, which can provide some important guide for future relative engineering design.

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Periodical:

Advanced Materials Research (Volumes 347-353)

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922-926

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October 2011

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] J. Hermanson and P. Dimotakis: J. Fluid Mech Vol. 199 (1989), p.333

Google Scholar

[2] P. McMurtry, J. Riley and R. Metcalfe: J. Fluid Mech Vol. 199 (1989), p.297

Google Scholar

[3] G.L. Brown and A. Roshko: J. Fluid Mech Vol. 64 (1974), p.775

Google Scholar

[4] I. Mahle, H. Foysi, S. Sarkar and R. Friedrich: J. Fluid Mech Vol. 593 (2007), p.171

Google Scholar

[5] L.M. Pickett and J.B. Ghandhi: Combust. Flame Vol. 132 (2003), p.138

Google Scholar

[6] D. Chakraborty, H.S. Mukunday and P.J. Paul, in: Effect of Stream Temperature on Hypervelocity Reacting Mixing Layer, (2003), AIAA 2003-1205.

DOI: 10.2514/6.2003-1205

Google Scholar

[7] T. Colonius, S.K. Lele and P. Moin: J. Fluid Mech Vol. 330 (1997), p.375.

Google Scholar

[8] A. Roshko: AIAA J. Vol. 14(10) (1976), p.349

Google Scholar