Abstract
In this paper, the supersonic chemically reacting mixing layer is simulated with the third order ENN scheme, based on the Navier-Stokes equations, containing transport equations of all species. The numerical results show that the thickness of mixing layer increases gradually along the flow direction, and that the Kelvin-Helmholtz instabilities may not exist in mixing layer flows.
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The project supported by the National Natural Science Foundation of China
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Jianqiang, C., Fenggan, Z. Numerical simulation of supersonic reacting mixing layer. Acta Mech Sinica 13, 97–105 (1997). https://doi.org/10.1007/BF02487915
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DOI: https://doi.org/10.1007/BF02487915