Numerical Simulation of the Supersonic Planar Mixing Layer
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.
Weiguo Pan, Jianxing Ren and Yongguang Li
J. L. Gu et al., "Numerical Simulation of the Supersonic Planar Mixing Layer", Advanced Materials Research, Vols. 347-353, pp. 922-926, 2012