COMPRESSIBILITY EFFECTS AND MIXING ENHANCEMENT IN TURBULENT FREE SHEAR FLOWS

Computational simulations have been performed to study compressible, spatially developing turbulent free shear layers with various velocity regimes-subsonic/subsonic, supersonic/subsonic, and supersonic/supersonic for convective Mach numbers in the range of 0.14-1.28. The numerical code used the finite volume technique and a modified Godunov's scheme, The computed results for the supersonic/subsonic case are first compared with experimental axial mean-velocity profiles, vorticity thickness, and turbulence parameters. Mixing layers with various velocity regimes are then calculated to investigate compressibility effects on the evolution of large-scale structures through the flow visualization of the vorticity field, growth rate of the vorticity thickness, and vorticity dynamics analysis. Various forcing frequencies are applied at the inflow boundary to examine mixing enhancement for free shear layers with higher convective Mach numbers. It is found for the first time that the growth rate of supersonic/supersonic free shear layers increases markedly when the forced layers move up and down with time instead of forming vortex roll up and pairing.