Abstract
The direct numerical simulation (DNS) of two-dimensional compressible turbulent mixing layers is reported in this paper. The numerical approach is based on a proven high-order finite difference method and results are presented for convective Mach numbers Mc =0.5, 0.8 and 1.0. All scales of flow are resolved with a 2562 grid, although results are also obtained for 642, 962 and 1282 grids for the purpose of determining the effective accuracy and grid-independence of our calculations. Results are reported for the growth rate of the vorticity thickness, the vortex roll-up in the flow field and the distribution of density. Furthermore, each term in the evolution equations for the Reynolds stress tensor has been computed for the purpose of examining the intensity of turbulence at the various Mach numbers. The effect of Mach number is reported for the 'shear' components of the anisotropy tensor, the dissipation tensor, pressure-strain, and the triple correlation tensor. For the Reynolds stress tensor the three components (R11, R12, R22) are compared for Mc =0.8. To our knowledge, these results on mixing layers are new but are quite invaluable in guiding modeling efforts intended for generating engineering design data.
| Original language | English |
|---|---|
| Pages | 8 |
| Number of pages | 8 |
| State | Published - 1997 |
| Event | Proceedings of the 1997 ASME Fluids Engineering Division Summer Meeting, FEDSM'97. Part 24 (of 24) - Vancouver, Can Duration: Jun 22 1997 → Jun 26 1997 |
Conference
| Conference | Proceedings of the 1997 ASME Fluids Engineering Division Summer Meeting, FEDSM'97. Part 24 (of 24) |
|---|---|
| City | Vancouver, Can |
| Period | 06/22/97 → 06/26/97 |
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