DIRECT NUMERICAL SIMULATION OF THE TRANSITIONAL SUPERSONIC BOUNDARY LAYER ON A FLAT PLATE |
| 4 | |
| 2011 |
| scientific article | 532.51;519.8 | ||
| 1235-1236 |
| On the basis of full unsteady Navier-Stokes equations of compressible gas the direct numerical simulation of linear and non- linear stages of laminar-turbulent transition in the flat-plate boundary layer is performed at flow Mach number M = 2. |
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