Numerical Simulation of Transpiration Cooling in a Laminar Hypersonic Boundary Layer - Dataset
Two-dimensional simulations of transpiration cooling in a laminar, hypersonic boundary layer were performed using the thermochemical implicit nonequilibrium algorithm (TINA): a Navier–Stokes solver. Coolant concentration and heat flux results are compared to data obtained from laminar transpiration...
| Autors principals: | , , , |
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| Format: | Dataset |
| Idioma: | English |
| Publicat: |
University of Oxford
2022
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