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...
| Main Authors: | , , , |
|---|---|
| Format: | Dataset |
| Jezik: | English |
| Izdano: |
University of Oxford
2022
|