Compressor cascade boundary conditions
I am doing a compressor cascade simulation in fluent. I have specified the boundary conditions as velocity inlet, pressure outlet, no slip wall for airfoil surfaces and periodic boundaries on the cascade walls.
I would like to know the mathematical idea behind solving this using the velocity inlet and pressure outlet. And what about the turbulence intensity to be specified? Can anyone help? |
All times are GMT -4. The time now is 11:37. |