The Setting of Boundary Conditions
I want to simulate a 2-Demensional supersonic inviscid flow over a circular body(the govering equation system is the 2-D Euler Equations system). I am planning to use shock-capturing schemes like ausm+.
But I have no ideal on how to determine the boundary conditions on the outflow and wall.
Thanks a lot.
|All times are GMT -4. The time now is 18:17.|