Transonic airplane
 

Hi!
Can you help me to set the .cas file to solve the flow over a transonic airplane using realizable k-epsilon turbulence?

First of all: what would you use as boundary condition to model the air intake of the motor?

And second: I've setted ideal gas and density based model. The energy equation is activated. But why does in "solve-controls-solution" I found only flow and turbulence in the equations and not the energy one? And I can't choose coupled? I think that the reason is that I setted Density based solver and so the coupled is implicit?

Thanks!
sarav