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Old   February 23, 2010, 09:51
Default Transonic airplane
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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?

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