i am simulating 3D flow over a cone cylinder at supersonic speed. mesh is cut at the base of the body and wake is not taken into account. which Boundary Condition should be used at the base and at that end of domain ?
i am using FLUENT 6.2 solver. 'Pressure far field' is used for inlet and side boundary faces.I cant use outflow boundary condition since pressure far field and out flow boundaries cant exist together(a message shown in fluent).
plz guide me
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