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supersonic flow problem

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Old   April 14, 2008, 07:02
Default I simulate flow over a cone (3
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YekaniYasari
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I simulate flow over a cone (3D) with following condition:
Mach number=3
Pressure=101325
Temp=300
Angle of attack=3deg
I use different solver and boundary condition in OF1.3 but the solution don't converge.
Is there any comment about solver, boundary condition, discretization ,... for this kind of problems?
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