supersonic flow problem -- CFD Online Discussion Forums

April 14, 2008, 08:02	I simulate flow over a cone (3	#1
yekaniyasari New Member YekaniYasari Join Date: Mar 2009 Location: Göteborg Posts: 6 Rep Power: 17	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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