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How to set boundary condition in supersonic airflow

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December 14, 2011, 01:44	How to set boundary condition in supersonic airflow	#1
sailor New Member qingkai Join Date: Apr 2011 Posts: 11 Rep Power: 15	Hi all, I'm doing Fluent work to compute cavity in air in supersonic condition. And the boundary condition is set as Pressure inflow, Pressure far field and pressure outflow. But not convergence, is there something wrong in boundary condition seting?

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