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jet in a supersonic crossflow with Fluent

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Old   July 18, 2024, 04:30
Default jet in a supersonic crossflow with Fluent
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付思泽
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I want to simulate supersonic cross-flow jets in Fluent,Now it is known that the total pressure of the cross-flow inlet is 241kPa and the total temperature is 295k; the total pressure of the jet inlet is 476kPa and the total temperature is 295k; the Mach number of the cross-flow inlet is 1.6 and the Mach number of the jet inlet is 1.I want to use pressure inlet and pressure outlet boundary conditions in fluent.Now I don't know how to set the gauge pressure at the exit
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