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Old   December 7, 2010, 14:03
Post supersonic combustion
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seyed shamsaldin naiemaie moosavi
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hi everyone,
I have problem with 2d supersonic combustion modeling with fluent. my case is air as mainflow with mach 2.2 and 50 kg/s massflowrate and also H2 as fuel with mach 1 and 1.5 kg/s mass flow rate. I get into troubble with mixing and converging residuals also I must model reaction but I dont know which boundray condition and solver should select for this case.
Please help me if you can.tnx alot...
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Old   December 27, 2010, 04:14
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seyed shamsaldin naiemaie moosavi
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I have the problem yet, but I think if I change the boundry condition, it can be solved .
anyone hasnt any idea???
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