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December 7, 2010, 13:03 |
supersonic combustion
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#1 |
New Member
seyed shamsaldin naiemaie moosavi
Join Date: Nov 2010
Posts: 2
Rep Power: 0 |
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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December 27, 2010, 03:14 |
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#2 |
New Member
seyed shamsaldin naiemaie moosavi
Join Date: Nov 2010
Posts: 2
Rep Power: 0 |
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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