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[Sponsors] |
December 9, 2001, 10:16 |
opposed jets modeling
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#1 |
Guest
Posts: n/a
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Hello! I have to proof that STAR-CD does for droplets combustion calculation.
In order to do this I want to re-obtain an existing experiment data (velocity and temperature flow fields). The experiment was carried out for opposed jets configuration with fuel spray. For the first approach I work with gaseous fuel. The cold flow model seems to work well, but I can't ignite the flow (I'm using CHKI reaction scheme). What ignition initiation characteristics should I set? Any advises wanted!!! |
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