opposed jets modeling
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!!!
|All times are GMT -4. The time now is 20:57.|