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Nozzle simulation for transitonal regime

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Old   June 16, 2016, 07:43
Default Nozzle simulation for transitonal regime
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anurag agrawal
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Dear all,

I have started using dsmc Foam recenty. I have done the tutorials and I think i have understood to some degree how to simulate flow over bodies. However, I need to simulate the exhaust of a rocket nozzle in transitional regime. Going over some threads i realized that some people have worked on it. My question how come we do this in dsmc Foam. The people i contacted told me to develop my own solver using Bird's code.

A line in reply would be helpful.

Thanks and regards
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