flow over rocket with plume -- CFD Online Discussion Forums

August 16, 2001, 11:53	flow over rocket with plume	#1
Rouham Ganji Guest Posts: n/a	Hi everyone, I have been modeling external flow over a rocket. I have been using pressure_far_field b.c. and it works fine. I wish to run a simulation with the engine on (with plume). Any suggestions on what boundary condition to use to simulate the plume. I don't have too much info at the nozzle exit. I know engine thrust, impulse and can estimate exhaust velocity. Appreciate any suggestions Thanks in advance Rouham

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