|June 16, 2016, 07:43||
Nozzle simulation for transitonal regime
Join Date: Jun 2016
Posts: 1Rep Power: 0
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
|Thread||Thread Starter||Forum||Replies||Last Post|
|Premixed flame simulation with CD nozzle||Subrat@cgpl||Main CFD Forum||0||March 29, 2016 03:54|
|Jet exhaust from the nozzle simulation||Krafta||OpenFOAM||0||September 2, 2014 12:30|
|Piston Cooling Nozzle Simulation||rajeev50588||STAR-CCM+||1||February 26, 2013 04:41|
|Nozzle - Simulation converges, but data incorrect||fade||CFX||0||July 20, 2009 04:13|
|Need assistance in BC's for simulation of Vacuum cleaning nozzle||bruce||OpenFOAM Running, Solving & CFD||0||May 22, 2009 13:56|