|October 27, 2009, 11:35||
Join Date: Oct 2009
Posts: 6Rep Power: 8
I am modeling a compressible turbulent non-premixed combustion in a nozzle.
I have some problems with boundary conditions and solver:
I set pressure inlnet for Air Inlet, pressure far-field for Outlet, velocity inlet for
Fuel Inlet. But for the walls I have no idea. Should I set all of them Heat Flux Zero? Should I let fluent to solve it by deafault conditions?
Fluent does not let me to solve it by density based solver. Why? What should I do for this problem?
Thanks in advance.
|Thread||Thread Starter||Forum||Replies||Last Post|
|Hydrogen Air combustion in a combustion chamber||popi||CFX||7||July 11, 2007 18:40|
|Need Similar Combustion Tutorial as my model||Arnab||CD-adapco||0||May 24, 2005 18:23|
|Multiresolution + Turbulence + Combustion||Raul||CD-adapco||0||March 18, 2005 08:56|
|Multiresolution + Turbulence + Combustion||Raul||FLUENT||0||March 18, 2005 08:54|
|Multiresolution + Turbulence + Combustion||Raul||Main CFD Forum||0||March 18, 2005 08:53|