|October 14, 2012, 17:04||
combustion of solid rocket propellant
Join Date: Oct 2012
Posts: 1Rep Power: 0
I am new to cfd and fluent 6.3. first of all I tried to define a new material following a post in this forum and the material got created. Then when I tried to use that material in non premixed combustion then that material was not found. I am also having problems in defining the boundary conditions and zones for 2D cylindical grain in Gambit. when the msh file is imported the zones are getting divided. Please help.
Last edited by email@example.com; October 15, 2012 at 08:39.
|Thread||Thread Starter||Forum||Replies||Last Post|
|nozzle flow for a solid propellant rocket||ilperalta||FLUENT||0||April 26, 2011 10:48|
|solid rocket combustion||ssixr||FLUENT||0||June 18, 2010 22:50|
|Rocket Combustion||Aralati||FloEFD, FloWorks & FloTHERM||0||March 13, 2010 22:42|
|Solid combustion problem....||godspeedsam||FLUENT||2||February 21, 2010 18:46|
|CFX4.3 -build analysis form||Chie Min||CFX||5||July 12, 2001 23:19|