|March 8, 2012, 08:05||
Join Date: Nov 2011
Posts: 13Rep Power: 6
I am Doing a simulation of valveless pulsejet engine.
After exhaust cycle when the pressure in the engine drops below the atm. pressure ,the flow is supposed to reverse at outlets,so now they become inlets leading the fresh air rushing in to the combustion space.
basically same the ports or sections toggle between inlet and outlet for intake and exhaust cycle,And thats the story behind theoperation of engine
Now how can i impose boundary conditions that are pressure dependent
|Thread||Thread Starter||Forum||Replies||Last Post|
|symmetry boundary conditions in cfx||lost.identity||CFX||41||May 22, 2013 07:21|
|Impinging Jet Boundary Conditions||Anindya||Main CFD Forum||24||January 11, 2012 14:40|
|OpenFOAM Variable Velocity Boundary Conditions||NickolasPl||OpenFOAM Programming & Development||2||May 19, 2011 05:37|
|boundary conditions and mesh exporting||vaina74||Open Source Meshers: Gmsh, Netgen, CGNS, ...||2||May 27, 2010 09:38|
|Trimmed cell and embedded refinement mesh conversion issues||michele||OpenFOAM Other Meshers: ICEM, Star, Ansys, Pointwise, GridPro, Ansa, ...||2||July 15, 2005 04:15|