How to set boundary condition in supersonic airflow -- CFD Online Discussion Forums

December 14, 2011, 02:44	How to set boundary condition in supersonic airflow	#1
sailor New Member qingkai Join Date: Apr 2011 Posts: 11 Rep Power: 15	Hi all, I'm doing Fluent work to compute cavity in air in supersonic condition. And the boundary condition is set as Pressure inflow, Pressure far field and pressure outflow. But not convergence, is there something wrong in boundary condition seting?

Posting Rules
You may not post new threads You may not post replies You may not post attachments You may not edit your posts BB code is On Smilies are On [IMG] code is On HTML code is Off Trackbacks are Off Pingbacks are On Refbacks are On Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
External Radiation Boundary Condition (Two sided wall), Grid Interface	CFD XUE	FLUENT	0	July 8, 2010 07:49
Looking for suggestions about how to set up a boundary condition	plaunie	STAR-CCM+	3	April 6, 2010 14:08
Boundary condition on 3D Supersonic nozzle problem with atmosphere	dokeun	FLUENT	0	April 1, 2010 22:59
how to set boundary condition	jai	CFX	0	March 10, 2009 07:28
[Commercial meshers] Trimmed cell and embedded refinement mesh conversion issues	michele	OpenFOAM Meshing & Mesh Conversion	2	July 15, 2005 05:15

All times are GMT -4. The time now is 19:53.