|November 9, 2009, 07:22||
Join Date: Apr 2009
Posts: 17Rep Power: 9
I am trying to simulate supersonic flow past a forward facing step using Riemann solvers at cell interfaces (i+1/2, j+1/2 etc). Not to sure how to implement boundary conditions at the corner.
The Corner is at (i + 1/2, j + 1/2) with flow traveling in increasing i direction
The B.C. for ghost pt (i+1, j) assuming zero pressure gradient, is it
P_(i+1, j) = P_(i, j)
P_(i+1, j) = P_(i + 1, j+1)
P_(i+1, j) = P(1, j+1)
or something completely different?
|Thread||Thread Starter||Forum||Replies||Last Post|
|Confusion between 'non-slip' and 'slip' B.C||jinwon park||Main CFD Forum||7||March 6, 2008 05:56|
|Urgent! Help on UDF to set B.C. of 3rd type||Ray Hong||FLUENT||0||December 28, 2005 20:35|
|How to set B.C. of the 2nd or 3rd type in UDS?||Ray Hong||FLUENT||0||December 28, 2005 07:03|
|Corner Vortex for Backward Facing Step||Patrick G. Hu||Main CFD Forum||0||August 6, 2002 09:34|
|Non-Reflecting B.C. in NSC2KE||Zou Chu||Main CFD Forum||2||May 27, 1999 21:26|