|January 19, 2011, 05:28||
How to visualise the mach number and pressure coefficient in ParaView
Join Date: May 2010
Posts: 44Rep Power: 7
I am now using rhoSimpleFoam to simulate the ONERA M6 WING in OpenFOAM.
And I have a question about how to get the mach number and pressure coefficient in ParaView.
Do I also need to set the initial and boundary condition for the Machnumber in the 0 folder?
Thanks in advance!
|January 19, 2011, 08:46||
Join Date: Aug 2009
Location: Braunschweig, Germany
Posts: 198Rep Power: 8
OpenFoam has tools to calculate the Mach number afterwards. The command might be "Mach". Have a look under utilities/postProcessing.
|Thread||Thread Starter||Forum||Replies||Last Post|
|Constant velocity of the material||Sas||CFX||15||July 13, 2010 08:56|
|RPM in Wind Turbine||Pankaj||CFX||9||November 23, 2009 05:05|
|Simulation of a single bubble with a VOF-method||Suzzn||CFX||18||October 2, 2009 04:18|
|air bubble is disappear increasing time using vof||xujjun||CFX||9||June 9, 2009 07:59|
|Automotive test case||vinz||OpenFOAM Running, Solving & CFD||98||October 27, 2008 09:43|