|February 20, 2014, 04:43||
Viewing static pressure and temperature in Paraview
Join Date: May 2013
Posts: 45Rep Power: 5
I've been running a simulation of a wedge airfoil in supersonic flow. After the iteration is done, I went to Paraview. I am able to see several parameters such as p, rho, u, etc. but I don't see static pressure and static temperature. When I click on p, the legend showed that most area in the flow field has the value of total pressure I given as boundary condition.
What should I do to show static pressure and temperature distribution ?
|February 22, 2014, 12:07||
Join Date: Mar 2009
Location: Lisbon, Portugal
Blog Entries: 39Rep Power: 106
Are you referring to the tutorial "compressible/sonicFoam/ras/nacaAirfoil"? Or at least based on it?
And I've done a bit of Googling:
site:cfd-online.com "openfoam" sonicFoam static pressure
As for static temperature... I have no idea what that is or at least I can't remember...
|Thread||Thread Starter||Forum||Replies||Last Post|
|Calculation of the Governing Equations||Mihail||CFX||7||September 7, 2014 06:27|
|Static Temperature / Opening Temperature||JulianP||CFX||6||March 23, 2013 17:03|
|Water subcooled boiling||Attesz||CFX||7||January 5, 2013 04:32|
|Bulk temperature Tf is obtained from total or static temperature?||NPU_conanxie||FLUENT||0||March 30, 2011 05:56|
|what the result is negatif pressure at inlet||chong chee nan||FLUENT||0||December 29, 2001 06:13|