|June 22, 2011, 19:20||
Join Date: Feb 2011
Posts: 469Rep Power: 11
This topic is related to http://www.cfd-online.com/Forums/ope...nfoam-v-v.html
Can someone give an example of an OpenFOAM steady viscous (laminar or turbulent (RANS)) incompressible, compressible, transonic, or supersonic aerodynamic (gamma=1.4, no chemistry) run where all the residuals were converged to machine zero?
Yes, the question is as basic as it seems. If one of the examples included with OpenFOAM answers the question, that would be fine too. Please just point it out.
|Thread||Thread Starter||Forum||Replies||Last Post|
|OpenFOAM 1.6.x - CentOS 5.3 x86_64||linnemann||OpenFOAM Installation||68||April 22, 2013 11:03|
|Cross-compiling OpenFOAM 1.6 on Linux for Windows 32 and 64bits with Mingw-w64||wyldckat||OpenFOAM Announcements from Other Sources||7||January 19, 2010 16:39|
|Problem installing OpenFOAM 1.5 installation on RHEL 4.||vwsj84||OpenFOAM Installation||4||April 23, 2009 04:48|
|2009 OpenFOAM Summer School in Zagreb, Croatia||hjasak||OpenFOAM Announcements from Other Sources||0||March 27, 2009 13:08|
|Convergence||Luiz Eduardo Bittencourt Sampaio (Sampaio)||OpenFOAM Running, Solving & CFD||11||July 20, 2005 06:33|