OpenFOAM Convergence -- CFD Online Discussion Forums

June 22, 2011, 20:20	OpenFOAM Convergence	#1
Martin Hegedus Senior Member Martin Hegedus Join Date: Feb 2011 Posts: 500 Rep Power: 19	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.

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