|August 5, 2010, 09:39||
Best practices for performing an analysis on a supersonic C-D nozzle in Star-CCM
Join Date: Jun 2009
Posts: 47Rep Power: 10
I am having a bit of difficulty creating an appropriate mesh and initializing my solution such that my CFD solution does not diverge (I am getting floating point exceptions after about 15 iterations).
Can anybody point me to a set of best practices to use for running CFD on C-D nozzles in Star-CCM
|August 9, 2010, 11:06||
Join Date: Oct 2009
Posts: 5Rep Power: 8
Assuming you are using the Coupled Solver, you should try AUSM+ for the Coupled Inviscid flux option and Grid Sequencing for the initialisation, then ramp your CFL.
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