|April 8, 2004, 09:27||
AUSM+ low Mach
I have a question for the implementation of the AUSM+ scheme for low Mach numbers flows.
If we modify the speed of sound at the interface as suggested Liou, for which Mach numbers we must use the preconditionned matrix \Gamma ( for exemple the weiss smith matrix) ?
Does anyone has some remarks for the implementation of the AUSM+ scheme ??
|Thread||Thread Starter||Forum||Replies||Last Post|
|Development of a Low mach PISO solver||nishant_hull||OpenFOAM Programming & Development||0||August 25, 2009 12:48|
|compressible at low Mach number with uniteration||ricklee||Main CFD Forum||2||October 20, 2005 23:15|
|non-dimensional analysis in Fluent||Endee||FLUENT||8||September 7, 2005 16:16|
|Multicomponent fluid||Andrea||CFX||2||October 11, 2004 05:12|
|TVD scheme at low Mach number||Axel Rohde||Main CFD Forum||5||August 6, 1999 02:01|