compressible at low Mach number with uniteration -- CFD Online Discussion Forums

October 19, 2005, 03:00	compressible at low Mach number with uniteration	#1
ricklee Guest Posts: n/a	Dear all I write a code for compressible flow. But I want used in low Mach number. Preconditioning is the best way to solve my problem. But the Preconditioning is always used in iteration process. I used approximation Godunov method, so the code is "uniteration". Can I used Preconditioning in my code to solve the problem at low Mach number?

Posting Rules
You may not post new threads You may not post replies You may not post attachments You may not edit your posts BB code is On Smilies are On [IMG] code is On HTML code is Off Trackbacks are Off Pingbacks are On Refbacks are On Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Turbulence model for low Reynolds number flow?	Nokadu	Main CFD Forum	3	May 26, 2013 11:42
No shock in airfoil 0012 case despite of Mach number exceeds 1	schwermetall	OpenFOAM	53	November 11, 2011 05:00
Boundary conditions low Mach number flow	lost.identity	Main CFD Forum	0	November 28, 2010 04:44
About compressible flow at low mach	hit	Main CFD Forum	2	October 26, 2009 21:21
non-dimensional analysis in Fluent	Endee	FLUENT	8	September 7, 2005 16:16

All times are GMT -4. The time now is 02:05.