CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > CFX

Solver Failure due to unrealistic high Mach number

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   March 13, 2009, 03:29
Default Solver Failure due to unrealistic high Mach number
  #1
Andreas
Guest
 
Posts: n/a
Hello everyone,

I have a strange problem. I am simulating slightly different geometries using pretty much the same unstructured mesh every time. Especially the wall distances are the same in every mesh, first node about y+ = 50 to 100 - just as required by the CFX-manual. My inflow air velocity is 36 m/s, so it is far from being transonic.

Strange thing is: Sometimes the solver will crash due to an Mach number that tends towards the hundreds. I could localize the region of the high velocities to a region close to a wall where separation most likely occurs.

Does anyone has an idea where this problem comes from and it can be solved? I am using SBF=0.75 and a physical timestep that is about five times higher than the automatically calculated one (in order to avoid the simulation of transient osciallations). The solver precision is set on double. The element quality as calculated by ICEM should be alright - worst element about 0.01, but only a handful maximum. And as I said: This setup works in 19 of 20 cases!!!

I am grateful for any ideas, maybe there is a expert parameter that could solve my problem?

Regards,

Andy
  Reply With Quote

Old   March 13, 2009, 05:58
Default Re: Solver Failure due to unrealistic high Mach nu
  #2
Bart Prast
Guest
 
Posts: n/a
Your time scale is too large. Start with local time step factor. And use the high resolution schema with automatic blend factor (but this is your choice ofcourse). The fact that your setup works in 19 of 20 cases means your were lucky (just inside stability range of your code/problem).

Success,

Bart
  Reply With Quote

Reply


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


Similar Threads
Thread Thread Starter Forum Replies Last Post
[snappyHexMesh] snappyHexMesh won't work - zeros everywhere! sc298 OpenFOAM Meshing & Mesh Conversion 2 March 27, 2011 21:11
[snappyHexMesh] snappyHexMesh aborting Tobi OpenFOAM Meshing & Mesh Conversion 0 November 10, 2010 03:23
Can a compressible solver solve incompressible ? jinwon park Main CFD Forum 17 December 13, 2007 05:00
High Mach number flows Riaan FLUENT 9 May 7, 2005 15:49
High mach number flow Logesh Main CFD Forum 12 June 30, 2003 09:43


All times are GMT -4. The time now is 13:51.