CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > FLUENT

aerospike simulation at mach number 6 using Fluent 6.3

Register Blogs Members List Search Today's Posts Mark Forums Read

Reply
 
LinkBack Thread Tools Display Modes
Old   September 27, 2014, 09:33
Default aerospike simulation at mach number 6 using Fluent 6.3
  #1
New Member
 
hesam
Join Date: Apr 2014
Posts: 2
Rep Power: 0
hesam.g is on a distinguished road
Dear All..
I am trying to do a hypersonic flow simulation over a spiked blunt body at mach 6 using fluent 6.3
In my case, I use first order upwind scheme and get a very well converged solution. however, when I switch to second
order upwind scheme, totally diverge
Any one has some suggestion to resolve this problem?
hesam.g is offline   Reply With Quote

Reply

Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
simpleFoam parallel AndrewMortimer OpenFOAM Running, Solving & CFD 12 August 7, 2015 18:45
Decomposing meshes Tobi OpenFOAM Pre-Processing 1 September 9, 2014 05:30
Fully Expanded Jet Mach Number. oe_jet Main CFD Forum 0 June 28, 2010 11:40
HOw to match the Mach number in FLUENT?? applemango Main CFD Forum 0 April 20, 2010 06:34
BlockMeshmergePatchPairs hjasak OpenFOAM Native Meshers: blockMesh 11 August 15, 2008 07:36


All times are GMT -4. The time now is 11:35.