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

Flow analysis in a Convergent-Divergent Nozzle (URGENT!)

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

Reply
 
LinkBack Thread Tools Display Modes
Old   June 16, 2009, 04:00
Exclamation Problem was Solved.
  #1
New Member
 
Aerospace Engineer
Join Date: Jun 2009
Posts: 6
Rep Power: 8
hasan_hzl is on a distinguished road
Problem was solved.

Last edited by hasan_hzl; June 26, 2009 at 04:03.
hasan_hzl is offline   Reply With Quote

Old   June 17, 2009, 11:51
Default
  #2
New Member
 
Aerospace Engineer
Join Date: Jun 2009
Posts: 6
Rep Power: 8
hasan_hzl is on a distinguished road
I tried to solve it give an error of "floating point". I think it is because of big pressure difference btw inlet and outlet. Now what do I have to do? Please help me
hasan_hzl is offline   Reply With Quote

Old   June 30, 2009, 00:46
Default floating point
  #3
New Member
 
Sudharshani
Join Date: Jun 2009
Location: Melbourne,Australia
Posts: 16
Rep Power: 8
Sudharshani is on a distinguished road
what is a floating point point?
which software are u using as i am also doing the same problem(supersonic CD nozzle) using ANSYS CFX...just started my project.
how did u designed ur nozzle shape? is it through parameric modeling of a function or do u have fixed data set?
sudhar
Sudharshani 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
Nozzle Flow - Divergence Problem Ijaz FLUENT 9 January 11, 2014 05:36
3D-Simulation of Water Flow From Nozzle into Air Navin Sampath FLOW-3D 2 February 26, 2009 11:46
Coolant flow analysis - IC engine Frank FLUENT 2 May 19, 2002 15:59
Nozzle Flow with shock jim clancy FLUENT 1 December 18, 2001 05:19
Verification of Supersonic Nozzle Flow Ali Khan FLUENT 0 October 12, 2000 07:53


All times are GMT -4. The time now is 02:43.