CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > FloEFD, FloWorks & FloTHERM

Results comparison problems

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

Reply
 
LinkBack Thread Tools Display Modes
Old   March 15, 2011, 04:58
Default Results comparison problems
  #1
New Member
 
koay kheng kean
Join Date: Mar 2011
Posts: 3
Rep Power: 6
ken87 is on a distinguished road
hi all, to studies of performance analysis on a NACA profile (lift and coefficient against AOA) is that possible to compare theoretical results, experimental results and simulation results by cosmofloworks?? can this 3 method get the same results (i have do it but i cannot get it, any suggestion?)? between how can i get the correct the theoretical results for NACA 0012 airfoil? and what is the factor that can effect lift and coefficient of NACA 0012 airfoil? anyone pls help regarding this problem....thanks a lots..
ken87 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
Convergence problems post impact[URGENT help needed] alastormoody11 STAR-CCM+ 1 March 22, 2011 09:52
problems with the stability of results ingeniero_82 CFX 3 March 18, 2011 07:19
problems viewing results with VNC Ralf Schmidt FLUENT 3 February 1, 2006 02:40
results comparison guang ai CD-adapco 2 March 22, 2003 07:59
benchmark results stefan CD-adapco 3 September 10, 2001 09:48


All times are GMT -4. The time now is 10:24.