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

naca2412 analysis

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

Reply
 
LinkBack Thread Tools Display Modes
Old   September 1, 2009, 18:59
Default naca2412 analysis
  #1
New Member
 
gaurav
Join Date: May 2009
Posts: 9
Rep Power: 7
gaurav is on a distinguished road
Hi,
I am trying to analyze a naca2412 airfoil in wind-us and trying to plot "lift" residuals using "resplt" but when I do so i get a constant value of zero after almost 30000 iterations. I am using an anngle of attack of 12 degrees and a free stream mach number of 0.2. I am unable to figure out where I am going wrong.

Thanks
gaurav 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
What exactly is a sensitivity analysis? Josh CFX 3 August 19, 2009 09:18
Fan Boundary conditions with external analysis Rob FloEFD, FloWorks & FloTHERM 1 February 10, 2009 00:04
FSI Transient Thermal Analysis Abduri CFX 0 December 8, 2008 20:00
Questions on Analysis Controls and Runtime Control Arnab CD-adapco 1 October 26, 2004 09:47
Short Course: Computational Thermal Analysis Dean S. Schrage Main CFD Forum 11 September 27, 2000 17:46


All times are GMT -4. The time now is 04:33.