CFD Online URL
[Sponsors]
Home > Forums > FLUENT

how to set lift and drag coefficients in force mon

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

Reply
 
LinkBack Thread Tools Display Modes
Old   November 16, 2008, 21:47
Default how to set lift and drag coefficients in force mon
  #1
alagesanj
Guest
 
Posts: n/a
I am simulating an airfoil for finding lift and drag coefficients. As per fluent tutorial for lift coefficient the value to be set in Force moniter is x = sin(theta), y = cos(theta).

But Cornell university tutorial says to use x = -sin(theta), y = cos(theta). I am confused. Which one is correct. Can any one help. Thanks.
  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
Calculation of lift and drag coefficients Prachi CFX 3 August 14, 2007 15:05
Lift and Drag Coefficients xdm CD-adapco 7 April 8, 2007 18:55
airfoil: drag and lift coefficients Pedro Clode FLUENT 1 January 1, 2007 13:44
Lift and Drag Coefficients Reliability Luis FLUENT 2 December 27, 2005 15:45
pressure. lift and drag coefficients waqar mahboob Main CFD Forum 0 July 25, 1998 04:34


All times are GMT -4. The time now is 08:17.