CFD Online Logo CFD Online URL
Home > Forums > FLUENT

Lift coefficient

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

LinkBack Thread Tools Display Modes
Old   November 26, 2005, 01:07
Default Lift coefficient
Man Hwan
Posts: n/a
I'm calculating airfoil flow. and I set airfoil's angle of attack zero. and I set flow's angle of attack 7 degree. While doing this calculation, Is Cd,Cl right? Do I convert Cd,Cl? or Just Do I use original Cd,Cl?
  Reply With Quote

Old   November 26, 2005, 02:57
Default Re: Lift coefficient
Posts: n/a
Hi Man, The direction of lift and drag is given by the flow direction, so u have to change. hope this helps bharat
  Reply With Quote


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
Lift coefficient in Eulerian multiphase model hennas FLUENT 1 July 4, 2011 16:50
Automotive test case vinz OpenFOAM Running, Solving & CFD 98 October 27, 2008 09:43
Zero Coefficient of Lift Problem MH FLUENT 0 February 25, 2007 12:48
Lift force or coefficient of lift Rola FLUENT 1 November 12, 2006 14:29
Help needed - lift coefficient on front/rear axle Jan Jagrik FLUENT 0 September 21, 2000 10:21

All times are GMT -4. The time now is 22:01.