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

Lift Coefficient Vs. Angle of Attack

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   August 23, 2002, 17:20
Default Lift Coefficient Vs. Angle of Attack
  #1
cfd_pro
Guest
 
Posts: n/a
I need to modify a Lift Coefficient Vs. Angle of Attack chart from Max. Upper Camber of 13.3% to 72%. Any suggestions. Thanks.
  Reply With Quote

Old   August 23, 2002, 18:21
Default Re: Lift Coefficient Vs. Angle of Attack
  #2
Axel Rohde
Guest
 
Posts: n/a
See if DesignFoil from www.dreesecode.com can help.
  Reply With Quote

Reply


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 Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Getting lift force at zero angle of attack Shamoon Jamshed FLUENT 14 September 5, 2012 00:16
when the angle of attack =?, the total lift coefficient begin to decrease suddenly liujmljm Main CFD Forum 6 August 3, 2012 06:46
[Netgen] Import netgen mesh to OpenFOAM hsieh OpenFOAM Meshing & Mesh Conversion 32 September 13, 2011 06:50
Automotive test case vinz OpenFOAM Running, Solving & CFD 98 October 27, 2008 09:43
Plotting of lift coefficient vs angle of attack?? John Main CFD Forum 1 August 18, 2003 10:31


All times are GMT -4. The time now is 02:55.