|
[Sponsors] |
August 23, 2002, 17:20 |
Lift Coefficient Vs. Angle of Attack
|
#1 |
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.
|
|
August 23, 2002, 18:21 |
Re: Lift Coefficient Vs. Angle of Attack
|
#2 |
Guest
Posts: n/a
|
See if DesignFoil from www.dreesecode.com can help.
|
|
|
|
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 |