|April 29, 2011, 17:46||
Spanwise lift distribution on a wing
Join Date: Jul 2010
Posts: 97Rep Power: 7
I was wondering if anyone knew how to create a lift distribution curve along the span of a wing? I would prefer it in a numerical form so I can export it to excel to compare to other experimental data. The only way I can think to do it is to create tons of sections and integrate the pressure of the section intersections with the wing but this is a lot of work and not as accurate as should be possible.
Also does anybody know how to subtract out the hydrostatic pressure of a "flatwave" from the pressure in ccm+? I ask because I have tried writing a field function that that was the the $pressure-$hydrostaticpressureofflatwave0 and it would not compile.
|Thread||Thread Starter||Forum||Replies||Last Post|
|Spanwise Lift Distribution||Riaan||FLUENT||9||January 13, 2013 15:03|
|Lift distribution||PB4||STAR-CCM+||1||October 28, 2010 06:59|
|Spanwise lift distribution on 3D wing||Bridou||FLUENT||1||August 26, 2007 20:39|
|spanwise lift distribution plot||Vincent||FLUENT||2||May 5, 2006 00:55|
|Lift distribution along wing||nico||FLUENT||2||February 2, 2004 13:21|