|
[Sponsors] |
February 2, 2005, 23:58 |
Lift-to-Drag ratio for Aircraft
|
#1 |
Guest
Posts: n/a
|
Hi All,
Please tell me how calculat lift to drag ratio for aircraft on Fluent. Cheers, Toshi |
|
February 15, 2005, 05:16 |
Re: Lift-to-Drag ratio for Aircraft
|
#2 |
Guest
Posts: n/a
|
the easyiest thing to do is you edit your output lift and drag files with excel and calculate there the finesse.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
pressure eq. "converges" after few time steps | maddalena | OpenFOAM Running, Solving & CFD | 69 | July 21, 2011 07:42 |
Lift and Drag Monitor Point Values Converging to Zero | Josh | CFX | 24 | May 9, 2011 10:38 |
how to caculate lift drag ratio in fluent | jouven | FLUENT | 2 | June 16, 2009 20:05 |
Correct lift but wrong pressure drag - possible? | zx | Main CFD Forum | 4 | July 27, 2007 23:38 |
range of lift to drag ratio in airfiols | chillaks | Main CFD Forum | 3 | December 26, 2005 01:47 |