|
[Sponsors] |
![]() |
![]() |
#1 |
Guest
Posts: n/a
|
I have done simulation on 2D airfoil. coefficient of lift and drag are known.Is it possible to compute Torque generated from cl & cd or is there any other option in fluent which calculates torque generated.Also will the same method will be used if we compute for 3D airfoil.
|
|
![]() |
![]() |
![]() |
#2 |
Guest
Posts: n/a
|
In report-force, you have "moments", it is the torque from lift+drag around the point you imput the coordinate.
|
|
![]() |
![]() |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
HELP ( 3D airfoil computation) | shan | FLUENT | 0 | April 3, 2008 08:59 |
Parallel computation | Jonas Pedro Caumo | CFX | 6 | December 19, 2006 14:51 |
computation bug? | Scott | Siemens | 3 | July 21, 2004 09:39 |
Need for help for 3D airfoil computation | D.T. | Main CFD Forum | 0 | May 6, 2003 12:04 |
Steady solutions in Airfoil Computation? | Tyler Sherk | Main CFD Forum | 4 | August 12, 2002 11:08 |