|
[Sponsors] |
October 8, 2005, 05:40 |
Hi guys thanks for all the hin
|
#1 |
Member
Muzio Grilli
Join Date: Mar 2009
Posts: 36
Rep Power: 17 |
Hi guys thanks for all the hints you gave me,now i can run rhoSimpleFoam solver and it gives good results, but now i have a new problem.
I'm triyng to test OpenFoam comparing the results it gives in naca0012 profile analisys, i need to calculate lift and drag coefficients but for the drag coefficient it always gives me zero. When i run the application it needs transport properties so i insert the file in the constant directory maybe i need to specify some more files? So i decided to visualize stressComponents but when i run this application it says that there is a dimensional difference between the two members of the equation. Someone can give me some hints? |
|
October 10, 2005, 05:42 |
Probably the liftDrag app does
|
#2 |
Senior Member
Mattijs Janssens
Join Date: Mar 2009
Posts: 1,419
Rep Power: 26 |
Probably the liftDrag app does not pick up your reference length and area correctly. You might need to have a look at the application itself and change its calculation.
|
|
October 14, 2005, 06:49 |
I Mattijs i looked at the appl
|
#3 |
Member
Muzio Grilli
Join Date: Mar 2009
Posts: 36
Rep Power: 17 |
I Mattijs i looked at the application and i saw that if i calculate the value
(pressureCoeff + viscousCoeff) & flowDirection) two times before the return it gives a drag coefficient different from zero(I don't know if it is good or not but it's a value). otherwise it gives a value that seems to be casual |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Lift & Drag | John | FLUENT | 4 | May 3, 2007 06:57 |
Lift and Drag | Pedro Lopes | CFX | 1 | February 19, 2007 09:18 |
Lift and drag | daniel | CFX | 1 | March 27, 2006 11:14 |
Drag and Lift | Daniel Fisher | Phoenics | 2 | April 8, 2005 04:51 |
Lift and drag | Karim Ozar | Main CFD Forum | 4 | March 9, 2000 03:35 |