|
[Sponsors] | |||||
|
|
|
#1 |
|
New Member
anonymous
Join Date: Dec 2012
Posts: 3
Rep Power: 2 ![]() |
I am modeling a NACA 0012 in 2D. I have drawn the aerofoil and the freestream box in NX and imported the CAD in. I then set everything up and I have set up two monitors for Cl and Cd in order to compare them to experimental data.
The Cl I have is around 1.2 which is a little high but the Cd i have is -3 and should be around 0.2. I have no idea why this is. I have set the reference values correctly I think in the monitor section (1.177 for density ref pressure is 101325 velocity is 6.943 force option is pressure +shear and the direction is set to components 0.9848,0.1736,0 as the aerofoil is simulated to be at 10 degrees. I have been looking for ages as to why the drag might be so high as I cant see anything wrong. any throughts? |
|
|
|
|
|
|
|
|
#2 |
|
Member
John
Join Date: Aug 2009
Posts: 93
Rep Power: 5 ![]() |
You should resolve forces in the streamwise(drag) and normal(lift) directions since your freestream is at an alpha.
|
|
|
|
|
|
|
|
|
#3 |
|
New Member
Niaz Ali Ahmed
Join Date: Jun 2010
Posts: 13
Rep Power: 4 ![]() |
Hi try choosing Standard K-Epsilon Low Re with adequate mesh resolution near the wall...
|
|
|
|
|
|
![]() |
| Tags |
| coefficient, drag, monitor, naca 0012 |
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| drag coeff to high - kOmegaSST turbulence model | RugbyGandalf | OpenFOAM | 5 | February 22, 2011 02:35 |
| high amount of drag coefficient. about 15????Is it okay? | ndabir | CFX | 3 | February 1, 2010 17:10 |
| High drag coeff. estimated by Gambit+fluent | M. suuri | FLUENT | 6 | November 6, 2006 08:02 |
| high drag value | sulfi | FLUENT | 1 | April 8, 2005 19:27 |
| Multicomponent fluid | Andrea | CFX | 2 | October 11, 2004 05:12 |