 |
 |
 |
|
|
|
[Sponsors] | ||||
February 12, 1999, 12:46
|
NACA 6A-series airfoil data
|
#1 |
|
Guest
Posts: n/a
|
I'am trying to test a 2D potential flow code over NACA airfoils, but I don't have analytical solutions nor any experimental data of the airfoil ordinates and the corresponding pressure distribution, if anyone can provide me with these data or knows where I can find them I'll be very gratful.
Thanks. |
|
|
||
|
February 12, 1999, 14:35
|
Re: NACA 6A-series airfoil data
|
#2 |
|
Guest
Posts: n/a
|
Start at http://amber.aae.uiuc.edu/~m-selig/ads.html and good luck. Note NVFoil there, it might be useful.
If all you need is to check a potential flow solver, why NACA airfoils? Joukowskii will do just as well. |
|
|
|
||
|
February 15, 1999, 06:25
|
Re: NACA 6A-series airfoil data
|
#3 |
|
Guest
Posts: n/a
|
hi Shereef, I've done some simulation on 3D-code upon the NACA65 ... Profile. If you can use my results please let me know.
|
|
|
|
||
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Lift and Drag Coefficient data for NACA 2412 Airfoil | mahbub03 | Main CFD Forum | 22 | May 25, 2014 16:39 |
| Symmetric NACA Airfoil Lift and Drag Data | jrider22 | Main CFD Forum | 3 | April 15, 2010 05:59 |
| NACA 0012 data | pixie | Main CFD Forum | 3 | August 5, 2009 04:01 |
| How to update polyPatchbs localPoints | liu | OpenFOAM Running, Solving & CFD | 6 | December 30, 2005 18:27 |
| About low Reynolds number airfoil experiment data. | zqnwpu | Main CFD Forum | 5 | December 25, 2004 04:52 |
Linear Mode
