 |
 |
 |
|
|
|
[Sponsors] | ||||
June 26, 2020, 16:23
|
naca0012
|
#1 |
|
New Member
burak
Join Date: Feb 2020
Posts: 6
Rep Power: 6  |
Hi all,
I have been working on Naca 0012 for about two months but the analysis results do not match experimental results at all. In general, my values at 0 degrees angle of attack are normal but I could not reach the results I wanted at 5,10,15 and 20 degrees. I used 3 million Reynold issues and Spalart Allmaras and k-omega SST. Solver is simpleFoam. When the y plus value is generally less than 10, the analysis is not working anyway, residual and force values are diverged. If you have a member with a file already made, can you share it about naca0012? Thank you |
|
|
|
|
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| NACA0012 Dat File | m_ridzon | Main CFD Forum | 3 | June 20, 2018 09:34 |
| Dont find the converge in NACA0012 with structured mesh | ynos | OpenFOAM Running, Solving & CFD | 2 | December 14, 2013 06:03 |
| NACA0012 Data as a function of Re for a VAWT model | psd | Main CFD Forum | 1 | July 31, 2009 22:04 |
| NACA0012 experimental results. | Kyung-Seok, Kim | Main CFD Forum | 0 | March 13, 2006 05:46 |
| I want NACA0012 simulation datas | Santana | Main CFD Forum | 2 | December 28, 2004 11:58 |
Linear Mode
