|
[Sponsors] |
Problem reaching lift and drag coefficients on NACA0012 with Spalart-Allmaras Model |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
June 8, 2024, 13:57 |
Problem reaching lift and drag coefficients on NACA0012 with Spalart-Allmaras Model
|
#1 |
New Member
Manuel Grosso Rodríguez
Join Date: Apr 2024
Posts: 2
Rep Power: 0 |
Hello everyone. I am doing my final degree project in OpenFOAM v8.
My project is about studying how a 2D fish (NACA0012) is affected by a perturbed waters at high reynolds (Re=6*10^6). In order to do this I created a mesh following the youtube tutorial of Sebastiano Stipa https://www.youtube.com/watch?v=72RvIkETWLg&t=6s. Now I have done three meshes: the first one is as the video, very coarse, the second one I doubled the cells and also the zgrading; the third one, has doubled the cells and zgrading of the middle mesh. Then in order to corroborate if the mesh is alright I contrasted with NASA research about 2D simulation on NACA0012 (https://turbmodels.larc.nasa.gov/naca0012_val_sa.html). After a lot simulations I have finally get to a CD=0.0085 if I put leadgrading=0.000001 Then I changed the U vector to have a velocity field of 10º, but I cannot match the data of NASA. So I will leave my middle mesh folder so anyone can investigate; I have not included the cylinder because that's the next step. So if you are going to try, just do./Allrun or blockMesh; extrudeMesh and then simpleFoam. (The folder is prepared to run for U=51 m/s alpha=0º) (u must change the U file to match the data here https://www.openfoam.com/documentati...irfoil-2d.html) Last edited by manuel.grosso; June 8, 2024 at 14:08. Reason: Did not attach the folder |
|
Tags |
spalart-all |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Residual fluctuations and inconsistent lift and drag coefficients in Fluent | tr.goktug.yilmaz | FLUENT | 2 | July 2, 2024 22:24 |
Calculation of lift and drag coefficients on airfoil | CoolHersheys | OpenFOAM Post-Processing | 5 | September 27, 2021 07:04 |
How to not overwrite drag and lift coefficients after a simulation | Giovanni Trovato | FLUENT | 1 | August 1, 2018 01:31 |
Lift and drag coefficients of the NACA 0018 | Volodymyr | CONVERGE | 4 | September 22, 2017 18:52 |
wrong SU2 calculation for lift and drag coefficient for NAC4421 | mechy | SU2 | 7 | January 9, 2017 06:18 |