|
[Sponsors] |
Questions about ReTheta & Gamma setup in airfoil calculation |
![]() |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
![]() |
![]() |
#1 |
New Member
kevin
Join Date: Nov 2018
Posts: 6
Rep Power: 8 ![]() |
Dear all,
I am calculating the NACA 64312 airfoil. The freestream velocity is 50m/s, the turbulent intensity is 1%. I use the Komega SSTLM transition model for calculation and my setup for U, k and Rethetat are shown in the attached figures. Unfortunately, the calculation fails. There may be some errors in my setup. Could anyone help me? Thank you. u.JPG k.JPG ReThetat.JPG |
|
![]() |
![]() |
![]() |
![]() |
#2 |
New Member
Abdelrahman Kamaleldin
Join Date: Jan 2021
Posts: 6
Rep Power: 6 ![]() |
Hello Sir,
Did you solve the issue, I am experiencing similar issue today. Thanks |
|
![]() |
![]() |
![]() |
![]() |
#3 | |
New Member
Dipanshu Pant
Join Date: Mar 2022
Posts: 1
Rep Power: 0 ![]() |
Quote:
|
||
![]() |
![]() |
![]() |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Questions on Boundary Layer Spring Method for 3D Calculation | didiean | FLUENT | 15 | December 18, 2014 22:09 |
Questions about pressure calculation on buoyancy flow(thermal stratified flow) | hwangpo | CFX | 5 | March 19, 2014 20:45 |
dynamicMesh case setup simpleton questions | tellico | OpenFOAM Pre-Processing | 2 | January 17, 2014 13:41 |
Gamma - ReTheta Transition Model | badger1 | STAR-CCM+ | 0 | February 10, 2013 10:34 |
[FloWorks] Request advice for an airfoil calculation problem | Bogey Jammer | Main CFD Forum | 0 | September 29, 2009 18:06 |