|
[Sponsors] |
Simulation of UAV rotor using SU2 rotating frame |
![]() |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
![]() |
![]() |
#1 |
New Member
Arnaud
Join Date: May 2017
Location: France
Posts: 1
Rep Power: 0 ![]() |
Dear SU2 users,
Currently working on a aeroacoustic project of UAV rotor, I'm trying to obtain the aerodynamics performances of the GWS 80*45 rotor to compare the SU2 results with an aerodynamic python code. I have meshed my geometry using Ansys Meshing exported in .cgns I write a .cfg file with the different indications given along the CFD online topics relative to SU2 rotating frame. I lauched several computations with Euler as physical problem, RPM=4000. However the results obtained are quite bad and for the moment I don't really understand why. Moreover, the computation don't go up to the 1000 iterations asked and often stop without writing any solution files. After having check the meshing I think it rather come from my .cfg file (I'm quite a novice in SU2 use ) Do you have any ideas it may come from? You could find here after, a link to my config file and some results obtained with SU2 https://drive.google.com/drive/folde...FE?usp=sharing I thank you in advance for your help Arnaud |
|
![]() |
![]() |
![]() |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
3D Windturbine simulation in SU2 | k.vimalakanthan | SU2 | 15 | October 12, 2023 05:53 |
How to transform data in Cartesian a frame to rotating reference frame? | carl jung | Main CFD Forum | 0 | November 13, 2016 18:35 |
SU2 Rotating reference frame incompressible flow | wgvanveen | SU2 | 0 | November 4, 2015 05:32 |
3D design optimization in a rotating frame? | ITA91 | SU2 Shape Design | 2 | May 20, 2015 10:01 |
Stirred tank with baffles simulation using single rotating reference frame | M.Zhou | FLUENT | 1 | March 5, 2000 15:01 |