[Drapier]

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