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#1 |
New Member
Join Date: Jun 2017
Posts: 19
Rep Power: 8 ![]() |
Hi
I am running the shape_optimization.py for a wing body configuration. I have given a fixed cl. My optimization process stops after the first design cycle. I also tried changing the tolerance parameters, number of iterations but it does not seem to go through. I am attaching a copy of the cfg file. any insights would be valuable. Regards |
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#2 |
Member
Join Date: Mar 2017
Posts: 61
Rep Power: 8 ![]() |
Relaxing your constraints may help you.
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#3 |
New Member
Chenzhou Xu
Join Date: Oct 2018
Posts: 5
Rep Power: 7 ![]() |
You use SU2v5.0.0 version right? If you use this version and use a fixed cl. mode, the CFD direct calculation process won't exit successfully. I met a situation that SU2 process returned error '6', but when i use a fixed aoa mode, the problem is avoided. I assume that this is a bug in SU2v5.0.0. I test SU2v6.2.0, the bug has already been fixed. You can try a newest version.
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