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June 15, 2018, 05:33 |
SU2 AD solver blowing up
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#1 |
New Member
Join Date: Jun 2017
Posts: 19
Rep Power: 9 |
Hi
I am running the AD solver in RANS mode to compute the drag sensitivities of onera M6 wing. I have validated the case given in https://su2code.github.io/tutorials/...ined_NACA0012/ for the naca0012 airfoil. For the onera case validation I am using the grid provided in the testcase suite https://su2code.github.io/tutorials/Turbulent_ONERAM6/ However when I run the case the adjoint solver blows up. I have tried many options like changing the cost functional, reducing the CFL for the adjoint solver, changing the discretization but none seems to work. I am hereby attaching the cfg file I have used for the latest computation(Had to change the extension to .txt). Any insights will be highly appreciated. Regards |
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June 29, 2018, 07:31 |
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#2 |
Super Moderator
Tim Albring
Join Date: Sep 2015
Posts: 195
Rep Power: 11 |
I just tested it with the files provided in the tutorial and it works for me.
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July 2, 2018, 00:44 |
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#3 |
New Member
Join Date: Jun 2017
Posts: 19
Rep Power: 9 |
Thanks,
That is surprising! Can you please share the .cfg file details..or is it the same file as the one I shared? regards |
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July 3, 2018, 06:57 |
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#4 |
Super Moderator
Tim Albring
Join Date: Sep 2015
Posts: 195
Rep Power: 11 |
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July 3, 2018, 08:09 |
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#5 |
New Member
Join Date: Jun 2017
Posts: 19
Rep Power: 9 |
Absolutely fine!..we get the results of the tutorial gives for the continious adjoints. Only having trouble with the discrete adjoints. Please do run the discrete_adjoint.py with the setting given in the .cfg file I have posted you would notice a blow up of the adjoint solver..
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Tags |
onera m6, su2 ad |
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