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Airfoil Optimization With ANSYS Adjoint Solver

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Old   September 21, 2017, 12:12
Default Airfoil Optimization With ANSYS Adjoint Solver
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I am working on a simple airfoil optimization project and using ANSYS Smart Shape Optimization tool with ANSYS Adjoint Solver. How can I get the new (optimized) airfoil shape coordinates to feed other softwares? I don't need to know mesh points just the shape is enough.
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Old   September 22, 2017, 03:28
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You may try to use profile to extract mesh points.

File->write->profile->select your curve/surface-> select any value (doesn't matter which you choose, because you need coordinates) -> write

In file you will get the 3 lists of coordinates (x,y,z) and list of value, you'd chosen.

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Old   September 22, 2017, 11:48
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Quote:
Originally Posted by AlexanderZ View Post
You may try to use profile to extract mesh points.

File->write->profile->select your curve/surface-> select any value (doesn't matter which you choose, because you need coordinates) -> write

In file you will get the 3 lists of coordinates (x,y,z) and list of value, you'd chosen.

Best regards
Dear AlexanderZ

It worked for me! Thank you very much sir!
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Old   July 24, 2018, 10:52
Default Airfoil shape optimization using adjoint solver
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Quote:
Originally Posted by Nemo Sanchez View Post
Dear AlexanderZ

It worked for me! Thank you very much sir!
Hi nemo, im just a beginner .ive been working on a similar project for awhile, and right now im trying to read as much as i can. I want to know how you ended the optimisation process. It was suggested that I use a script. But ive no experience using one. Did you use any other method? Thanks in advance. Any help would be appreciated.
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