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Buckling constraints in the wing box optimization problem #347
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Constitutive classes like |
Thanks for the reply, this will help me a lot. Can I ask a few more clarifying questions?
con.setFailureModes( Is this setting not supported in older versions yet?
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Hi @Gittwell, you can either checkout TACS 3.7.2 which is the last release before the mphys wrapper update, but doesn't contain the improvements I added in #319, including the 2 stiffener buckling modes. Or you could checkout the last commit before we updated the mphys wrapper (f3c69ea) which will include the most recent improvements to |
Thanks, I'll try to use version 2.8.0 before mphys update. I think new features are very useful. |
Hello, thanks for your answers, they were really helpful. Could you also clarify for me? Can I use BladeStiffenedShellConstitutive for an isotropic material? I found an example in the tests (https://github.com/smdogroup/tacs/blob/master/tests/constitutive_tests/test_blade_stiffened_shell_constitutive.py), but I want to make sure. |
Yes, isotropic properties should work fine with |
Dears colleagues!
Please tell me, how I can set up optimization with a buckling constraints. I use tacs 3.3.1 and mphys 1.1.0.
I can add KSFailure constraint,but I can't find any information on how to add buckling constraints.
model.add_constraint("tip_shear.ks_vmfailure", lower=0.0, upper=1.0, scaler=1.0
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