Stress constrained Optimization
Dear all,
I would like to do a stress constrained optimization on a small aircraft wing.
My objective: Minimize the volume
Constraint: Max von-Mises stress < yield stress of the material.
Can you let me know how to formulate this in Optistruct?
I got the following error in my first try:
*** ERROR # 1812 ***
Multiple responses are assigned to the DESOBJ objective function.
A MINMAX/MAXMIN objective function definition with DOBJREF should
be used instead.
Minmax reduces the maximum of a parameters, in this case von-Mises stress can be given. but I want to set a limit for the stress. Can this be done using Optistruct?
Answers
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Hi Suraj,
I missed this post, sorry for that.
What type of optimization are you running.
You can specify stress constraint on DTPL card, if you are running topology optimization.
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Hi Suraj,
Did you solve the problem ? If you solved, Can you explain me how to formulate ?
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