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Boundary Load Change Having No Effect.
Posted 24.11.2015, 13:07 GMT-5 Geometry, Structural Mechanics Version 5.1 4 Replies
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Hi there,
I am new to COMSOL and still learning it's functionality. I am trying to apply a strain on the 4 fan edges (boundaries 13,14,18,20,29,30,43,44) of my structure and view it's resulting von Mises stress in the centre.
My problem is that no matter what value i enter as the boundary load, the resulting structure is always stretched by the same amount (20 microns) which is not correct. Any thoughts on what i am doing wrong would be greatly appreciated.
(As added information.... my goal is to simulate a 0.2% biaxial strain on the whole structure and view the von Mises stress profile in the centre of the structure.)
I am new to COMSOL and still learning it's functionality. I am trying to apply a strain on the 4 fan edges (boundaries 13,14,18,20,29,30,43,44) of my structure and view it's resulting von Mises stress in the centre.
My problem is that no matter what value i enter as the boundary load, the resulting structure is always stretched by the same amount (20 microns) which is not correct. Any thoughts on what i am doing wrong would be greatly appreciated.
(As added information.... my goal is to simulate a 0.2% biaxial strain on the whole structure and view the von Mises stress profile in the centre of the structure.)
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4 Replies Last Post 24.11.2015, 14:25 GMT-5