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Shell Edge Load Application on a Plate 1

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FEAMonkey

Aerospace
Nov 17, 2019
15
Hi Everyone,

I have modelled a 3D plate using shell elements in Abaqus. I have applied a fixture to the bottom edge and load on the top edge of the plate. The setup and the result of the analysis:
PLATE_jly83w.png


As you can see, the top edge of the plate where the load is applied is curved in the direction of the load. In reality, the load is applied by a big clamp which pulls the whole edge up. Therefore, in the simulation result my deformed shape should show straight top and bottom edges.
How can I apply the load in the appropriate way?

Thanks for your help.
 
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Create a kinematic coupling on the top edge and apply the load to the reference node of the coupling.
 
You can use kinematic coupling or rigid body constraint to apply this load. Second option might be preferable in this case
 
Thank you for your quick response.

I have applied a rigid body constraint on the top edge with "Pin" region type.
It seems to work well. :)
 
Can someone give me a scientific reason why the maximum stress is lower when the rigid body constraint is applied on the top edge?
 
A view on the right image you've posted should explain that.
 
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