ConwaysGlider
Structural
- Sep 23, 2015
- 2
Hello,
I am using Abaqus to analyze I beams (with shell elements), for various load cases. I have some problems with applying end moments. Until now, I have applied shell edge loads at the end of the beam with a linear stress distribution (along the height of the profile) in order to simulate the application of a bending moment. This worked quite well but is not exact enough, since after yielding, the stress distribution is no longer linear. I have also tried to apply a constant shell edge load (compression on one half, tension on the other) in order to simulate the fully plastic distribution of stresses. I am using a Riks step because I am interested in buckling limit loads, taking into account plasticity, etc.
Technically, I think it may be possible to add a stiff end plate of some sorts and apply the end moments through an eccentricity of applied loads, however I would prefer not to do this, since I am using Python scripts due to the large number of simulations and this would complicate things quite a bit.
Would anyone have a suggestion on how to apply an end moment, in this type of case? I have tried a bit to apply BC rotations at the end and I have also tried using a reference point, but with no success.
Any help would be much appreciated. Thanks in advance,
Cristi
I am using Abaqus to analyze I beams (with shell elements), for various load cases. I have some problems with applying end moments. Until now, I have applied shell edge loads at the end of the beam with a linear stress distribution (along the height of the profile) in order to simulate the application of a bending moment. This worked quite well but is not exact enough, since after yielding, the stress distribution is no longer linear. I have also tried to apply a constant shell edge load (compression on one half, tension on the other) in order to simulate the fully plastic distribution of stresses. I am using a Riks step because I am interested in buckling limit loads, taking into account plasticity, etc.
Technically, I think it may be possible to add a stiff end plate of some sorts and apply the end moments through an eccentricity of applied loads, however I would prefer not to do this, since I am using Python scripts due to the large number of simulations and this would complicate things quite a bit.
Would anyone have a suggestion on how to apply an end moment, in this type of case? I have tried a bit to apply BC rotations at the end and I have also tried using a reference point, but with no success.
Any help would be much appreciated. Thanks in advance,
Cristi