isok89
Civil/Environmental
- May 9, 2016
- 37
I have subjected a thin-walled beam to a moment load only by
using references point on both ends (supports).
- Shell elements
- Implicit dynamic solver with quasi-static application
- moment applied at supports
The supports (total cross section EDGES due to shell elements at the supports) are constrained by 'pin nodes'towards the reference points. On these reference points I have applied the support
boundary conditions and the moment
However in results my applied moment does not reduce after failure.I clearly see in the animation (scale factor =1) that the beam completely fails but my applied moment in the results stays the same until the simulation aborts due to extreme deflection.
The beams I use should immediatly fail after reaching ultimate load.
Before I used a three-point bending model and everything worked accordingly (peak ultimate load). Right now I switched to moment loads at the supports and am having this problem.
Any solutions?
using references point on both ends (supports).
- Shell elements
- Implicit dynamic solver with quasi-static application
- moment applied at supports
The supports (total cross section EDGES due to shell elements at the supports) are constrained by 'pin nodes'towards the reference points. On these reference points I have applied the support
boundary conditions and the moment
However in results my applied moment does not reduce after failure.I clearly see in the animation (scale factor =1) that the beam completely fails but my applied moment in the results stays the same until the simulation aborts due to extreme deflection.
The beams I use should immediatly fail after reaching ultimate load.
Before I used a three-point bending model and everything worked accordingly (peak ultimate load). Right now I switched to moment loads at the supports and am having this problem.
Any solutions?