kribri
Materials
- Feb 17, 2009
- 20
Hi,
I hope someone can help me with this.
I'm analysing Monolithic glass vs Laminated glass.
I'm looking at a window of the size 800x1600mm.
The monolithic is 8mm thick.
The laminate consists of glass faces and is glued together with PVB. The laminate is 4+0.76+4mm.
Isotropic Glass material properties are: E=70GPa, v=0.23
Isotropic PVB material properties are: E=3.78MPA, v=0.49
When modelling this with shell elements (composite layup) in Abaqus the results does not make sense. (I ran a test where the monolithic window was stiffer than the laminate with double the thickness)
For the shell model elements I understand that the elements use first order shear deformation theory for transverse shear deformation. This assumes that plane sections remain plane, but can rotate relative to the shell surface. The shear stiffness is adjusted to compensate for the fact that the real deformation violates this assumption, but the adjustment is approximate. It is claimed to work for normal lay-ups, including sandwich lay-ups, but I have clearly gone far beyond the limits of validity of the procedure used - there is simply far too much shear deformation concentrated into the thin adhesive layer.
Any suggestions on how this can be modelled? Either as solid or as shell?
kind regards
Krish
I hope someone can help me with this.
I'm analysing Monolithic glass vs Laminated glass.
I'm looking at a window of the size 800x1600mm.
The monolithic is 8mm thick.
The laminate consists of glass faces and is glued together with PVB. The laminate is 4+0.76+4mm.
Isotropic Glass material properties are: E=70GPa, v=0.23
Isotropic PVB material properties are: E=3.78MPA, v=0.49
When modelling this with shell elements (composite layup) in Abaqus the results does not make sense. (I ran a test where the monolithic window was stiffer than the laminate with double the thickness)
For the shell model elements I understand that the elements use first order shear deformation theory for transverse shear deformation. This assumes that plane sections remain plane, but can rotate relative to the shell surface. The shear stiffness is adjusted to compensate for the fact that the real deformation violates this assumption, but the adjustment is approximate. It is claimed to work for normal lay-ups, including sandwich lay-ups, but I have clearly gone far beyond the limits of validity of the procedure used - there is simply far too much shear deformation concentrated into the thin adhesive layer.
Any suggestions on how this can be modelled? Either as solid or as shell?
kind regards
Krish