dear all,
please, i have a composite plate with 10 layers and the proporties of a lamina materiel with his fail stress. after that, i was testing loding the plate in the first directon with exceeding the fail stress value (in the same direction : tensile fail stress in the fiber direction)but i...
dear all,
i want know if any one have an idea how to solve this problem.
I have represent a composite plate with ten plys and I have choose the Lamina like type of material for this composite, then I entered the parameters of this material (E1, E2, G12, G23, G13 and ?12) and the fail stress (ten...
dear deyentl,
thx I saw the Abaqus documentation and I want to ask, if any one knw how I can represent and associat the ideal mesh for a composite with several layers (type of matriel is : lamina) on ABAQUS (ie : creat section shell composite or creat a solid layup composite and associat it a 3D...
Dear all
I want to ask, if any one knw how I can represent and associat the ideal mesh for a composite with several layers (type of matriel is : lamina) on ABAQUS (ie : creat section shell composite or creat a solid layup composite and associat it a 3D stress or continuum shell mesh.
Any idea...
from the module visialization choose: XY data odb field output choose your output variables (example S11, E11) edit your selection (example for an unique nodal) from the part then you will have S11 v. time and E11 v. time,
then in the same selection you can have stress vs strain by choosing: XY...
Hi, please i want to ask how can i represent a composite with 24 layers on abaqus?
When i draw a part(solid deformable with 24 cell paritions) and i associate the properties of a lamina for evry parition with a mesh 3d stress (Hex structured), there will be always the same error "lamina may...
