anto_772
Mechanical
- Jul 19, 2018
- 7
Hi guys, I'm intending to carry out a simulation of an lightning impact over a compoiste plate using Abaqus (Coupled thermal-electrical analysis). First of all I put here the finite element model and boundary conditions:
-Specimen has 100mm width and 150mm lenght. Thickness of 4mm.
- Composite laminate are 32-ply quasi-isotropic [+45/0/-45/90]4s. Thickness of each ply 0.125mm
- Each lamina of composite laminate divided using 8-node isoparametric solid element to the thickness direction up to 1,5mm(0,0125mm x 12 ply).
- Orthotopic material properties calculated using rule of mixture were used for the elements deeper than 1,5mm to reduce number of elements.
Boundary conditions:
- Electrical potential at the bottom assumed to be zero (copper plate under the bottom of a specimen was electrically grounded)
- Eletrical potencial at side surfaces are zero
- Thermal radiation given fot upper and sides surfaces. Bottom surface adiabatic (Emissivity = 0.9 Environment Temperature =25ºC)
- Convective heat transfer around specimen ignored because extremely short period.
Loads:
- Impulse current of 40kA in the middle of the plate
The initial time increment was 0.01µs; the automatic time increment function provided from Abaqus was used. The resultant time increment was 0.001-0.1µs. After an impulse current test,no electrical load exist. Therefore general transient heat transfer analysis was conducted to save calculation time. The time increment was 0.1s; the calculation was terminated at 10s after lightning.
I want to reproduce this simulation with Abaqus. I create a solid part and create 12 sections for the first 12 plies. Then I create a composite Layup(solid) for the first 12 plies and I asign an isotropic material properties for the section below(deeper than 1,5 mm). I want help for introduce theses BC and if I'm modelling good the composite plate.
Thank you.
-Specimen has 100mm width and 150mm lenght. Thickness of 4mm.
- Composite laminate are 32-ply quasi-isotropic [+45/0/-45/90]4s. Thickness of each ply 0.125mm
- Each lamina of composite laminate divided using 8-node isoparametric solid element to the thickness direction up to 1,5mm(0,0125mm x 12 ply).
- Orthotopic material properties calculated using rule of mixture were used for the elements deeper than 1,5mm to reduce number of elements.
Boundary conditions:
- Electrical potential at the bottom assumed to be zero (copper plate under the bottom of a specimen was electrically grounded)
- Eletrical potencial at side surfaces are zero
- Thermal radiation given fot upper and sides surfaces. Bottom surface adiabatic (Emissivity = 0.9 Environment Temperature =25ºC)
- Convective heat transfer around specimen ignored because extremely short period.
Loads:
- Impulse current of 40kA in the middle of the plate
The initial time increment was 0.01µs; the automatic time increment function provided from Abaqus was used. The resultant time increment was 0.001-0.1µs. After an impulse current test,no electrical load exist. Therefore general transient heat transfer analysis was conducted to save calculation time. The time increment was 0.1s; the calculation was terminated at 10s after lightning.
I want to reproduce this simulation with Abaqus. I create a solid part and create 12 sections for the first 12 plies. Then I create a composite Layup(solid) for the first 12 plies and I asign an isotropic material properties for the section below(deeper than 1,5 mm). I want help for introduce theses BC and if I'm modelling good the composite plate.
Thank you.