Geometry
Dimensions
Laminate
| # | Material | Thickness | Angle [°] |
|---|
Custom materials
Add an orthotropic or isotropic material, then assign it to one or more layers.
Modes
Load
More load options
Profiles at
Click or drag on the plate map to move the evaluation point.
Theory
More options
Transverse stresses from
ED3
Plots
Explore Structural Theories
Reference model
Run the same case with the CUF option selected below. The main results above are left unchanged.
Expansion Function
Legendre
Expansion Function
Taylor
Run the theory study to compute additional shear correction factors and response plots.
Explore Transverse Normal Stretching Influence
Constant-w approximation
u and v follow the selected structural theory. C33 is multiplied by 104, suppressing transverse normal stretching: εzz ≈ 0.
Expansion Function
Legendre
Expansion Function
Taylor
Select a theory and run the study.