OUTLINE:
- Composite Material (2D Orthotropic) – UD Carbon Fiber
- 9-ply Symmetric Layup (45°/-45°/0°/90°/0°/90°/0°/-45°/45°)
- Laminate Property with Hill Failure Theory
- Meshing – just like standard plate elements
- Material Orientation – the reference angle
- Post Processing – deflection, stress and failure indices