This example problem demonstrates the use of solid-shell element technology to model a layered-composite structure. The problem simulates interface delamination through the debonding capability of contact elements.
The following features and capabilities are highlighted:
Use of the solid-shell element technology to model layered composites
Bonded contact with a cohesive zone model to simulate delamination (also known as debonding)
Use of constraint equations to model periodic symmetry
The following topics are available:
You can also perform this example analysis entirely in the Ansys Mechanical Application. For more information, see Delamination of a Stiffened Composite Panel Under a Compressive Load in the Mechanical Technology Showcase: Example Problems.