Lecture

Composite Laminate Analysis

Description

This lecture covers the Classical Laminate Theory, which provides a method to compute stresses and displacements in laminated composites. It explains the steps to define reduced stiffness matrices for each ply, transform ply stiffness matrices, compute mid-plane strain and curvature, find stresses in each ply, and analyze stresses in global and local coordinates.

About this result
This page is automatically generated and may contain information that is not correct, complete, up-to-date, or relevant to your search query. The same applies to every other page on this website. Please make sure to verify the information with EPFL's official sources.