In this subject, Dr. C. Kassapoglou continues the discussion about Classical Laminated Plate theory.
Last time he ended with in-plane laminate behavior, this time the out-of-plane behavior for the case of pure bending and membrane-bending coupling behavior are discussed. He tells how to obtain the equivalent stress-strain relations for a laminate bycombining everything. He then shows what the stiffness matrix should look like for symmetric and balanced laminates and how the elastic constants for a laminates can be obtained.
In the second part of the lecture Dr. C. Kassapoglou talks about the first ply failure criteria and failure prediction in general, followed by the description of ply failure modes. He finishes the course introduction with a review of the most commonly used failure criteria and their relation to experimental results. The final segment covers real world composite structures examples.
Advanced Design and Optimization of Composite Structures I – Week 2
Privacy & Cookies Policy
Necessary cookies are absolutely essential for the website to function properly. This category only includes cookies that ensures basic functionalities and security features of the website. These cookies do not store any personal information.
Any cookies that may not be particularly necessary for the website to function and is used specifically to collect user personal data via analytics, ads, other embedded contents are termed as non-necessary cookies. It is mandatory to procure user consent prior to running these cookies on your website.