Large Deflection of Laminated Circular Plates With Clamped Edge and Uniform Loading

Authors

• Qiuhua Li, Wright State University
• Junghsen Lieh, Wright State University - Main CampusFollow
• A. Mayer, Wright Patterson AFB

Document Type

Article

Publication Date

2-1-2005

Find this in a Library

Catalog Record

Abstract

An analytical nonlinear elasticity theory was developed and used to predict large deflection of laminated circular plates with clamped boundaries. For comparison purposes, numerical solutions were obtained with a finite element software, ANSYS. Experiments were carried out using a fibre optical displacement sensor to validate the theory. Results from these three approaches show agreement.

Repository Citation

Li, Q., Lieh, J., & Mayer, A. (2005). Large Deflection of Laminated Circular Plates With Clamped Edge and Uniform Loading. Proceedings of the Institution of Mechanical Engineers, Part E: Journal of Process Mechanical Engineering, 219 (1), 83-88.
https://corescholar.libraries.wright.edu/mme/718

DOI

10.1243/095440805X8647