A comprehensive study on the buckling behaviour of woven composite plates with major aerospace cutouts under uniaxial loading

Current research paper presents a comprehensive study based on Finite Element Method (FEM) to understand the effect of cutout shape and area on the buckling behaviour of E-glass composite plates. Considered plate has a dimension of 150 mm × 75mm × 3mm where loading edges are simple supported (shorte...

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Bibliographic Details
Main Author: S. B. Rayhan
Format: Article
Language:English
Published: Universiti Malaysia Pahang Publishing 2019-06-01
Series:Journal of Mechanical Engineering and Sciences
Subjects:
Online Access:https://journal.ump.edu.my/jmes/article/view/446