A plane-stress damage model for vectran laminated composite

The aim of this paper is to present a plane-stress damage model based on the Classical Lamination Theory (CLT), developed for polymer fibre-based composite. The proposed numerical model utilises a damage mechanics methodology coupled with fracture mechanics to predict composite failure, particularly...

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Bibliographic Details
Main Authors: Abdullah, S. I. B. S., Iannucci, L., Greenhalgh, E. S., Ahmad, Z.
Format: Article
Language:English
Published: Springer Science and Business Media B.V. 2021
Subjects:
Online Access:http://eprints.utm.my/id/eprint/95425/1/Abdullah2021_Article_APlaneStressDamageModelForVec.pdf
http://eprints.utm.my/id/eprint/95425/
http://dx.doi.org/10.1007/s10443-021-09888-w
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