Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation

Hassan Ijaz, Waqas Saleem, Muhammad Zain-ul-abdein, Aqeel Ahmad Taimoor, Abdullah Salmeen Bin Mahfouz

Research output: Contribution to journalArticlepeer-review

4 Citations (Scopus)
2 Downloads (Pure)

Abstract

Glass fibre-reinforced plastic (GFRP) composite laminates are used in many industries due to their excellent mechanical and thermal properties. However, these materials are prone to the initiation and propagation of delamination crack growth between different plies forming the laminate. The crack propagation may ultimately result in the failure of GFRP laminates as structural parts. In this research, a comprehensive mathematical model is presented to study the delamination crack growth in GFRP composite laminates under fatigue loading. A classical static damage model proposed by Allix and Ladevèze is modified as a fatigue damage model. Subsequently, the model is implemented in commercial finite element software via UMAT subroutine. The results obtained by the finite element simulations verify the experimental findings of Kenane and Benzeggagh for the fatigue crack growth in GFRP composite laminates.
Original languageEnglish
Article number2081785
Number of pages8
JournalInternational Journal of Aerospace Engineering
Volume2018
DOIs
Publication statusPublished - 28 Mar 2018
Externally publishedYes

Bibliographical note

This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Fingerprint

Dive into the research topics of 'Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation'. Together they form a unique fingerprint.

Cite this