Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Investigation of Delamination Suppression in Highly Tapered Composite Laminates
Download
index.pdf
Date
2023-12
Author
Ergin, Fırat
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
105
views
50
downloads
Cite This
The presence of ply termination locations makes tapered composite laminates susceptible to delamination, thereby reducing the overall structural performance. The primary objective of this study is to propose a novel design alternative for highly tapered laminates with the aim of suppressing delamination onset. In situ experiments on dropped ply specimens are conducted to identify the failure mechanisms within ply drop-off regions. Different delamination modes and their dynamic progression in dropped ply specimens are effectively captured through experimental procedures. Material characterization tests for a Glass Fiber Reinforced Polymer (GFRP) and epoxy resin system are conducted to obtain the mechanical properties essential for the development of finite element models. Cohesive zone modeling technique is employed in FE models to predict delamination. Effects of through-thickness compression enhancement of shear properties and modeling details around the resin pocket are also investigated numerically. The finite element models for single-stage ply drop-off region effectively replicated the delamination onset loads and locations observed in the experimental studies. A parametric taper angle study on a single-stage ply drop-off region revealed that an increase in the taper angle significantly decreases the delamination onset load at the beginning of the thin section of the tapered laminate. Building on this finding, the study introduces the variable taper angle design concept. This design aims to delay the thin section delamination in highly tapered laminates by providing a gradual transition in the taper region. The finite element results of the proposed design concept demonstrated that a substantial improvement of nearly 80% on delamination onset load can be achieved through the proper selection of the taper geometry.
Subject Keywords
Tapered Laminates
,
Delamination Suppression
,
Cohesive Zone Method
,
Finite Element Method
URI
https://hdl.handle.net/11511/107658
Collections
Graduate School of Natural and Applied Sciences, Thesis
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
F. Ergin, “Investigation of Delamination Suppression in Highly Tapered Composite Laminates,” M.S. - Master of Science, Middle East Technical University, 2023.