The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination

Andrew T Rhead, Richard Butler, Wenli Liu, Neil Baker

Research output: Contribution to journalArticle

  • 3 Citations

Abstract

A combination of uniaxial compression tests and Strip Model and Finite Element analyses of laminates artificially delaminated to create circular [±θ] sublaminates is used to assess the influence of fibre angle on the compressive strength of composite laminates.
LanguageEnglish
Pages1315-1330
Number of pages16
JournalAeronautical Journal
Volume116
Issue number1186
StatusPublished - Dec 2012

Fingerprint

Delamination
Compressive strength
Laminates
Buckling
Fibers
Composite materials
Poisson ratio
Stiffness
Tensile strain
Crack propagation
Compaction

Keywords

  • damage tolerance

Cite this

The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination. / Rhead, Andrew T; Butler, Richard; Liu, Wenli; Baker, Neil.

In: Aeronautical Journal, Vol. 116, No. 1186, 12.2012, p. 1315-1330.

Research output: Contribution to journalArticle

@article{985faf0f093245e5882aac7ca5210673,
title = "The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination",
keywords = "damage tolerance",
author = "Rhead, {Andrew T} and Richard Butler and Wenli Liu and Neil Baker",
note = "Paper No: 3886",
year = "2012",
month = "12",
language = "English",
volume = "116",
pages = "1315--1330",
journal = "Aeronautical Journal",
issn = "0001-9240",
publisher = "Royal Aeronautical Society",
number = "1186",

}

TY - JOUR

T1 - The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination

AU - Rhead,Andrew T

AU - Butler,Richard

AU - Liu,Wenli

AU - Baker,Neil

N1 - Paper No: 3886

PY - 2012/12

Y1 - 2012/12

KW - damage tolerance

UR - http://www.scopus.com/inward/record.url?scp=84872346647&partnerID=8YFLogxK

UR - http://aerosociety.com/News/Publications/Aero-Journal/Online/936/The-influence-of-surface-ply-fibre-angle-on-the-compressive-strength-of-composite-laminates-containing-delamination

M3 - Article

VL - 116

SP - 1315

EP - 1330

JO - Aeronautical Journal

T2 - Aeronautical Journal

JF - Aeronautical Journal

SN - 0001-9240

IS - 1186

ER -