Fully reversed mode-II fatigue testing

Rico Kuehlewind; Luiz F. Kawashita; Stephen R. Hallett

Fully reversed mode-II fatigue testing

Rico Kuehlewind, Luiz F. Kawashita, Stephen R. Hallett

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

1 Citation (Scopus)

Abstract

Composite structures for aerospace applications are constantly subjected to vibration loading from a variety of sources including aerodynamic loading and aero-engine vibration. This loading is by nature both cyclic and "fully reversed", i.e. the structure deforms both in the positive and negative senses. Fully reversed fatigue degradation needs to be better understood from a material point of view. This paper presents a novel test method for fully reversed mode-II delamination fatigue. The test has been used to study the material behaviour of laminated carbon fibre composites in fully reversed loading and its validity been investigated. First test results are presented and discussed which will help identify underlying material behaviour for future model development.

Original language	English
Title of host publication	ECCM 2016 - Proceeding of the 17th European Conference on Composite Materials
Publisher	European Conference on Composite Materials, ECCM
ISBN (Electronic)	9783000533877
Publication status	Published - 2016
Event	17th European Conference on Composite Materials, ECCM 2016 - Munich, Germany Duration: 26 Jun 2016 → 30 Jun 2016

Conference

Conference	17th European Conference on Composite Materials, ECCM 2016
Abbreviated title	ECCM 2016
Country/Territory	Germany
City	Munich
Period	26/06/16 → 30/06/16

Keywords

Composite
Delamination
Fatigue
Fully reversed loading
Test method

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@inproceedings{39234a1333904c2ab540616b3cbc0066,

title = "Fully reversed mode-II fatigue testing",

abstract = "Composite structures for aerospace applications are constantly subjected to vibration loading from a variety of sources including aerodynamic loading and aero-engine vibration. This loading is by nature both cyclic and {"}fully reversed{"}, i.e. the structure deforms both in the positive and negative senses. Fully reversed fatigue degradation needs to be better understood from a material point of view. This paper presents a novel test method for fully reversed mode-II delamination fatigue. The test has been used to study the material behaviour of laminated carbon fibre composites in fully reversed loading and its validity been investigated. First test results are presented and discussed which will help identify underlying material behaviour for future model development.",

keywords = "Composite, Delamination, Fatigue, Fully reversed loading, Test method",

author = "Rico Kuehlewind and Kawashita, {Luiz F.} and Hallett, {Stephen R.}",

year = "2016",

language = "English",

booktitle = "ECCM 2016 - Proceeding of the 17th European Conference on Composite Materials",

publisher = "European Conference on Composite Materials, ECCM",

note = "17th European Conference on Composite Materials, ECCM 2016, ECCM 2016 ; Conference date: 26-06-2016 Through 30-06-2016",

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TY - GEN

T1 - Fully reversed mode-II fatigue testing

AU - Kuehlewind, Rico

AU - Kawashita, Luiz F.

AU - Hallett, Stephen R.

PY - 2016

Y1 - 2016

N2 - Composite structures for aerospace applications are constantly subjected to vibration loading from a variety of sources including aerodynamic loading and aero-engine vibration. This loading is by nature both cyclic and "fully reversed", i.e. the structure deforms both in the positive and negative senses. Fully reversed fatigue degradation needs to be better understood from a material point of view. This paper presents a novel test method for fully reversed mode-II delamination fatigue. The test has been used to study the material behaviour of laminated carbon fibre composites in fully reversed loading and its validity been investigated. First test results are presented and discussed which will help identify underlying material behaviour for future model development.

AB - Composite structures for aerospace applications are constantly subjected to vibration loading from a variety of sources including aerodynamic loading and aero-engine vibration. This loading is by nature both cyclic and "fully reversed", i.e. the structure deforms both in the positive and negative senses. Fully reversed fatigue degradation needs to be better understood from a material point of view. This paper presents a novel test method for fully reversed mode-II delamination fatigue. The test has been used to study the material behaviour of laminated carbon fibre composites in fully reversed loading and its validity been investigated. First test results are presented and discussed which will help identify underlying material behaviour for future model development.

KW - Composite

KW - Delamination

KW - Fatigue

KW - Fully reversed loading

KW - Test method

UR - http://www.scopus.com/inward/record.url?scp=85018603614&partnerID=8YFLogxK

M3 - Conference Contribution (Conference Proceeding)

AN - SCOPUS:85018603614

BT - ECCM 2016 - Proceeding of the 17th European Conference on Composite Materials

PB - European Conference on Composite Materials, ECCM

T2 - 17th European Conference on Composite Materials, ECCM 2016

Y2 - 26 June 2016 through 30 June 2016

ER -

Fully reversed mode-II fatigue testing

Abstract

Conference

Keywords

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