Cyclic-fatigue crack growth in composite and adhesively-bonded structures: the FAA slow crack growth approach to certification and the problem of similitude

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Title: Cyclic-fatigue crack growth in composite and adhesively-bonded structures: the FAA slow crack growth approach to certification and the problem of similitude
Author(s): Kinloch, AJ
Jones, R
Hu, W
Item Type: Journal Article
Publication Date: 9-Mar-2016
Date of Acceptance: 4-Mar-2016
URI: http://hdl.handle.net/10044/1/30114
DOI: http://dx.doi.org/10.1016/j.ijfatigue.2016.03.008
ISSN: 1879-3452
Publisher: Elsevier
Start Page: 10
End Page: 18
Journal / Book Title: International Journal of Fatigue
Volume: 88
Copyright Statement: © 2016 Published by Elsevier Ltd. Licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/
Keywords: Science & Technology
Technology
Engineering, Mechanical
Materials Science, Multidisciplinary
Engineering
Materials Science
Similitude
Adhesives
Composites
Fatigue crack growth
Delamination
POLYMER-MATRIX COMPOSITES
DELAMINATION GROWTH
STRESS-RATIO
MODE-I
THRESHOLD
JOINTS
CFRP
INTENSITY
TOUGHNESS
AIRCRAFT
Mechanical Engineering & Transports
0913 Mechanical Engineering
0905 Civil Engineering
Publication Status: Published
Appears in Collections:Faculty of Engineering
Mechanical Engineering



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