Delamination growth in polymer-matrix fibre composites and the use of fracture mechanics data for material characterisation and life prediction-Reference-Cited by-同舟云学术

Delamination growth in polymer-matrix fibre composites and the use of fracture mechanics data for material characterisation and life prediction

Published:2017-11 Issue: Volume:180 Page:316-333
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Jones R.,Kinloch A.J.,Michopoulos J.G.,Brunner A.J.,Phan N.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference82 articles.

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3. Federal Aviation Authority, (2009) Airworthiness Advisory Circular No: 20–107B. Composite Aircraft Structure, 09/08/2009.

4. Murri GB., Evaluation of delamination onset and growth characterization methods under mode I fatigue loading. Langley Research Center, Hampton, Virginia. NASA/TM-2013-217966, 2013.

5. Cyclic fatigue delamination of carbon fiber-reinforced polymer-matrix composites: data analysis and design considerations;Brunner;Int J Fatigue,2016

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