Delamination Growth in Polymer-Matrix Fibre Composites and the Use of Fracture-Mechanics Data for Material Characterization and Life Prediction-Reference-Cited by-同舟云学术

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Delamination Growth in Polymer-Matrix Fibre Composites and the Use of Fracture-Mechanics Data for Material Characterization and Life Prediction

Published:2018 Issue: Volume: Page:763-797
ISSN:
Container-title:Aircraft Sustainment and Repair
language:
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Author:

Jones Rhys,Kinloch Anthony J.,Michopoulos John G.,Brunner Andreas J.,Phan Nam

Publisher

Elsevier

Reference81 articles.

1. Department of Defense Joint Service Specification Guide, Aircraft Structures, JSSG-2006, 1998.

2. Composite Materials Handbook, vol. 3: Polymer Matrix Composites Materials Usage, Design and Analysis, SAE International, 2012.

3. Federal Aviation Authority, Airworthiness Advisory Circular No: 20-07B, Composite Aircraft Structure, 2009.

4. Evaluation of Delamination Onset and Growth Characterization Methods under Mode I Fatigue Loading;Murri,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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