Temperature effects on fatigue delamination behavior in thermoset composite laminates
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Reference35 articles.
1. Federal Aviation Authority. Airworthiness Advisory Circular No: 20-107B. Composite Aircraft Structure, 2009.
2. Development of a standardized procedure for the characterization of interlaminar delamination propagation in advanced composites under fatigue mode I loading conditions;Brunner;Engng Fract Mech,2009
3. Mode I delamination fatigue crack growth in unidirectional fiber reinforced composites: Development of a standardized test procedure;Stelzer;Compos Sci Technol,2012
4. Effect of data reduction and fiber-bridging on mode I delamination characterization of unidirectional composites;Murri;J Compos Mater,2014
5. Mode I delamination fatigue crack growth in unidirectional fiber reinforced composites Results from ESIS TC 4 round-robins;Stelzer;Engng Fract Mech,2014
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1. Hygrothermal ageing effects on mode I fatigue delamination in multidirectional composite laminates;International Journal of Fatigue;2024-11
2. Fractographic analysis of damage mechanisms dominated by delamination in composite laminates: A comprehensive review;Polymer Testing;2024-05
3. Determination of the In-Plane Shear Behavior of and Process Influence on Uncured Unidirectional CF/Epoxy Prepreg Using Digital Image Correlation Analysis;Journal of Composites Science;2024-04-05
4. On Cyclic-Fatigue Crack Growth in Carbon-Fibre-Reinforced Epoxy–Polymer Composites;Polymers;2024-02-04
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