Cohesive analysis of a 3D benchmark for delamination growth under quasi‐static and fatigue loading conditions
Author:
Affiliation:
1. Faculty of Aerospace Engineering Delft University of Technology Delft The Netherlands
2. Durability, Damage Tolerance and Reliability Branch NASA Langley Research Center Hampton Virginia USA
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1111/ffe.13712
Reference27 articles.
1. Single-Stringer Compression Specimen for the Assessment of Damage Tolerance of Postbuckled Structures
2. Three-dimensional finite element modelling of delamination growth in notched composite laminates under compression loading
3. Damage development in open-hole composite specimens in fatigue. Part 1: Experimental investigation
4. Delamination Growth in a Notched Graphite/Epoxy Laminate Under Compression Fatigue Loading
5. Experimental and numerical investigation of the influence of rivetless nut plate joints on fatigue crack growth in adhesively bonded composite joints
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