Numerical investigation of composite laminates subject to low-velocity edge-on impact and compression after impact
Author:
Funder
Boeing Company
Publisher
Elsevier BV
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference47 articles.
1. Prediction of impact induced penetration and delamination in thick composite laminates;Potti;Int J Impact Eng,1997
2. Indentation-flexure and low-velocity impact damage in graphite epoxy laminates;Sankar;J Compos Technol Res,1993
3. Delaminations in composite plates under transverse impact loads – experimental results;Finn;Compos Struct,1993
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5. Impact damage detection in composite plates using deflectometry and the virtual fields method;Devivier;Compos Part A: Appl Sci Manuf,2013
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1. Synergistically improving the edge-on impact damage resistance of composite laminates using multi-scale CNF/Z-pin toughening;Composites Science and Technology;2024-06
2. Edge-on impact behaviors of helicoidal fiber arrangement of composite laminates;Journal of Reinforced Plastics and Composites;2023-11-13
3. Mechanical response and failure mechanism of composite laminates subjected to low velocity impact on free edge;Composite Structures;2023-02
4. In-Plane and Oblique Edge-on Impact on Thick Glass-Fibre/Epoxy Composite Laminates;International Journal of Impact Engineering;2023-01
5. Effect of Stitching, Stitch Density, Stacking Sequences on Low-Velocity Edge Impact and Compression after Edge Impact (CAEI) Behavior of Stitched CFRP Laminates;Materials;2022-12-10
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