A high fidelity multiscale approach for compression-after-impact behavior of 2D triaxially braided composites
Author:
Funder
National Natural Science Foundation of China
Chinese Aeronautical Establishment Aeronautical Science Foundation
Publisher
Elsevier BV
Reference37 articles.
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3. Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements;Rivallant;Composites A,2013
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1. Towards accurate prediction of the dynamic behavior and failure mechanisms of three-dimensional braided composites: A multiscale analysis scheme;Thin-Walled Structures;2024-10
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