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A machine learning enhanced characteristic length method for failure prediction of open hole tension composites (2024)

First Author: Azeem O

Attributed to: Vera: A new paradigm to enable efficient design of VERy large Aircraft structures - the key for innovative aircraft design concepts funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.jcomc.2024.100524

Publication URI: http://dx.doi.org/10.1016/j.jcomc.2024.100524

Type: Journal Article/Review

Parent Publication: Composites Part C: Open Access