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Experimental investigation, non-linear numerical modelling and optimization of carbon fiber reinforced sandwich three-bolt, single-lap joints used for aeronautical structures

Crossref DOI link: https://doi.org/10.1007/s12008-026-02607-4

Published Online: 2026-06-02

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Ounss, Soukaina https://orcid.org/0000-0001-7495-9132
Mounir, Hamid
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Text and Data Mining valid from 2026-06-02

Version of Record valid from 2026-06-02
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Article History

Received: 14 July 2024

Revised: 4 May 2025

Accepted: 6 May 2026

First Online: 2 June 2026

Declarations

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: The authors have no competing interests to declare that are relevant to the content of this article.

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