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Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model Cover

Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model

Fatigue of Aircraft Structures
Volume 2024 (2024): Issue 16 (December 2024)
By: ,  ,  ,  ,   and    
Open Access
|Jul 2025
Articles in this issue
DOI: https://doi.org/10.2478/fas-2024-0004 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 45 - 56
Published on: Jul 7, 2025
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Keywords:
Composite,
damage model,
stiffened panel,
post-bucking
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2025 Benoît Morlet, Fabrice Congourdeau, Guy Sola, Dominique Martini, Alban Robin, Vincent Jacques, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Volume 2024 (2024): Issue 16 (December 2024)
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