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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

Open Access
|Jul 2025
Language: English
Page range: 45 - 56
Published on: Jul 7, 2025
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 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.