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

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Published in:Fatigue of Aircraft Structures
Format: Online Article RSS Article
Published: 2025
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container_title Fatigue of Aircraft Structures
description
discipline_display Aeronautics and space flight
discipline_facet Aeronautics and space flight
format Online Article
RSS Article
genre Journal Article
id rss_article:85057
institution FRELIP
journal_source_facet Fatigue of Aircraft Structures
last_indexed 2026-06-20T21:41:21.451Z
publishDate 2025
publishDateSort 2025
record_format rss_article
spellingShingle Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
Aeronautics and space flight
General
Aeronautics and space flight
sub_discipline_display General
sub_discipline_facet General
subject_display Aeronautics and space flight
General
Aeronautics and space flight
subject_facet Aeronautics and space flight
General
Aeronautics and space flight
title Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
title_alt Análisis de resistencia residual de un panel rigidizado compuesto después de una desunión del rigidizador utilizando un modelo numérico de daño industrial
Analyse de la résistance résiduelle d'un panneau raidisseur composite après décollement d'un raidisseur à l'aide d'un modèle numérique industriel d'endommagement
Análise de Resistência Residual de um Painel Reforçado de Compósito Após Descolagem de Reforço Usando um Modelo Numérico de Dano Industrial
title_auth Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
title_es_txt Análisis de resistencia residual de un panel rigidizado compuesto después de una desunión del rigidizador utilizando un modelo numérico de daño industrial
title_fr_txt Analyse de la résistance résiduelle d'un panneau raidisseur composite après décollement d'un raidisseur à l'aide d'un modèle numérique industriel d'endommagement
title_full Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
title_fullStr Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
title_full_unstemmed Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
title_pt_txt Análise de Resistência Residual de um Painel Reforçado de Compósito Após Descolagem de Reforço Usando um Modelo Numérico de Dano Industrial
title_short Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model
title_sort residual strength analysis of a composite stiffened panel after a stiffener debonding using an industrial numerical damage model
topic Aeronautics and space flight
General
Aeronautics and space flight
url https://sciendo.com/article/10.2478/fas-2024-0004