Numerical study of quasi-static and fatigue delamination growth in a post-buckled composite stiffened panel-Reference-Cited by-同舟云学术

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Numerical study of quasi-static and fatigue delamination growth in a post-buckled composite stiffened panel

Published:2020-02 Issue: Volume:182 Page:107589
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Raimondo A.,Doesburg S.A.,Bisagni C.

Funder

Office of Naval Research

H2020 Marie Skłodowska-Curie Actions

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference35 articles.

1. Postbuckling and failure of stiffened composite panels under axial compression;Kong;Compos Struct,1998

2. A rational analytic theory of fatigue;Paris;Trend Eng,1961

3. A critical analysis of crack propagation laws;Paris;J. Basic. Eng.,1963

4. Delamination under fatigue loads in composite laminates: a review on the observed phenomenology and computational methods;Bak;Appl Mech Rev,2014

5. Accurate simulation of delamination under mixed-mode loading using a cohesive model with a mode-dependent penalty stiffness;Turon;Compos Struct,2018

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2. Buckling and failure assessment of curved butt-joint stiffened thermoplastic composite panels with roller boundary conditions;Composites Science and Technology;2024-07

3. A Numerical Assessment of the Influence of Local Stress Ratio in the Fatigue Analysis of Post-Buckled Composite Single-Stringer Specimen;Journal of Composites Science;2024-04-11

4. A review on buckling of the laminated composite panel under in-plane load;Engineering Research Express;2024-04-04

5. Investigation on strength loss in buckling of composite columns subjected to fatigue loading;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2024-03

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