Buckling mode transition in hat-stiffened composite panels loaded in uniaxial compression-Reference-Cited by-同舟云学术

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Buckling mode transition in hat-stiffened composite panels loaded in uniaxial compression

Published:1997-02 Issue:2 Volume:37 Page:253-267
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Falzon Brian G.,Steven Grant P.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference17 articles.

1. Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression;Starnes;AIAA Journal Paper 82-0777,1982

2. Postbuckling failure of composite panels;Buskell,1985

3. Postbuckling response and failure prediction of graphite-epoxy plates loaded in compression;Englestad;AIAA J.,1992

4. Experimental study on the buckling and postbuckling of carbon fibre composite panels with and without interply disbonds;Chai,1989

5. Post-buckling of flat stiffened graphite/epoxy panels under cyclic compression;Frostig,1989

Cited by 33 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical simulations and testing of notched composite plates under envelope loadings: Validation with the safe life domain method;Composite Structures;2024-07

2. Influence of Fillers on the Post-buckling Behavior of the Hat-Stiffened Composite Panels;International Journal of Aeronautical and Space Sciences;2023-05-23

3. Design and Testing of Impacted Stiffened CFRP Panels under Compression with the VERTEX Test Rig;Aerospace;2023-03-25

4. Investigation on buckling and mode jumping of composite plates under thermomechanical loads;International Journal of Non-Linear Mechanics;2022-01

5. Postbuckling response of unitized stiffened textile composite panels: Experiments;International Journal of Non-Linear Mechanics;2021-12

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