Experiment and Numerical Simulation for the Compressive Buckling Behavior of Double-Sided Laser-Welded Al–Li Alloy Aircraft Fuselage Panel

The aim of this work was to study the buckling behavior and failure mode of the double-sided laser-welded Al–Li alloy panel structure under the effect of axial compression via experimental and numerical simulation methods. In the test, multi-frequency fringe projection profilometry was used to monit...

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Detalles Bibliográficos
Autores principales: Zhang, Yunlong, Tao, Wang, Chen, Yanbin, Lei, Zhenkun, Bai, Ruixiang, Lei, Zhenglong
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7475844/
https://www.ncbi.nlm.nih.gov/pubmed/32823948
http://dx.doi.org/10.3390/ma13163599

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7475844/
https://www.ncbi.nlm.nih.gov/pubmed/32823948
http://dx.doi.org/10.3390/ma13163599

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