Progressive Damage Numerical Modelling and Simulation of Aircraft Composite Bolted Joints Bearing Response

Finite element numerical progressive damage modelling and simulations applied to the strength prediction of airframe bolted joints on composite laminates can lead to shorter and more efficient product cycles in terms of design, analysis and certification, while benefiting the economic manufacturing...

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Detalles Bibliográficos
Autores principales: Gao, Guoqiang, An, Luling, Giannopoulos, Ioannis K., Han, Ning, Ge, Ende, Hu, Geng
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7763887/
https://www.ncbi.nlm.nih.gov/pubmed/33302590
http://dx.doi.org/10.3390/ma13245606

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