Failure Analysis of Hat-Stringer-Stiffened Aircraft Composite Panels under Four-Point Bending Loading

Hat-stringer-stiffened composite panels have been widely used in aircrafts. Accurate failure analysis of them is important for the safety and integrity of the fuselage. During the service period, these panels will bear not only the lateral force caused by the bending of fuselage, but also the radial...

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Detalles Bibliográficos
Autores principales: Li, Binkai, Gong, Yu, Gao, Yukui, Hou, Mengqing, Li, Lei
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9000179/
https://www.ncbi.nlm.nih.gov/pubmed/35407760
http://dx.doi.org/10.3390/ma15072430

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9000179/
https://www.ncbi.nlm.nih.gov/pubmed/35407760
http://dx.doi.org/10.3390/ma15072430

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