Experimental and Numerical Study of Low-Velocity Impact and Tensile after Impact for CFRP Laminates Single-Lap Joints Adhesively Bonded Structure

To investigate the mechanical behavior of the single-lap joints (SLJs) adhesively bonded structure of carbon fiber reinforced polymer (CFRP) laminates under the low-velocity impact (LVI) and tensile-after impact (TAI), tests and simulations were carried out. A finite element model (FEM) was establis...

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Detalles Bibliográficos
Autores principales: Hu, Chunxing, Huang, Guibin, Li, Cheng
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7924855/
https://www.ncbi.nlm.nih.gov/pubmed/33669959
http://dx.doi.org/10.3390/ma14041016

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7924855/
https://www.ncbi.nlm.nih.gov/pubmed/33669959
http://dx.doi.org/10.3390/ma14041016

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