Mode I Crack Propagation Experimental Analysis of Adhesive Bonded Joints Comprising Glass Fibre Composite Material under Impact and Constant Amplitude Fatigue Loading

The T-90 Calima is a low-wing monoplane aircraft. Its structure is mainly composed of different components of composite materials, which are mainly bonded by using adhesive joints of different thicknesses. The T-90 Calima is a trainer aircraft; thus, adverse operating conditions such as hard landing...

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Detalles Bibliográficos
Autores principales: Bautista Villamil, Alirio Andres, Casas-Rodriguez, Juan Pablo, Porras Holguin, Alicia, Silva Barrera, Maribel
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8402028/
https://www.ncbi.nlm.nih.gov/pubmed/34442904
http://dx.doi.org/10.3390/ma14164380

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8402028/
https://www.ncbi.nlm.nih.gov/pubmed/34442904
http://dx.doi.org/10.3390/ma14164380

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