Modified Fourier–Galerkin Solution for Aerospace Skin-Stiffener Panels Subjected to Interface Force and Mixed Boundary Conditions

Aeronautical stiffened panels composed of thin shells and beams are prone to deformation or buckling due to the combined loading, functional boundary conditions and interface forces between joined parts in the assembly processes. In this paper, a mechanical prediction model of the multi-component pa...

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Detalles Bibliográficos
Autores principales: Hou, Renluan, Wang, Qing, Li, Jiangxiong, Ke, Yinglin
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6747805/
https://www.ncbi.nlm.nih.gov/pubmed/31480238
http://dx.doi.org/10.3390/ma12172794

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6747805/
https://www.ncbi.nlm.nih.gov/pubmed/31480238
http://dx.doi.org/10.3390/ma12172794

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