Experimental and Numerical Investigations of Thin-Walled Stringer-Stiffened Panels Welded with RFSSW Technology under Uniaxial Compression

Many aircraft structures are thin walled and stringer-stiffened, and therefore, prone to a loss of stability. This paper deals with accurate and validated stability analysis of the model of aircraft skin under compressive loading. Both experimental and numerical analyzes are conducted. Two different...

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Detalles Bibliográficos
Autores principales: Kubit, Andrzej, Trzepiecinski, Tomasz, Święch, Łukasz, Faes, Koen, Slota, Jan
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6601042/
https://www.ncbi.nlm.nih.gov/pubmed/31159451
http://dx.doi.org/10.3390/ma12111785

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6601042/
https://www.ncbi.nlm.nih.gov/pubmed/31159451
http://dx.doi.org/10.3390/ma12111785

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