On the Evaluation of a Coupled Sequential Approach for Rotorcraft Landing Simulation

Maximum loads acting on aircraft structures generally arise when the aircraft is undergoing some form of acceleration, such as during landing. Landing, especially when considering rotorcrafts, is thus crucial in determining the operational load spectrum, and accurate predictions on the actual health...

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Detalles Bibliográficos
Autores principales: Cristiani, Demetrio, Colombo, Luca, Zielinski, Wojciech, Sbarufatti, Claudio, Cadini, Francesco, Dziendzikowski, Michal, Giglio, Marco
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7248906/
https://www.ncbi.nlm.nih.gov/pubmed/32365708
http://dx.doi.org/10.3390/s20092540

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7248906/
https://www.ncbi.nlm.nih.gov/pubmed/32365708
http://dx.doi.org/10.3390/s20092540

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