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Comparison of numerical and experimental strain distributions in composite panel for aerospace applications

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Comparison of numerical and experimental strain distributions in composite panel for aerospace applications

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dc.contributor.author Mucha, Waldemar es_ES
dc.contributor.author Kuś, Wacław es_ES
dc.contributor.author Viana, Júlio es_ES
dc.contributor.author Nunes, João es_ES
dc.date.accessioned 2022-09-28T07:34:46Z
dc.date.available 2022-09-28T07:34:46Z
dc.date.issued 2022-05-11
dc.identifier.isbn 9788490489697
dc.identifier.uri http://hdl.handle.net/10251/186655
dc.description.abstract [EN] In structural applications of aerospace industry, weight efficiency, understood as minimal weight and maximal stiffness, is of great importance. This criterion can be achieved by composite lightweight structures. Typical structures for aforementioned applications are sandwich panels (e.g., with honeycomb core) and stiffened panels (e.g., with blade ribs, T-bar ribs, or hat ribs). In this paper, a hat-stiffened panel, made of carbon/epoxy woven composite, is considered. Results of experiments, consisting of loading the panel and measuring exciting forces and strains (using strain gages), are presented. The results are compared to strains distribution obtained from finite element model of the panel. es_ES
dc.description.sponsorship The research was partially funded from financial resources from the statutory subsidy of the Faculty of Mechanical Engineering, Silesian University of Technology, in 2021. W.M. acknowledges the National Agency for Academic Exchange of Poland (under the Academic International Partnerships program, grant agreement PPI/APM/2018/1/00004) for supporting training in the University of Minho, which enabled execution of the study. es_ES
dc.format.extent 9 es_ES
dc.language Inglés es_ES
dc.publisher Editorial Universitat Politècnica de València es_ES
dc.relation.ispartof Proceedings of the YIC 2021 - VI ECCOMAS Young Investigators Conference
dc.rights Reconocimiento - No comercial - Compartir igual (by-nc-sa) es_ES
dc.subject Aerostructures es_ES
dc.subject Lightweight structures es_ES
dc.subject Strain measurement es_ES
dc.subject Finite element method es_ES
dc.subject Operational load monitoring es_ES
dc.subject Artificial intelligence es_ES
dc.title Comparison of numerical and experimental strain distributions in composite panel for aerospace applications es_ES
dc.type Capítulo de libro es_ES
dc.type Comunicación en congreso es_ES
dc.identifier.doi 10.4995/YIC2021.2021.12572
dc.relation.projectID info:eu-repo/grantAgreement/SUT//PPI/APM/2018%2F1%2F00004 es_ES
dc.rights.accessRights Abierto es_ES
dc.description.bibliographicCitation Mucha, W.; Kuś, W.; Viana, J.; Nunes, J. (2022). Comparison of numerical and experimental strain distributions in composite panel for aerospace applications. En Proceedings of the YIC 2021 - VI ECCOMAS Young Investigators Conference. Editorial Universitat Politècnica de València. 403-411. https://doi.org/10.4995/YIC2021.2021.12572 es_ES
dc.description.accrualMethod OCS es_ES
dc.relation.conferencename VI ECCOMAS Young Investigators Conference es_ES
dc.relation.conferencedate Julio 07-09, 2021 es_ES
dc.relation.conferenceplace Valencia, España es_ES
dc.relation.publisherversion http://ocs.editorial.upv.es/index.php/YIC/YIC2021/paper/view/12572 es_ES
dc.description.upvformatpinicio 403 es_ES
dc.description.upvformatpfin 411 es_ES
dc.type.version info:eu-repo/semantics/publishedVersion es_ES
dc.relation.pasarela OCS\12572 es_ES
dc.contributor.funder Silesian University of Technology es_ES


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