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dc.contributor.authorPaz Méndez, Javier
dc.contributor.authorDíaz, J.
dc.contributor.authorRomera, Luis
dc.date.accessioned2020-02-14T18:50:23Z
dc.date.available2020-02-14T18:50:23Z
dc.date.issued2020
dc.identifier.citationCrashworthiness Analysis and Enhancement of Aircraft Structures Under Vertical Impact Scenarios. J. Paz, J. Díaz, and L. Romera. Journal of Aircraft 2020 57:1, 3-12es_ES
dc.identifier.urihttp://hdl.handle.net/2183/24913
dc.description.abstract[Abstract] This research focuses on the crashworthiness study and enhancement of commercial aircraft structures by developing crushable energy absorbers to work as vertical struts. To assess their contribution on a representative crash scenario, a numerical simulation of a Boeing 737-200 drop test developed and verified with experimental data is used as a benchmark. The numerical model is then enhanced with four hybrid energy absorbers designed for programmed and progressive collapse, added in the cargo compartment connecting the underfloor beams and the frames. These devices are composed of a square aluminum tube filled with a composite skeleton and foam extrusions for maximized energy absorption. The enhanced aircraft is later on simulated under hard landing and water ditching scenarios, analyzing the benefits resulting from the absorbers according to structural efficiency and biometric criteria. Results show increased plastic dissipation values by the main structural components given the modified collapse mechanism obtained when adding the crushable absorbers. Peak acceleration values are also reduced, consequently lessening the passenger injury prediction at the studied locations.es_ES
dc.description.sponsorshipThe research leading to these results has received funding from the Spanish Goverment (Ministerio de Economía y Competitividad) under grant agreement DPI2016-76934-R, as well as funding from the Fundación Barriées_ES
dc.language.isoenges_ES
dc.publisherAmerican Institute of Aeronautics and Astronauticses_ES
dc.relationinfo:eu-repo/grantAgreement/AEI/Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016/DPI2016-76934-R/ES/OPTIMIZACION PROBABILISTA DE ESTRUCTURAS AERONAUTICAS INTACTAS Y DAÑADAS FRENTE A CARGAS DINAMICAS Y DE IMPACTO/
dc.relation.urihttps://doi.org/10.2514/1.C035435es_ES
dc.subjectAircraft designes_ES
dc.subjectCrashworthinesses_ES
dc.subjectHard landinges_ES
dc.subjectWater ditchinges_ES
dc.subjectBiometric criteriaes_ES
dc.subjectHybrid energy absorberses_ES
dc.titleCrashworthiness Analysis and Enhancement of Aircraft Structures Under Vertical Impact Scenarioses_ES
dc.typeinfo:eu-repo/semantics/articlees_ES
dc.rights.accessinfo:eu-repo/semantics/openAccesses_ES
UDC.journalTitleJournal of Aircraftes_ES
UDC.volume57es_ES
UDC.issue1es_ES
UDC.startPage3es_ES
UDC.endPage12es_ES
dc.identifier.doi10.2514/1.C035435


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