Fail-safe design optimization of an aircraft fuselage-wing section using the DamageCreator software

UDC.coleccionInvestigaciónes_ES
UDC.conferenceTitleAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022es_ES
UDC.departamentoConstrucións e Estruturas Arquitectónicas, Civís e Aeronáuticases_ES
UDC.grupoInvMecánica de Estruturas (ME)es_ES
UDC.institutoCentroCITEEC - Centro de Innovación Tecnolóxica en Edificación e Enxeñaría Civiles_ES
dc.contributor.authorCid, Clara
dc.contributor.authorBaldomir, Aitor
dc.contributor.authorRodríguez-Segade, Miguel
dc.contributor.authorHernández, Santiago
dc.date.accessioned2025-01-16T14:35:05Z
dc.date.available2025-01-16T14:35:05Z
dc.date.issued2022
dc.descriptionVersión aceptada de: https://doi.org/10.2514/6.2022-1277es_ES
dc.description.abstract[Abstract] Fail-safe design in aerospace is often addressed by the use of envelopes of possible damaged configurations when there is uncertainty about the size or location of the damage. This strategy leads to oversized designs, since realistic damage scenarios are not considered. In a previous research, we developed the DamageCreator software to automatically generate a large set of damaged FE meshes representing real accidental situations, coming from uncontained engine failures or propeller blade failures. This paper aims to perform a fail-safe optimization of a industry-like aerospace structure using realistic damaged scenarios automatically generated by the DamageCreator tool. A real historical accident database will be taken as input to generate the set of damaged configurations.es_ES
dc.description.sponsorshipThe research leading to these results has been conducted under Grant PID2019-108307RB-I00 funded by MCIN/AEI/10.13039/501100011033. The authors also acknowledge funding received from the Galician Government through research grant ED431C 2017/72. The first author also acknowledges the sponsorship of the Galician Government through the grant “axudas de apoio á etapa predoutoral cofinanciadas parcialmente polo programa operativo FSE Galicia 2014-2020” under identification number ED481A-2018/193.es_ES
dc.description.sponsorshipXunta de Galicia; ED431C 2017/72es_ES
dc.description.sponsorshipXunta de Galicia; ED481A-2018/193es_ES
dc.identifier.citationClara Cid Bengoa, Aitor Baldomir, Miguel Rodríguez-Segade and Santiago Hernández (2022). Fail-safe design optimization of an aircraft fuselage-wing section using the DamageCreator software, AIAA 2022-1277. AIAA SCITECH 2022 Forum. https://doi.org/10.2514/6.2022-1277es_ES
dc.identifier.doi10.2514/6.2022-1277
dc.identifier.isbn9781624106316
dc.identifier.urihttp://hdl.handle.net/2183/40748
dc.language.isoenges_ES
dc.publisherAmerican Institute of Aeronautics and Astronautics Inc, AIAAes_ES
dc.relation.projectIDinfo:eu-repo/grantAgreement/AEI/Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020/PID2019-108307RB-I00/ES/OPTIMIZACION PROBABILISTA FRENTE A IMPACTO Y TOLERANTE A DAÑOS DE ESTRUCTURAS DE FUSELAJE DE NUEVA GENERACIONes_ES
dc.relation.urihttps://doi.org/10.2514/6.2022-1277es_ES
dc.rightsThis version of the article has been accepted for publication, after peer review, but is not the Version of Record and does not reflect post acceptance improvements, or any corrections. The Version of Record is available online at: https://doi.org/10.2514/6.2022-1277es_ES
dc.rights.accessRightsopen accesses_ES
dc.subjectStructural responsees_ES
dc.subjectAircraft structureses_ES
dc.subjectUncontained engine failurees_ES
dc.subjectPropeller bladeses_ES
dc.subjectFinite element modelinges_ES
dc.subjectAerospace industryes_ES
dc.subjectYoung's moduluses_ES
dc.subjectNarrow body aircraftes_ES
dc.subjectNumerical optimizationes_ES
dc.subjectIndustrial applicationses_ES
dc.titleFail-safe design optimization of an aircraft fuselage-wing section using the DamageCreator softwarees_ES
dc.typeconference outputes_ES
dspace.entity.typePublication
relation.isAuthorOfPublication79c27f6c-e912-4c62-85cf-1ee045e0c39f
relation.isAuthorOfPublication64ec0814-6c5d-43f4-8b18-401e25f057f6
relation.isAuthorOfPublication129a7f0b-20d3-4151-91c8-20268b326067
relation.isAuthorOfPublication.latestForDiscovery79c27f6c-e912-4c62-85cf-1ee045e0c39f

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