Fail-safe design optimization of an aircraft fuselage-wing section using the DamageCreator software
| UDC.coleccion | Investigación | es_ES |
| UDC.conferenceTitle | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 | es_ES |
| UDC.departamento | Construcións e Estruturas Arquitectónicas, Civís e Aeronáuticas | es_ES |
| UDC.grupoInv | Mecánica de Estruturas (ME) | es_ES |
| UDC.institutoCentro | CITEEC - Centro de Innovación Tecnolóxica en Edificación e Enxeñaría Civil | es_ES |
| dc.contributor.author | Cid, Clara | |
| dc.contributor.author | Baldomir, Aitor | |
| dc.contributor.author | Rodríguez-Segade, Miguel | |
| dc.contributor.author | Hernández, Santiago | |
| dc.date.accessioned | 2025-01-16T14:35:05Z | |
| dc.date.available | 2025-01-16T14:35:05Z | |
| dc.date.issued | 2022 | |
| dc.description | Versión aceptada de: https://doi.org/10.2514/6.2022-1277 | es_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.sponsorship | The 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.sponsorship | Xunta de Galicia; ED431C 2017/72 | es_ES |
| dc.description.sponsorship | Xunta de Galicia; ED481A-2018/193 | es_ES |
| dc.identifier.citation | Clara 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/10.2514/6.2022-1277 | es_ES |
| dc.identifier.doi | 10.2514/6.2022-1277 | |
| dc.identifier.isbn | 9781624106316 | |
| dc.identifier.uri | http://hdl.handle.net/2183/40748 | |
| dc.language.iso | eng | es_ES |
| dc.publisher | American Institute of Aeronautics and Astronautics Inc, AIAA | es_ES |
| dc.relation.projectID | info: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 GENERACION | es_ES |
| dc.relation.uri | https://doi.org/10.2514/6.2022-1277 | es_ES |
| dc.rights | This 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/10.2514/6.2022-1277 | es_ES |
| dc.rights.accessRights | open access | es_ES |
| dc.subject | Structural response | es_ES |
| dc.subject | Aircraft structures | es_ES |
| dc.subject | Uncontained engine failure | es_ES |
| dc.subject | Propeller blades | es_ES |
| dc.subject | Finite element modeling | es_ES |
| dc.subject | Aerospace industry | es_ES |
| dc.subject | Young's modulus | es_ES |
| dc.subject | Narrow body aircraft | es_ES |
| dc.subject | Numerical optimization | es_ES |
| dc.subject | Industrial applications | es_ES |
| dc.title | Fail-safe design optimization of an aircraft fuselage-wing section using the DamageCreator software | es_ES |
| dc.type | conference output | es_ES |
| dspace.entity.type | Publication | |
| relation.isAuthorOfPublication | 79c27f6c-e912-4c62-85cf-1ee045e0c39f | |
| relation.isAuthorOfPublication | 64ec0814-6c5d-43f4-8b18-401e25f057f6 | |
| relation.isAuthorOfPublication | 129a7f0b-20d3-4151-91c8-20268b326067 | |
| relation.isAuthorOfPublication.latestForDiscovery | 79c27f6c-e912-4c62-85cf-1ee045e0c39f |
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