Multi-disciplinary design optimization for conceptual design of hybrid-electric aircraft

dc.contributorSilva, Higor Luis
dc.contributorGuimarães, Thiago Augusto Machado
dc.contributorhttp://lattes.cnpq.br/0859338195145281
dc.contributorMorais, Tobias Souza
dc.creatorCruz, Mateus Alves Araújo
dc.date2020-03-25T18:17:01Z
dc.date2020-03-25T18:17:01Z
dc.date2019-12-20
dc.date.accessioned2023-09-28T21:24:23Z
dc.date.available2023-09-28T21:24:23Z
dc.identifierCRUZ, Mateus Alves Araújo. Multi-disciplinary design optimization for conceptual design of hybrid-electric aircraft. 2019. 85 f. Trabalho de Conclusão de Curso (Graduação em Engenharia Aeronáutica) - Universidade Federal de Uberlândia, Uberlândia, 2020.
dc.identifierhttps://repositorio.ufu.br/handle/123456789/29042
dc.identifier.urihttps://repositorioslatinoamericanos.uchile.cl/handle/2250/9069161
dc.descriptionTrabalho de Conclusão de Curso (Graduação)
dc.descriptionThis work presents a multidisciplinary design optimization (MDO) for general aviation and hybrid-electricaircraftdesignintegratingboxesofaerodynamics,structures,flightmechanicsand performance. The methodologies used in each box are presented and, to increase the reliability on new designs, these tools were made to minimize or not use at all any historical data. The aircraft designed is present in the general aviation market and the requirements are specified according to its competitors, taking credit of a distributed propulsion system. Furthermore, the objective-functions are minimize fuel consumption and maximum takeoff weight. The results in terms of geometry, aerodynamic parameters and performance were compared to the aircraft competitors to evaluate the accuracy of the MDO. At least, the MDO generated a final project in order to highlight the commitment relationships of a hybrid-electric aircraft in matters of the objectuve-functions definded to this project.
dc.formatapplication/pdf
dc.languageeng
dc.publisherUniversidade Federal de Uberlândia
dc.publisherBrasil
dc.publisherEngenharia Aeronáutica
dc.rightsAcesso Aberto
dc.subjectMultidisciplinary design optimization
dc.subjectGeneral aviation
dc.subjectHybrid-electric aircraft
dc.subjectDistributed propulsion
dc.subjectOtimização de projeto multidisciplinar
dc.subjectAviação geral
dc.subjectAeronaves híbridas elétricas
dc.subjectPropulsão distribuída
dc.subjectCNPQ::ENGENHARIAS
dc.titleMulti-disciplinary design optimization for conceptual design of hybrid-electric aircraft
dc.typeTrabalho de Conclusão de Curso


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