1. Repositório Institucional - Universidade Federal de Uberlândia
  2. Faculdade de Engenharia Mecânica (FEMEC)
  3. TCC - Engenharia Aeronáutica
Please use this identifier to cite or link to this item: https://repositorio.ufu.br/handle/123456789/29042
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dc.creatorCruz, Mateus Alves Araújo-
dc.date.accessioned2020-03-25T18:17:01Z-
dc.date.available2020-03-25T18:17:01Z-
dc.date.issued2019-12-20-
dc.identifier.citationCRUZ, 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.pt_BR
dc.identifier.urihttps://repositorio.ufu.br/handle/123456789/29042-
dc.languageengpt_BR
dc.publisherUniversidade Federal de Uberlândiapt_BR
dc.rightsAcesso Abertopt_BR
dc.subjectMultidisciplinary design optimizationpt_BR
dc.subjectGeneral aviationpt_BR
dc.subjectHybrid-electric aircraftpt_BR
dc.subjectDistributed propulsionpt_BR
dc.subjectOtimização de projeto multidisciplinarpt_BR
dc.subjectAviação geralpt_BR
dc.subjectAeronaves híbridas elétricaspt_BR
dc.subjectPropulsão distribuídapt_BR
dc.titleMulti-disciplinary design optimization for conceptual design of hybrid-electric aircraftpt_BR
dc.typeTrabalho de Conclusão de Cursopt_BR
dc.contributor.advisor-co1Silva, Higor Luis-
dc.contributor.advisor1Guimarães, Thiago Augusto Machado-
dc.contributor.advisor1Latteshttp://lattes.cnpq.br/0859338195145281pt_BR
dc.contributor.referee1Morais, Tobias Souza-
dc.description.degreenameTrabalho de Conclusão de Curso (Graduação)pt_BR
dc.description.resumoThis 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.pt_BR
dc.publisher.countryBrasilpt_BR
dc.publisher.courseEngenharia Aeronáuticapt_BR
dc.sizeorduration85pt_BR
dc.subject.cnpqCNPQ::ENGENHARIASpt_BR
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