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/123456789/31133
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dc.creatorCaixeta, Matheus Araujo-
dc.date.accessioned2021-01-22T16:16:30Z-
dc.date.available2021-01-22T16:16:30Z-
dc.date.issued2020-12-22-
dc.identifier.citationCAIXETA, Matheus Araujo. Modelling a coupling routine between tools used in aircraft design. 2020. 65 f. Trabalho de Conclusão de Curso (Graduação em Engenharia Aeronáutica) - Universidade Federal de Uberlândia, Uberlândia, 2021.pt_BR
dc.identifier.urihttps://repositorio.ufu.br/handle/123456789/31133-
dc.description.sponsorshipPesquisa sem auxílio de agências de fomentopt_BR
dc.languageengpt_BR
dc.publisherUniversidade Federal de Uberlândiapt_BR
dc.rightsAcesso Abertopt_BR
dc.subjectPROOSISpt_BR
dc.subjectPacelab APDpt_BR
dc.subjectAircraft designpt_BR
dc.subjectEngine designpt_BR
dc.subjectEngine performance simulationpt_BR
dc.titleModelling a coupling routine between tools used in aircraft designpt_BR
dc.typeTrabalho de Conclusão de Cursopt_BR
dc.contributor.advisor-co1Joksimović, Aleksandar-
dc.contributor.advisor1Martins, Roberto de Souza-
dc.contributor.advisor1Latteshttp://lattes.cnpq.br/4586350967708284pt_BR
dc.contributor.referee1Guimarães, Thiago Augusto Machado-
dc.contributor.referee1Latteshttp://lattes.cnpq.br/0859338195145281pt_BR
dc.contributor.referee2Morais, Tobias Souza-
dc.contributor.referee2Latteshttp://lattes.cnpq.br/1662045974941011pt_BR
dc.description.degreenameTrabalho de Conclusão de Curso (Graduação)pt_BR
dc.description.resumoRecent changes in the aircraft design procedure have made the development of the propulsion system increasingly detailed already in the conceptual phases of the project. Moreover, the use of simulation software in this process has increased considerably in recent years, due to technological advances in processing capacity, optimization algorithms and artificial intelligence. Therefore, a coupling between aircraft design software, PROOSIS and Pacelab APD, was intended to improve the simulations made during these initial phases. Thus, considering the requirements of a commercial transport aircraft, an engine was modelled, dimensioned, and analysed in order to obtain its performance characteristics for different flight phases. The data obtained was then incorporated into the design of the chosen aircraft, using a data import tool. Then, the impacts of this incorporation in the calculation of the aircraft's mission were analysed in order to identify not only the gains achieved, but also the possible failures of the chosen procedure. With the developed manual coupling routine, the designed aircraft had an increase of 7.5% in its range, due to the better representativeness of the data obtained for fuel consumption in cruise condition. In addition, other coupling possibilities, improvements on the coupling achieved and its capacity of generalization were also discussed.pt_BR
dc.publisher.countryBrasilpt_BR
dc.publisher.courseEngenharia Aeronáuticapt_BR
dc.sizeorduration65pt_BR
dc.subject.cnpqCNPQ::ENGENHARIAS::ENGENHARIA AEROESPACIALpt_BR
dc.description.embargo2022-12-22-
Appears in Collections:TCC - Engenharia Aeronáutica

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