Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution

Detalhes bibliográficos
Autor(a) principal: Nonaka, Iago Tetsuo
Data de Publicação: 2023
Tipo de documento: Trabalho de conclusão de curso
Idioma: eng
Título da fonte: Repositório Institucional da UFU
Texto Completo: https://repositorio.ufu.br/handle/123456789/41541
Resumo: Trabalho de Conclusão de Curso (Graduação)
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spelling Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolutionPropellerBladeThrustOptimizationCNPQ::ENGENHARIAS::ENGENHARIA AEROESPACIAL::PROPULSAO AEROESPACIAL::MAQUINAS DE FLUXOTrabalho de Conclusão de Curso (Graduação)Aircraft engines operate by Newton's Third Law, which states that for every action, there is a reaction. Normally, those that operate at low Mach produce thrust by a combination of engine and propeller. The propeller works by pushing air backward, it may propel a high quantity of air at a lower speed until a small quantity at higher velocities. In this thesis, an analytical method to optimize the design and performance of a propeller is presented. The main objective is to create an approach, that defines an optimal airscrew that will best suit an engine. Accurate propeller predictions are crucial in aircraft performance since detailed analysis consists of computational simulations or experiments, which are highly time-consuming and expensive. First, the Blade Element Momentum Theory is implemented, based on a database built by XFOIL. To validate, the results are compared with other analytical and experimental results from other theses. Then, an algorithm of optimization called Accelerated Differential Evolution was implemented. It developed an optimized propeller that produces 4\% higher efficiency compared to the one made for an electrical aircraft.Universidade Federal de UberlândiaBrasilEngenharia AeronáuticaVedovotto, João Marcelohttp://lattes.cnpq.br/5630598971511798Vedovotto, João Marcelohttp://lattes.cnpq.br/5630598971511798Cavallini Junior, Aldemir Aparecidohttp://lattes.cnpq.br/0387727577180664Elias, Alex Joséhttp://lattes.cnpq.br/6260628541386586Nonaka, Iago Tetsuo2024-07-02T17:43:26Z2024-07-02T17:43:26Z2023-12-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/bachelorThesisapplication/pdfNONAKA, Iago Tetsuo. Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution. 2023. 58 f. Trabalho de Conclusão de Curso (Graduação em Engenharia Aeronáutica) - Universidade Federal de Uberlândia, Uberlândia, 2024.https://repositorio.ufu.br/handle/123456789/41541engAttribution 3.0 United Stateshttp://creativecommons.org/licenses/by/3.0/us/info:eu-repo/semantics/openAccessreponame:Repositório Institucional da UFUinstname:Universidade Federal de Uberlândia (UFU)instacron:UFU2024-07-03T06:20:12Zoai:repositorio.ufu.br:123456789/41541Repositório InstitucionalONGhttp://repositorio.ufu.br/oai/requestdiinf@dirbi.ufu.bropendoar:2024-07-03T06:20:12Repositório Institucional da UFU - Universidade Federal de Uberlândia (UFU)false
dc.title.none.fl_str_mv Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
title Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
spellingShingle Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
Nonaka, Iago Tetsuo
Propeller
Blade
Thrust
Optimization
CNPQ::ENGENHARIAS::ENGENHARIA AEROESPACIAL::PROPULSAO AEROESPACIAL::MAQUINAS DE FLUXO
title_short Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
title_full Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
title_fullStr Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
title_full_unstemmed Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
title_sort Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution
author Nonaka, Iago Tetsuo
author_facet Nonaka, Iago Tetsuo
author_role author
dc.contributor.none.fl_str_mv Vedovotto, João Marcelo
http://lattes.cnpq.br/5630598971511798
Vedovotto, João Marcelo
http://lattes.cnpq.br/5630598971511798
Cavallini Junior, Aldemir Aparecido
http://lattes.cnpq.br/0387727577180664
Elias, Alex José
http://lattes.cnpq.br/6260628541386586
dc.contributor.author.fl_str_mv Nonaka, Iago Tetsuo
dc.subject.por.fl_str_mv Propeller
Blade
Thrust
Optimization
CNPQ::ENGENHARIAS::ENGENHARIA AEROESPACIAL::PROPULSAO AEROESPACIAL::MAQUINAS DE FLUXO
topic Propeller
Blade
Thrust
Optimization
CNPQ::ENGENHARIAS::ENGENHARIA AEROESPACIAL::PROPULSAO AEROESPACIAL::MAQUINAS DE FLUXO
description Trabalho de Conclusão de Curso (Graduação)
publishDate 2023
dc.date.none.fl_str_mv 2023-12-01
2024-07-02T17:43:26Z
2024-07-02T17:43:26Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/bachelorThesis
format bachelorThesis
status_str publishedVersion
dc.identifier.uri.fl_str_mv NONAKA, Iago Tetsuo. Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution. 2023. 58 f. Trabalho de Conclusão de Curso (Graduação em Engenharia Aeronáutica) - Universidade Federal de Uberlândia, Uberlândia, 2024.
https://repositorio.ufu.br/handle/123456789/41541
identifier_str_mv NONAKA, Iago Tetsuo. Propeller optimization approach: Blade Element Momentum Theory in accelerated differential evolution. 2023. 58 f. Trabalho de Conclusão de Curso (Graduação em Engenharia Aeronáutica) - Universidade Federal de Uberlândia, Uberlândia, 2024.
url https://repositorio.ufu.br/handle/123456789/41541
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv Attribution 3.0 United States
http://creativecommons.org/licenses/by/3.0/us/
info:eu-repo/semantics/openAccess
rights_invalid_str_mv Attribution 3.0 United States
http://creativecommons.org/licenses/by/3.0/us/
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Universidade Federal de Uberlândia
Brasil
Engenharia Aeronáutica
publisher.none.fl_str_mv Universidade Federal de Uberlândia
Brasil
Engenharia Aeronáutica
dc.source.none.fl_str_mv reponame:Repositório Institucional da UFU
instname:Universidade Federal de Uberlândia (UFU)
instacron:UFU
instname_str Universidade Federal de Uberlândia (UFU)
instacron_str UFU
institution UFU
reponame_str Repositório Institucional da UFU
collection Repositório Institucional da UFU
repository.name.fl_str_mv Repositório Institucional da UFU - Universidade Federal de Uberlândia (UFU)
repository.mail.fl_str_mv diinf@dirbi.ufu.br
_version_ 1805569568768262144

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