Development of an UAV for the Air Cargo Challenge 2017 Competition

Detalhes bibliográficos
Autor(a) principal: Gomes, Alexandra Almeida
Data de Publicação: 2017
Tipo de documento: Dissertação
Idioma: eng
Título da fonte: Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
Texto Completo: http://hdl.handle.net/10400.6/7950
Resumo: The present dissertation reports the development of an unmanned remotely piloted aircraft for the Air Cargo Challenge 2017 competition. Air Cargo Challenge is a Design, Build, Fly Aeronautical Engineering competition held in Europe every two years. Given the frequent participation of the Department of Aerospace Sciences from University of Beira Interior in this competition and considering the lack of documentation regarding these participations, this Master of Science Dissertation aims to transmit the accumulated knowledge to future teams and the UAV development community. The aircraft was developed using computer aided engineering tools in the greatest possible extent. The tools used for the development effort include: OpenFOAM®, XFOIL/XFLR5 for airfoil development and detailed wing design and analysis; 3D CAD software as Dassault Systems CATIA® V5 and SolidWorks®; CNC rapid prototyping like 3D printing and CNC hot wire foam core cutting. Experimental test rigs were developed for different studies regarding LiPo batteries for the propulsion and flight testing of high lift devices and roll control. New low Reynolds number airfoils were designed as well as a Fowler flap with an innovative extension mechanism. This mechanism was built using 3D printing technology. Several tests were performed to different batteries to maximize propulsive system power. Furthermore, for the first time in an Air Cargo Challenge, a University of Beira Interior team used mould technology to build the aircraft in carbon fibre reinforced plastics. Several delays and mishaps prevented the development of the aircraft from being completely ready for the competition.
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spelling Development of an UAV for the Air Cargo Challenge 2017 CompetitionAir Cargo ChallengeAircraftAirfoilFowler FlapLow Reynolds NumberUavXflr5XfoilDomínio/Área Científica::Engenharia e Tecnologia::Engenharia AeronáuticaThe present dissertation reports the development of an unmanned remotely piloted aircraft for the Air Cargo Challenge 2017 competition. Air Cargo Challenge is a Design, Build, Fly Aeronautical Engineering competition held in Europe every two years. Given the frequent participation of the Department of Aerospace Sciences from University of Beira Interior in this competition and considering the lack of documentation regarding these participations, this Master of Science Dissertation aims to transmit the accumulated knowledge to future teams and the UAV development community. The aircraft was developed using computer aided engineering tools in the greatest possible extent. The tools used for the development effort include: OpenFOAM®, XFOIL/XFLR5 for airfoil development and detailed wing design and analysis; 3D CAD software as Dassault Systems CATIA® V5 and SolidWorks®; CNC rapid prototyping like 3D printing and CNC hot wire foam core cutting. Experimental test rigs were developed for different studies regarding LiPo batteries for the propulsion and flight testing of high lift devices and roll control. New low Reynolds number airfoils were designed as well as a Fowler flap with an innovative extension mechanism. This mechanism was built using 3D printing technology. Several tests were performed to different batteries to maximize propulsive system power. Furthermore, for the first time in an Air Cargo Challenge, a University of Beira Interior team used mould technology to build the aircraft in carbon fibre reinforced plastics. Several delays and mishaps prevented the development of the aircraft from being completely ready for the competition.A presente Dissertação reporta o desenvolvimento de um veículo aéreo não tripulado para a competição Air Cargo Challenge 2017. O Air Cargo Challenge é uma competição de Engenharia Aeronáutica do tipo Design, Build, Fly, que acontece na Europa a cada dois anos. Dada a frequente participação do Departamento de Ciências Aeroespaciais da Universidade da Beira Interior nesta competição e considerando a falta de documentação relativa a estas participações, esta Dissertação de Mestrado pretende transmitir o conhecimento acumulado para futuras equipas e para a comunidade que desenvolve UAV. A aeronave foi desenvolvida, tanto quanto possível, com ferramentas de engenharia assistida por computador. As ferramentas usadas incluem: OpenFOAM®, XFOIL/XFLR5 para o desenvolvimento de perfis, desenho e análise detalhados da asa; software CAD 3D Dassault Systems CATIA® V5 e SolidWorks®; ferramentas de prototipagem rápida como impressão 3D e máquina CNC de corte de espuma com fio quente. Foram desenvolvidas diferentes bancadas de teste para estudos de baterias LiPo para a propulsão e para ensaios de voo de dispositivos híper-sustentadores e de controlo de rolamento. Foram desenhados novos perfis de baixo Reynolds bem como um flap Fowler com um inovador mecanismo de extensão. Este mecanismo foi construído com tecnologia de impressão 3D. Vários testes foram feitos para diferentes baterias de forma a maximizar a potência do sistema propulsivo. Além disso, pela primeira vez uma equipa da Universidade da Beira Interior utilizou tecnologia de moldes para construir o avião em plásticos reforçados com fibra de carbono. Diversos atrasos e imprevistos levaram a que a aeronave não estivesse plenamente desenvolvida e pronta para participar na competição.Silvestre, Miguel Ângelo RodriguesuBibliorumGomes, Alexandra Almeida2019-12-18T16:59:20Z2017-11-172017-10-32017-11-17T00:00:00Zinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesisapplication/pdfhttp://hdl.handle.net/10400.6/7950TID:202339874enginfo:eu-repo/semantics/openAccessreponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãoinstacron:RCAAP2023-12-15T09:47:37Zoai:ubibliorum.ubi.pt:10400.6/7950Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-20T00:48:23.720662Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãofalse
dc.title.none.fl_str_mv Development of an UAV for the Air Cargo Challenge 2017 Competition
title Development of an UAV for the Air Cargo Challenge 2017 Competition
spellingShingle Development of an UAV for the Air Cargo Challenge 2017 Competition
Gomes, Alexandra Almeida
Air Cargo Challenge
Aircraft
Airfoil
Fowler Flap
Low Reynolds Number
Uav
Xflr5
Xfoil
Domínio/Área Científica::Engenharia e Tecnologia::Engenharia Aeronáutica
title_short Development of an UAV for the Air Cargo Challenge 2017 Competition
title_full Development of an UAV for the Air Cargo Challenge 2017 Competition
title_fullStr Development of an UAV for the Air Cargo Challenge 2017 Competition
title_full_unstemmed Development of an UAV for the Air Cargo Challenge 2017 Competition
title_sort Development of an UAV for the Air Cargo Challenge 2017 Competition
author Gomes, Alexandra Almeida
author_facet Gomes, Alexandra Almeida
author_role author
dc.contributor.none.fl_str_mv Silvestre, Miguel Ângelo Rodrigues
uBibliorum
dc.contributor.author.fl_str_mv Gomes, Alexandra Almeida
dc.subject.por.fl_str_mv Air Cargo Challenge
Aircraft
Airfoil
Fowler Flap
Low Reynolds Number
Uav
Xflr5
Xfoil
Domínio/Área Científica::Engenharia e Tecnologia::Engenharia Aeronáutica
topic Air Cargo Challenge
Aircraft
Airfoil
Fowler Flap
Low Reynolds Number
Uav
Xflr5
Xfoil
Domínio/Área Científica::Engenharia e Tecnologia::Engenharia Aeronáutica
description The present dissertation reports the development of an unmanned remotely piloted aircraft for the Air Cargo Challenge 2017 competition. Air Cargo Challenge is a Design, Build, Fly Aeronautical Engineering competition held in Europe every two years. Given the frequent participation of the Department of Aerospace Sciences from University of Beira Interior in this competition and considering the lack of documentation regarding these participations, this Master of Science Dissertation aims to transmit the accumulated knowledge to future teams and the UAV development community. The aircraft was developed using computer aided engineering tools in the greatest possible extent. The tools used for the development effort include: OpenFOAM®, XFOIL/XFLR5 for airfoil development and detailed wing design and analysis; 3D CAD software as Dassault Systems CATIA® V5 and SolidWorks®; CNC rapid prototyping like 3D printing and CNC hot wire foam core cutting. Experimental test rigs were developed for different studies regarding LiPo batteries for the propulsion and flight testing of high lift devices and roll control. New low Reynolds number airfoils were designed as well as a Fowler flap with an innovative extension mechanism. This mechanism was built using 3D printing technology. Several tests were performed to different batteries to maximize propulsive system power. Furthermore, for the first time in an Air Cargo Challenge, a University of Beira Interior team used mould technology to build the aircraft in carbon fibre reinforced plastics. Several delays and mishaps prevented the development of the aircraft from being completely ready for the competition.
publishDate 2017
dc.date.none.fl_str_mv 2017-11-17
2017-10-3
2017-11-17T00:00:00Z
2019-12-18T16:59:20Z
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dc.identifier.uri.fl_str_mv http://hdl.handle.net/10400.6/7950
TID:202339874
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instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação
instacron:RCAAP
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