Experimental aerodynamic drag analysis of a rocket model with straight and angled fins

Página do item simplificado Estatísticas
dc.contributor.advisorMarinho, George Santos
dc.contributor.advisor-co1Azoni, Giovani Pozza
dc.contributor.advisor-co1IDhttps://orcid.org/0009-0004-0950-1298pt_BR
dc.contributor.advisor-co1Latteshttp://lattes.cnpq.br/1525938463255303pt_BR
dc.contributor.advisorIDhttps://orcid.org/0000-0003-3565-4744pt_BR
dc.contributor.advisorLatteshttp://lattes.cnpq.br/0490476694313938pt_BR
dc.contributor.authorSantos, Luísa Mirelle Costa dos
dc.contributor.authorIDhttps://orcid.org/0000-0001-5895-3160pt_BR
dc.contributor.authorLatteshttp://lattes.cnpq.br/0300209367448693pt_BR
dc.contributor.referees1Marinho, George Santos
dc.contributor.referees1IDhttps://orcid.org/0000-0003-3565-4744pt_BR
dc.contributor.referees1Latteshttp://lattes.cnpq.br/0490476694313938pt_BR
dc.contributor.referees2Silva, Douglas do Nascimento
dc.contributor.referees2IDhttps://orcid.org/0000-0001-5934-9491pt_BR
dc.contributor.referees2Latteshttp://lattes.cnpq.br/0841120842454720pt_BR
dc.contributor.referees3Sousa, Roberto Silva de
dc.contributor.referees3Latteshttp://lattes.cnpq.br/4012782800846844pt_BR
dc.date.accessioned2023-07-20T17:12:58Z
dc.date.available2023-07-20T17:12:58Z
dc.date.issued2023-07-12
dc.description.resumoThe drag generated by the fins attached to a model rocket was studied experimentally. Rocket models (designed for 100 meters of apogee) were tested in a didactic wind tunnel in two situations: with straight and angular fins (at 5° and 10°), under wind speeds of 3, 4, 5 and 6 m/s. The results obtained experimentally were compared to the results of the theoretical analysis, allowing a better understanding of the effect of the fins.pt_BR
dc.identifier.citationSANTOS, Luísa Mirelle Costa dos. Experimental aerodynamic drag analysis of a rocket model with straight and angled fins. Orientador: George Santos Marinho. 2023. 8f. Trabalho de Conclusão de Curso (Graduação em Engenharia Mecânica) - Departamento de Engenharia Mecânica, Universidade Federal do Rio Grande do Norte, Natal, 2023.pt_BR
dc.identifier.urihttps://repositorio.ufrn.br/handle/123456789/53939
dc.languageenpt_BR
dc.publisherUniversidade Federal do Rio Grande do Nortept_BR
dc.publisher.countryBrasilpt_BR
dc.publisher.departmentEngenharia Mecânicapt_BR
dc.publisher.initialsUFRNpt_BR
dc.publisher.programEngenharia Mecânicapt_BR
dc.rightsAttribution-NoDerivs 3.0 Brazil*
dc.rights.urihttp://creativecommons.org/licenses/by-nd/3.0/br/*
dc.subjectRocket modelspt_BR
dc.subjectDidactic wind tunnelpt_BR
dc.subjectFinspt_BR
dc.subjectDrag forcept_BR
dc.subject.cnpqCNPQ::ENGENHARIAS::ENGENHARIA MECANICApt_BR
dc.titleExperimental aerodynamic drag analysis of a rocket model with straight and angled finspt_BR
dc.typebachelorThesispt_BR

Arquivos

Pacote Original

Agora exibindo 1 - 1 de 1
Nenhuma Miniatura disponível
Nome:
Santos L_Azoni G_Marinho G_2023.pdf
Tamanho:
850.82 KB
Formato:
Adobe Portable Document Format
Nenhuma Miniatura disponível
Baixar

Licença do Pacote

Agora exibindo 1 - 1 de 1
Nenhuma Miniatura disponível
Nome:
license.txt
Tamanho:
1.45 KB
Formato:
Item-specific license agreed upon to submission
Nenhuma Miniatura disponível
Baixar

Coleções

CT - TCC - Engenharia Mecânica
Repositório Institucional - UFRN Campus Universitário Lagoa NovaCEP 59078-970 Caixa postal 1524 Natal/RN - BrasilUniversidade Federal do Rio Grande do Norte© Copyright 2025. Todos os direitos reservados.
Contato+55 (84) 3342-2260 - R232Setor de Repositórios Digitaisrepositorio@bczm.ufrn.br
DSpaceIBICT
OasisBR
LAReferencia
Customizado pela CAT - BCZM