Aerodynamic analysis of a scramjet for atmospheric flight

Página do item simplificado Estatísticas
dc.contributor.advisorToro, Paulo Gilberto de Paula
dc.contributor.advisor-co1George Santos Marinhopt_BR
dc.contributor.authorSilva, Elder Samuel Taveira da
dc.contributor.referees1Borba, Gilvan Luiz
dc.contributor.referees2Cavalcanti, Eduardo José Cidade
dc.date.accessioned2018-12-14T12:56:13Z
dc.date.accessioned2021-10-05T16:02:37Z
dc.date.available2018-12-14T12:56:13Z
dc.date.available2021-10-05T16:02:37Z
dc.date.issued2018-11
dc.description.resumoThis paper presents an aerodynamic conception of an academic scramjet designed for a flight at 6.2 km of altitude with a speed corresponding to Mach number 4.18, which will be coupled to the intermediate training rocket (FTI) of the Barreira do Inferno Launch Center (CLBI) in Rio Grande do Norte (RN), Brazil. The current means of access to space is limited by the quantity of fuel that rockets need to take to get out of the dense layers of the atmosphere, which causes little payload to be boarded, limiting aerospace activities. The scramjet technological demonstrator is being studied as a new technology of access to space, as this technology proposes a new system of airbreathing propulsion. The proposed academic scramjet will be coupled in the FTI, functioning as a second stage in order to obtain more power during the flight. Calculations were made in the geometry variation in order to select the best compression and expansion section for the scramjet, with heat addition. In the compression section, only one configuration with three tamps was considered. The analytical results were compared with simulation results.pt_BR
dc.identifier20170009070pt_BR
dc.identifier.citationSILVA, Elder Samuel Taveira da. Aerodynamic analysis of a scramjet for atmospheric flight 2018. 12f. Trabalho de Conclusão de Curso (Graduação em Engenharia Mecânica) - Centro de Tecnologia, Curso de Engenharia Mecânica, Universidade Federal do Rio Grande do Norte, Natal, 2018.pt_BR
dc.identifier.urihttps://repositorio.ufrn.br/handle/123456789/43070
dc.languageenpt_BR
dc.language.isoenpt_BR
dc.publisherUniversidade Federal do Rio Grande do Nortept_BR
dc.publisher.countryBrasilpt_BR
dc.publisher.departmentEngenharia Mecânicapt_BR
dc.publisher.initialsUFRNpt_BR
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 Brazil*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/br/*
dc.subjectScramjetpt_BR
dc.subjectHypersonicspt_BR
dc.subjectShock wavespt_BR
dc.subjectThermal propertiespt_BR
dc.subjectNumerical simulationpt_BR
dc.titleAerodynamic analysis of a scramjet for atmospheric flightpt_BR
dc.typebachelorThesispt_BR

Arquivos

Pacote Original

Agora exibindo 1 - 1 de 1
Nenhuma Miniatura disponível
Nome:
AerodynamicAnalisys_Silva_2018.pdf
Tamanho:
2.98 MB
Formato:
Adobe Portable Document Format
Descrição:
AerodynamicAnalisys_Silva_2018
Nenhuma Miniatura disponível
Baixar

Licença do Pacote

Agora exibindo 1 - 1 de 1
Nenhuma Miniatura disponível
Nome:
license.txt
Tamanho:
714 B
Formato:
Plain Text
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