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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Sitemtc-m16.sid.inpe.br (namespace prefix: upn:KLE2JH)
Repositóriosid.inpe.br/marciana/2004/01.08.14.59
Última Atualização2009:03.11.18.14.21 (UTC) administrator
Repositório de Metadadossid.inpe.br/marciana/2004/01.08.14.59.17
Última Atualização dos Metadados2018:06.05.01.20.41 (UTC) administrator
Chave SecundáriaINPE-10383-PRE/5883
Chave de CitaçãoLeiteBast:2003:NuEvCo
TítuloNumerical evaluation of the combustion process in a vitiated air generator of a direct-connected supersonic combustion research facility
FormatoOn-line
Ano2003
Data de Acesso07 nov. 2026
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho574 KiB
2. Contextualização
Autor1 Leite, Valéria Serrano Faillace Oliveira
2 Bastos Netto, Demetrio
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JGTG
Grupo1 LCP-INPE-MCT-BR
Afiliação1 Instituto de Estudos Avançados (IEAv / CTA) - Rodovia dos Tamoios Km. 5, 5, São José dos Campos, CEP: 12228-840
2 Combustão, Instituto nacional de Pesquisas Espaciais. laboratório Associado de
Nome do EventoInternational Congress of Mathematical Engineering, 17.
Localização do EventoSão Paulo
Data10-14 nov. 2003
Editora (Publisher)ABCM
Título do LivroAnais
Acervo Hospedeirosid.inpe.br/banon/2003/08.15.17.40 upn:KLE2JH
Histórico (UTC)2008-06-10 23:02:15 :: administrator -> marciana ::
2009-03-11 18:14:22 :: marciana -> administrator ::
2018-06-05 01:20:41 :: administrator -> marciana :: 2003
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Palavras-Chavesupersonic combustion
hypersonic flight
scramjets
ram accelerators
ResumoThe direct-connected supersonic combustion research facility, now being assembled at the Combustion and Propulsion Laboratory (LCP) of the National Institute for Space Research (INPE) with the Institute for Advanced Studies (IEAv/CTA), consists basically of a vitiated air generator unit and a nozzle which is to be directly coupled to the supersonic combustor to be tested. The flow at the combustor inlet should simulate the conditions of the air behind the oblique or conical shock waves over wedges, cones or other axisymmetric surfaces used to compress the freestream flow in supersonic combustion air breathing systems like scramjets or ram accelerators. This is a high temperature, supersonic flow. The nozzle is designed to generate the desired Mach number and the air high temperature is obtained in the vitiated air generator by combustion. The evaluation of the combustion efficiency in the vitiated air generator shows the behavior of the fuel and air mass flow rates and the equivalence ratio needed to better control the stagnation temperature and the products composition. This control allows for the conditions achieved at the nozzle exit to be close to those of the air entering the combustor during actual flight operation, i.e., those of the air behind the oblique or conical shock waves formed at the entrance of scramjet engines or in front of the nose cone of ram accelerators in the super detonative mode. This paper discusses the combustion process in the vitiated air generator with fuels such as benzene (C6H6) and hydrogen (H2) using the packages PSR and PLUG of the software CHEMKIN III. Supersonic Combustion, Hypersonic Flight, Scramjets, Ram Accelerators.
ÁreaCOMB
Arranjourlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Numerical evaluation of...
Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreementnão têm arquivos
4. Condições de acesso e uso
URI dos dadosupn:KLE2JH:sid.inpe.br/marciana/2004/01.08.14.59
URL dos dadoshttp://urlib.net/ibi/sid.inpe.br/marciana/2004/01.08.14.59
URL dos dados zipadoshttp://urlib.net/zip/sid.inpe.br/marciana/2004/01.08.14.59
Idiomaen
Arquivo Alvonumerical.pdf
Grupo de Usuáriosadministrator
marciana
Visibilidadeshown
Detentor da CópiaSID/SCD
Permissão de Leituraallow from all
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/3ET38CH
Lista de Itens Citandosid.inpe.br/bibdigital/2013/09.25.23.49 - 76
sid.inpe.br/mtc-m21/2012/07.13.14.44.29 - 12
sid.inpe.br/mtc-m21/2012/06.05.15.34.41 - 2
sid.inpe.br/banon/2003/08.15.17.40.18 - 2
6. Notas
Campos Vaziosarchivingpolicy archivist callnumber copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor electronicmailaddress identifier isbn issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress readergroup rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume
7. Controle da descrição
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