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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/marciana/2004/01.08.14.59
Last Update2009:03.11.18.14.21 (UTC) administrator
Metadata Repositorysid.inpe.br/marciana/2004/01.08.14.59.17
Metadata Last Update2018:06.05.01.20.41 (UTC) administrator
Secondary KeyINPE-10383-PRE/5883
Citation KeyLeiteBast:2003:NuEvCo
TitleNumerical evaluation of the combustion process in a vitiated air generator of a direct-connected supersonic combustion research facility
FormatOn-line
Year2003
Access Date2024, May 18
Secondary TypePRE CI
Number of Files1
Size574 KiB
2. Context
Author1 Leite, Valéria Serrano Faillace Oliveira
2 Bastos Netto, Demetrio
Resume Identifier1
2 8JMKD3MGP5W/3C9JGTG
Group1 LCP-INPE-MCT-BR
Affiliation1 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
Conference NameInternational Congress of Mathematical Engineering, 17.
Conference LocationSão Paulo
Date10-14 nov. 2003
PublisherABCM
Book TitleAnais
History (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. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Keywordssupersonic combustion
hypersonic flight
scramjets
ram accelerators
AbstractThe 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.
AreaCOMB
Arrangementurlib.net > LABCP > Numerical evaluation of...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/sid.inpe.br/marciana/2004/01.08.14.59
zipped data URLhttp://urlib.net/zip/sid.inpe.br/marciana/2004/01.08.14.59
Languageen
Target Filenumerical.pdf
User Groupadministrator
marciana
Visibilityshown
Copy HolderSID/SCD
Read Permissionallow from all
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.44.29 1
sid.inpe.br/bibdigital/2013/09.25.23.49 1
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
Empty Fieldsarchivingpolicy 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. Description control
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