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Please use this identifier to cite or link to this item: http://acervodigital.unesp.br/handle/11449/72271
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dc.contributor.authorPassaro, Angelo-
dc.contributor.authorCarinhana, Dermeval-
dc.contributor.authorGonçalves, Enizete Aparecida-
dc.contributor.authorda Silva, Marcio Moreira-
dc.contributor.authorGuimarães, Ana Paula Lasmar-
dc.contributor.authorAbe, Nancy Mieko-
dc.contributor.authordos Santos, Alberto Monteiro-
dc.date.accessioned2014-05-27T11:25:27Z-
dc.date.accessioned2016-10-25T18:33:30Z-
dc.date.available2014-05-27T11:25:27Z-
dc.date.available2016-10-25T18:33:30Z-
dc.date.issued2011-01-01-
dc.identifierhttp://dx.doi.org/10.5028/jatm.2011.03019610-
dc.identifier.citationJournal of Aerospace Technology and Management, v. 3, n. 1, p. 13-20, 2011.-
dc.identifier.issn1984-9648-
dc.identifier.issn2175-9146-
dc.identifier.urihttp://hdl.handle.net/11449/72271-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/72271-
dc.description.abstractThe C 2 * radical is used as a system probe tool to the reactive flow diagnostic, and it was chosen due to its large occurrence in plasma and combustion in aeronautics and aerospace applications. The rotational temperatures of C 2 * species were determined by the comparison between experimental and theoretical data. The simulation code was developed by the authors, using C++ language and the object oriented paradigm, and it includes a set of new tools that increase the efficacy of the C 2 * probe to determine the rotational temperature of the system. A brute force approach for the determination of spectral parameters was adopted in this version of the computer code. The statistical parameter c 2 was used as an objective criterion to determine the better match of experimental and synthesized spectra. The results showed that the program works even with low-quality experimental data, typically collected from in situ airborne compact apparatus. The technique was applied to flames of a Bunsen burner, and the rotational temperature of ca. 2100 K was calculated.en
dc.format.extent13-20-
dc.language.isoeng-
dc.sourceScopus-
dc.subjectCombustion control-
dc.subjectComputer programs-
dc.subjectComputerized simulation-
dc.subjectOptical emission spectra-
dc.subjectRotational spectra-
dc.subjectAerospace applications-
dc.subjectCombustion-
dc.subjectComputer simulation languages-
dc.subjectEmission spectroscopy-
dc.subjectFlow visualization-
dc.subjectMass spectrometry-
dc.subjectMolecular spectroscopy-
dc.subjectProbes-
dc.subjectProgram diagnostics-
dc.subjectStatistical methods-
dc.subjectComputer software-
dc.titleThe use of molecular spectra simulation for diagnostics of reactive flowsen
dc.typeoutro-
dc.contributor.institutionSão José dos Campos-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationInstituto de Estudos Avançados São José dos Campos-
dc.description.affiliationInstituto Nacional de Pesquisas Espaciais São José dos Campos-
dc.description.affiliationUniversidade Estadual Paulista, Guaratinguetá-
dc.description.affiliationUnespUniversidade Estadual Paulista, Guaratinguetá-
dc.identifier.doi10.5028/jatm.2011.03019610-
dc.rights.accessRightsAcesso aberto-
dc.identifier.file2-s2.0-79955935553.pdf-
dc.relation.ispartofJournal of Aerospace Technology and Management-
dc.identifier.scopus2-s2.0-79955935553-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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