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http://acervodigital.unesp.br/handle/11449/72271
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DC Field | Value | Language |
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dc.contributor.author | Passaro, Angelo | - |
dc.contributor.author | Carinhana, Dermeval | - |
dc.contributor.author | Gonçalves, Enizete Aparecida | - |
dc.contributor.author | da Silva, Marcio Moreira | - |
dc.contributor.author | Guimarães, Ana Paula Lasmar | - |
dc.contributor.author | Abe, Nancy Mieko | - |
dc.contributor.author | dos Santos, Alberto Monteiro | - |
dc.date.accessioned | 2014-05-27T11:25:27Z | - |
dc.date.accessioned | 2016-10-25T18:33:30Z | - |
dc.date.available | 2014-05-27T11:25:27Z | - |
dc.date.available | 2016-10-25T18:33:30Z | - |
dc.date.issued | 2011-01-01 | - |
dc.identifier | http://dx.doi.org/10.5028/jatm.2011.03019610 | - |
dc.identifier.citation | Journal of Aerospace Technology and Management, v. 3, n. 1, p. 13-20, 2011. | - |
dc.identifier.issn | 1984-9648 | - |
dc.identifier.issn | 2175-9146 | - |
dc.identifier.uri | http://hdl.handle.net/11449/72271 | - |
dc.identifier.uri | http://acervodigital.unesp.br/handle/11449/72271 | - |
dc.description.abstract | The 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.extent | 13-20 | - |
dc.language.iso | eng | - |
dc.source | Scopus | - |
dc.subject | Combustion control | - |
dc.subject | Computer programs | - |
dc.subject | Computerized simulation | - |
dc.subject | Optical emission spectra | - |
dc.subject | Rotational spectra | - |
dc.subject | Aerospace applications | - |
dc.subject | Combustion | - |
dc.subject | Computer simulation languages | - |
dc.subject | Emission spectroscopy | - |
dc.subject | Flow visualization | - |
dc.subject | Mass spectrometry | - |
dc.subject | Molecular spectroscopy | - |
dc.subject | Probes | - |
dc.subject | Program diagnostics | - |
dc.subject | Statistical methods | - |
dc.subject | Computer software | - |
dc.title | The use of molecular spectra simulation for diagnostics of reactive flows | en |
dc.type | outro | - |
dc.contributor.institution | São José dos Campos | - |
dc.contributor.institution | Universidade Estadual Paulista (UNESP) | - |
dc.description.affiliation | Instituto de Estudos Avançados São José dos Campos | - |
dc.description.affiliation | Instituto Nacional de Pesquisas Espaciais São José dos Campos | - |
dc.description.affiliation | Universidade Estadual Paulista, Guaratinguetá | - |
dc.description.affiliationUnesp | Universidade Estadual Paulista, Guaratinguetá | - |
dc.identifier.doi | 10.5028/jatm.2011.03019610 | - |
dc.rights.accessRights | Acesso aberto | - |
dc.identifier.file | 2-s2.0-79955935553.pdf | - |
dc.relation.ispartof | Journal of Aerospace Technology and Management | - |
dc.identifier.scopus | 2-s2.0-79955935553 | - |
Appears in Collections: | Artigos, TCCs, Teses e Dissertações da Unesp |
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