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The use of molecular spectra simulation for diagnostics of reactive flows

Bibliographic Details
Main Author: Passaro, Angelo
Publication Date: 2011
Other Authors: Carinhana, Dermeval, Gonçalves, Enizete Aparecida, da Silva, Marcio Moreira, Guimarães, Ana Paula Lasmar [UNESP], Abe, Nancy Mieko, dos Santos, Alberto Monteiro
Format: Article
Language: eng
Source: Repositório Institucional da UNESP
Download full: http://dx.doi.org/10.5028/jatm.2011.03019610
http://hdl.handle.net/11449/72271
Summary: 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.
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spelling The use of molecular spectra simulation for diagnostics of reactive flowsCombustion controlComputer programsComputerized simulationOptical emission spectraRotational spectraAerospace applicationsCombustionComputer simulation languagesEmission spectroscopyFlow visualizationMass spectrometryMolecular spectroscopyProbesProgram diagnosticsStatistical methodsComputer softwareThe 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.Instituto de Estudos Avançados São José dos CamposInstituto Nacional de Pesquisas Espaciais São José dos CamposUniversidade Estadual Paulista, GuaratinguetáUniversidade Estadual Paulista, GuaratinguetáSão José dos CamposUniversidade Estadual Paulista (Unesp)Passaro, AngeloCarinhana, DermevalGonçalves, Enizete Aparecidada Silva, Marcio MoreiraGuimarães, Ana Paula Lasmar [UNESP]Abe, Nancy Miekodos Santos, Alberto Monteiro2014-05-27T11:25:27Z2014-05-27T11:25:27Z2011-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article13-20application/pdfhttp://dx.doi.org/10.5028/jatm.2011.03019610Journal of Aerospace Technology and Management, v. 3, n. 1, p. 13-20, 2011.1984-96482175-9146http://hdl.handle.net/11449/7227110.5028/jatm.2011.030196102-s2.0-799559355532-s2.0-79955935553.pdfScopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengJournal of Aerospace Technology and Management0,2040,204info:eu-repo/semantics/openAccess2025-04-03T14:59:28Zoai:repositorio.unesp.br:11449/72271Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestrepositoriounesp@unesp.bropendoar:29462025-04-03T14:59:28Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv The use of molecular spectra simulation for diagnostics of reactive flows
title The use of molecular spectra simulation for diagnostics of reactive flows
spellingShingle The use of molecular spectra simulation for diagnostics of reactive flows
Passaro, Angelo
Combustion control
Computer programs
Computerized simulation
Optical emission spectra
Rotational spectra
Aerospace applications
Combustion
Computer simulation languages
Emission spectroscopy
Flow visualization
Mass spectrometry
Molecular spectroscopy
Probes
Program diagnostics
Statistical methods
Computer software
title_short The use of molecular spectra simulation for diagnostics of reactive flows
title_full The use of molecular spectra simulation for diagnostics of reactive flows
title_fullStr The use of molecular spectra simulation for diagnostics of reactive flows
title_full_unstemmed The use of molecular spectra simulation for diagnostics of reactive flows
title_sort The use of molecular spectra simulation for diagnostics of reactive flows
author Passaro, Angelo
author_facet Passaro, Angelo
Carinhana, Dermeval
Gonçalves, Enizete Aparecida
da Silva, Marcio Moreira
Guimarães, Ana Paula Lasmar [UNESP]
Abe, Nancy Mieko
dos Santos, Alberto Monteiro
author_role author
author2 Carinhana, Dermeval
Gonçalves, Enizete Aparecida
da Silva, Marcio Moreira
Guimarães, Ana Paula Lasmar [UNESP]
Abe, Nancy Mieko
dos Santos, Alberto Monteiro
author2_role author
author
author
author
author
author
dc.contributor.none.fl_str_mv São José dos Campos
Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Passaro, Angelo
Carinhana, Dermeval
Gonçalves, Enizete Aparecida
da Silva, Marcio Moreira
Guimarães, Ana Paula Lasmar [UNESP]
Abe, Nancy Mieko
dos Santos, Alberto Monteiro
dc.subject.por.fl_str_mv Combustion control
Computer programs
Computerized simulation
Optical emission spectra
Rotational spectra
Aerospace applications
Combustion
Computer simulation languages
Emission spectroscopy
Flow visualization
Mass spectrometry
Molecular spectroscopy
Probes
Program diagnostics
Statistical methods
Computer software
topic Combustion control
Computer programs
Computerized simulation
Optical emission spectra
Rotational spectra
Aerospace applications
Combustion
Computer simulation languages
Emission spectroscopy
Flow visualization
Mass spectrometry
Molecular spectroscopy
Probes
Program diagnostics
Statistical methods
Computer software
description 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.
publishDate 2011
dc.date.none.fl_str_mv 2011-01-01
2014-05-27T11:25:27Z
2014-05-27T11:25:27Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.5028/jatm.2011.03019610
Journal of Aerospace Technology and Management, v. 3, n. 1, p. 13-20, 2011.
1984-9648
2175-9146
http://hdl.handle.net/11449/72271
10.5028/jatm.2011.03019610
2-s2.0-79955935553
2-s2.0-79955935553.pdf
url http://dx.doi.org/10.5028/jatm.2011.03019610
http://hdl.handle.net/11449/72271
identifier_str_mv Journal of Aerospace Technology and Management, v. 3, n. 1, p. 13-20, 2011.
1984-9648
2175-9146
10.5028/jatm.2011.03019610
2-s2.0-79955935553
2-s2.0-79955935553.pdf
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Journal of Aerospace Technology and Management
0,204
0,204
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 13-20
application/pdf
dc.source.none.fl_str_mv Scopus
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv repositoriounesp@unesp.br
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