The use of molecular spectra simulation for diagnostics of reactive flows
Main Author: | |
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Publication Date: | 2011 |
Other Authors: | , , , , , |
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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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 |
_version_ |
1834482554210615296 |