Aeroelastic analysis including servomechanism transfer functions.
Ano de defesa: | 2001 |
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Autor(a) principal: | |
Orientador(a): | |
Banca de defesa: | |
Tipo de documento: | Dissertação |
Tipo de acesso: | Acesso aberto |
Idioma: | eng |
Instituição de defesa: |
Instituto Tecnológico de Aeronáutica
|
Programa de Pós-Graduação: |
Não Informado pela instituição
|
Departamento: |
Não Informado pela instituição
|
País: |
Não Informado pela instituição
|
Palavras-chave em Português: | |
Link de acesso: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2461 |
Resumo: | This study presents an aeroelastic analysis including the servomechanism transfer functions. The aeroelastic (flutter) behavior of the dynamic structure is analyzed when a feedback control is introduced. A structural dynamic model is elaborated together with an aerodynamic model in order to obtain the aeroelastic model. A feedback control model was then implemented in the aeroelastic model to obtain the servomechanism model that is the focus of the analysis. A parametric study was made to analyze the behavior of the aeroelastic model with the feedback control. This parametric study consists in the variation of the parameters (gains of the transfer functions), which compound the feedback control model, and for each variation, a stability analysis (flutter analysis) was made and the results were plotted in the "v-g-f" graphs for obtaining the stability boundaries. From these graphs the stability tendencies with the introduction of the control system in the analysis could be determined. |
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oai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2461 |
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ITA |
network_name_str |
Biblioteca Digital de Teses e Dissertações do ITA |
spelling |
Aeroelastic analysis including servomechanism transfer functions.AeroelasticidadeAnálise estrutural dinâmicaEstrutura de aeronavesServomecanismosControle com realimentaçãoFunções de transferênciaVibração aeroelásticaMecânica dos sólidosAerodinâmicaEngenharia eletrônicaEngenharia mecânicaThis study presents an aeroelastic analysis including the servomechanism transfer functions. The aeroelastic (flutter) behavior of the dynamic structure is analyzed when a feedback control is introduced. A structural dynamic model is elaborated together with an aerodynamic model in order to obtain the aeroelastic model. A feedback control model was then implemented in the aeroelastic model to obtain the servomechanism model that is the focus of the analysis. A parametric study was made to analyze the behavior of the aeroelastic model with the feedback control. This parametric study consists in the variation of the parameters (gains of the transfer functions), which compound the feedback control model, and for each variation, a stability analysis (flutter analysis) was made and the results were plotted in the "v-g-f" graphs for obtaining the stability boundaries. From these graphs the stability tendencies with the introduction of the control system in the analysis could be determined. Instituto Tecnológico de AeronáuticaMaher Nasr Bismarck-NasrMarcelo Nogueira2001-00-00info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2461reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:04:48Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2461http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:39:13.856Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
dc.title.none.fl_str_mv |
Aeroelastic analysis including servomechanism transfer functions. |
title |
Aeroelastic analysis including servomechanism transfer functions. |
spellingShingle |
Aeroelastic analysis including servomechanism transfer functions. Marcelo Nogueira Aeroelasticidade Análise estrutural dinâmica Estrutura de aeronaves Servomecanismos Controle com realimentação Funções de transferência Vibração aeroelástica Mecânica dos sólidos Aerodinâmica Engenharia eletrônica Engenharia mecânica |
title_short |
Aeroelastic analysis including servomechanism transfer functions. |
title_full |
Aeroelastic analysis including servomechanism transfer functions. |
title_fullStr |
Aeroelastic analysis including servomechanism transfer functions. |
title_full_unstemmed |
Aeroelastic analysis including servomechanism transfer functions. |
title_sort |
Aeroelastic analysis including servomechanism transfer functions. |
author |
Marcelo Nogueira |
author_facet |
Marcelo Nogueira |
author_role |
author |
dc.contributor.none.fl_str_mv |
Maher Nasr Bismarck-Nasr |
dc.contributor.author.fl_str_mv |
Marcelo Nogueira |
dc.subject.por.fl_str_mv |
Aeroelasticidade Análise estrutural dinâmica Estrutura de aeronaves Servomecanismos Controle com realimentação Funções de transferência Vibração aeroelástica Mecânica dos sólidos Aerodinâmica Engenharia eletrônica Engenharia mecânica |
topic |
Aeroelasticidade Análise estrutural dinâmica Estrutura de aeronaves Servomecanismos Controle com realimentação Funções de transferência Vibração aeroelástica Mecânica dos sólidos Aerodinâmica Engenharia eletrônica Engenharia mecânica |
dc.description.none.fl_txt_mv |
This study presents an aeroelastic analysis including the servomechanism transfer functions. The aeroelastic (flutter) behavior of the dynamic structure is analyzed when a feedback control is introduced. A structural dynamic model is elaborated together with an aerodynamic model in order to obtain the aeroelastic model. A feedback control model was then implemented in the aeroelastic model to obtain the servomechanism model that is the focus of the analysis. A parametric study was made to analyze the behavior of the aeroelastic model with the feedback control. This parametric study consists in the variation of the parameters (gains of the transfer functions), which compound the feedback control model, and for each variation, a stability analysis (flutter analysis) was made and the results were plotted in the "v-g-f" graphs for obtaining the stability boundaries. From these graphs the stability tendencies with the introduction of the control system in the analysis could be determined. |
description |
This study presents an aeroelastic analysis including the servomechanism transfer functions. The aeroelastic (flutter) behavior of the dynamic structure is analyzed when a feedback control is introduced. A structural dynamic model is elaborated together with an aerodynamic model in order to obtain the aeroelastic model. A feedback control model was then implemented in the aeroelastic model to obtain the servomechanism model that is the focus of the analysis. A parametric study was made to analyze the behavior of the aeroelastic model with the feedback control. This parametric study consists in the variation of the parameters (gains of the transfer functions), which compound the feedback control model, and for each variation, a stability analysis (flutter analysis) was made and the results were plotted in the "v-g-f" graphs for obtaining the stability boundaries. From these graphs the stability tendencies with the introduction of the control system in the analysis could be determined. |
publishDate |
2001 |
dc.date.none.fl_str_mv |
2001-00-00 |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/masterThesis |
status_str |
publishedVersion |
format |
masterThesis |
dc.identifier.uri.fl_str_mv |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2461 |
url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2461 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
application/pdf |
dc.publisher.none.fl_str_mv |
Instituto Tecnológico de Aeronáutica |
publisher.none.fl_str_mv |
Instituto Tecnológico de Aeronáutica |
dc.source.none.fl_str_mv |
reponame:Biblioteca Digital de Teses e Dissertações do ITA instname:Instituto Tecnológico de Aeronáutica instacron:ITA |
reponame_str |
Biblioteca Digital de Teses e Dissertações do ITA |
collection |
Biblioteca Digital de Teses e Dissertações do ITA |
instname_str |
Instituto Tecnológico de Aeronáutica |
instacron_str |
ITA |
institution |
ITA |
repository.name.fl_str_mv |
Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica |
repository.mail.fl_str_mv |
|
subject_por_txtF_mv |
Aeroelasticidade Análise estrutural dinâmica Estrutura de aeronaves Servomecanismos Controle com realimentação Funções de transferência Vibração aeroelástica Mecânica dos sólidos Aerodinâmica Engenharia eletrônica Engenharia mecânica |
_version_ |
1706805000031698944 |