Application of piezoelectric materials as sensor and actuator for aeroelastic investigation
Autor(a) principal: | |
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Data de Publicação: | 2014 |
Tipo de documento: | Dissertação |
Idioma: | eng |
Título da fonte: | Biblioteca Digital de Teses e Dissertações do ITA |
Texto Completo: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3038 |
Resumo: | This dissertation aims to apply piezoelectric materials as actuator and sensor to perform aeroelastic analysis. Two semi-span wing models based on flat plates with different characteristics were tested using PZT (Lead Zirconate Titanate) as actuator, PVDF (Polyvinylidene Fluoride) as sensor and the results were compared with vibrometer laser results. An aluminum model with a ballast on the wing tip, whose its location can be modified was tested in experimental modal analysis. Using the aluninum model, an investigation about aeroelastic behaviour was conducted in wind tunnel and the V-g/V-f diagram determined. This diagram shows the aeroelastic evolution of the natural frequencies and damping as function of speed (or dynamic pressure). In this aeroelastic analysis, the ability of the PVDF in determining the V-g/V-f diagram was evaluated. A numerical model of composite flat plate was generated considering the piezoelectric instrumentations. The second specimen tested corresponds to composite wing models that are based on laminate composite flat plate. Five models with different fiber orientations were tested in (pure) experimental modal analyses and wind tunnel, hence, the capability of excitation of PZT was verified. Good results were obtained regarding the estimation of natural frequency and damping factor using a single PVDF element. The application of PZT as actuator in the wind tunnel test showed improvement on the data acquisition in terms of noise. However, were observed some characteristics that require careful. As support to experimental tests, several studies were performed. |
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Biblioteca Digital de Teses e Dissertações do ITA |
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Application of piezoelectric materials as sensor and actuator for aeroelastic investigationAeroelasticidadeAnálise estrutural dinâmicaEstruturas de aeronavesVibração aeroelásticaPZTMateriais piezoelétricosAerodinâmicaEngenharia mecânicaEngenharia aeronáuticaThis dissertation aims to apply piezoelectric materials as actuator and sensor to perform aeroelastic analysis. Two semi-span wing models based on flat plates with different characteristics were tested using PZT (Lead Zirconate Titanate) as actuator, PVDF (Polyvinylidene Fluoride) as sensor and the results were compared with vibrometer laser results. An aluminum model with a ballast on the wing tip, whose its location can be modified was tested in experimental modal analysis. Using the aluninum model, an investigation about aeroelastic behaviour was conducted in wind tunnel and the V-g/V-f diagram determined. This diagram shows the aeroelastic evolution of the natural frequencies and damping as function of speed (or dynamic pressure). In this aeroelastic analysis, the ability of the PVDF in determining the V-g/V-f diagram was evaluated. A numerical model of composite flat plate was generated considering the piezoelectric instrumentations. The second specimen tested corresponds to composite wing models that are based on laminate composite flat plate. Five models with different fiber orientations were tested in (pure) experimental modal analyses and wind tunnel, hence, the capability of excitation of PZT was verified. Good results were obtained regarding the estimation of natural frequency and damping factor using a single PVDF element. The application of PZT as actuator in the wind tunnel test showed improvement on the data acquisition in terms of noise. However, were observed some characteristics that require careful. As support to experimental tests, several studies were performed.Instituto Tecnológico de AeronáuticaRoberto Gil Annes da SilvaAdolfo Gomes MartoÉder Luiz Oliveira2014-04-16info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3038reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:05:03Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:3038http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:40:55.81Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
dc.title.none.fl_str_mv |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation |
title |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation |
spellingShingle |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation Éder Luiz Oliveira Aeroelasticidade Análise estrutural dinâmica Estruturas de aeronaves Vibração aeroelástica PZT Materiais piezoelétricos Aerodinâmica Engenharia mecânica Engenharia aeronáutica |
title_short |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation |
title_full |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation |
title_fullStr |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation |
title_full_unstemmed |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation |
title_sort |
Application of piezoelectric materials as sensor and actuator for aeroelastic investigation |
author |
Éder Luiz Oliveira |
author_facet |
Éder Luiz Oliveira |
author_role |
author |
dc.contributor.none.fl_str_mv |
Roberto Gil Annes da Silva Adolfo Gomes Marto |
dc.contributor.author.fl_str_mv |
Éder Luiz Oliveira |
dc.subject.por.fl_str_mv |
Aeroelasticidade Análise estrutural dinâmica Estruturas de aeronaves Vibração aeroelástica PZT Materiais piezoelétricos Aerodinâmica Engenharia mecânica Engenharia aeronáutica |
topic |
Aeroelasticidade Análise estrutural dinâmica Estruturas de aeronaves Vibração aeroelástica PZT Materiais piezoelétricos Aerodinâmica Engenharia mecânica Engenharia aeronáutica |
dc.description.none.fl_txt_mv |
This dissertation aims to apply piezoelectric materials as actuator and sensor to perform aeroelastic analysis. Two semi-span wing models based on flat plates with different characteristics were tested using PZT (Lead Zirconate Titanate) as actuator, PVDF (Polyvinylidene Fluoride) as sensor and the results were compared with vibrometer laser results. An aluminum model with a ballast on the wing tip, whose its location can be modified was tested in experimental modal analysis. Using the aluninum model, an investigation about aeroelastic behaviour was conducted in wind tunnel and the V-g/V-f diagram determined. This diagram shows the aeroelastic evolution of the natural frequencies and damping as function of speed (or dynamic pressure). In this aeroelastic analysis, the ability of the PVDF in determining the V-g/V-f diagram was evaluated. A numerical model of composite flat plate was generated considering the piezoelectric instrumentations. The second specimen tested corresponds to composite wing models that are based on laminate composite flat plate. Five models with different fiber orientations were tested in (pure) experimental modal analyses and wind tunnel, hence, the capability of excitation of PZT was verified. Good results were obtained regarding the estimation of natural frequency and damping factor using a single PVDF element. The application of PZT as actuator in the wind tunnel test showed improvement on the data acquisition in terms of noise. However, were observed some characteristics that require careful. As support to experimental tests, several studies were performed. |
description |
This dissertation aims to apply piezoelectric materials as actuator and sensor to perform aeroelastic analysis. Two semi-span wing models based on flat plates with different characteristics were tested using PZT (Lead Zirconate Titanate) as actuator, PVDF (Polyvinylidene Fluoride) as sensor and the results were compared with vibrometer laser results. An aluminum model with a ballast on the wing tip, whose its location can be modified was tested in experimental modal analysis. Using the aluninum model, an investigation about aeroelastic behaviour was conducted in wind tunnel and the V-g/V-f diagram determined. This diagram shows the aeroelastic evolution of the natural frequencies and damping as function of speed (or dynamic pressure). In this aeroelastic analysis, the ability of the PVDF in determining the V-g/V-f diagram was evaluated. A numerical model of composite flat plate was generated considering the piezoelectric instrumentations. The second specimen tested corresponds to composite wing models that are based on laminate composite flat plate. Five models with different fiber orientations were tested in (pure) experimental modal analyses and wind tunnel, hence, the capability of excitation of PZT was verified. Good results were obtained regarding the estimation of natural frequency and damping factor using a single PVDF element. The application of PZT as actuator in the wind tunnel test showed improvement on the data acquisition in terms of noise. However, were observed some characteristics that require careful. As support to experimental tests, several studies were performed. |
publishDate |
2014 |
dc.date.none.fl_str_mv |
2014-04-16 |
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=3038 |
url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3038 |
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 Estruturas de aeronaves Vibração aeroelástica PZT Materiais piezoelétricos Aerodinâmica Engenharia mecânica Engenharia aeronáutica |
_version_ |
1706809294671839232 |