Application of piezoelectric materials as sensor and actuator for aeroelastic investigation

Detalhes bibliográficos
Autor(a) principal: Éder Luiz Oliveira
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.
id ITA_b9f3c99785d41663226a1a5aa4ef1e90
oai_identifier_str oai:agregador.ibict.br.BDTD_ITA:oai:ita.br:3038
network_acronym_str ITA
network_name_str Biblioteca Digital de Teses e Dissertações do ITA
spelling 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