On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom

Detalhes bibliográficos
Autor(a) principal: Vasconcellos, Rui [UNESP]
Data de Publicação: 2014
Outros Autores: Abdelkefi, Abdessattar
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1115/DETC201435144
http://hdl.handle.net/11449/167796
Resumo: A nonlinear characterization based on modern methods of nonlinear dynamics is performed to identify the effects of a multisegmented nonlinearity on the response of an aeroelastic system. This system consists of a plunging and pitching rigid airfoil supported by a linear spring in the plunge degree of freedom and a nonlinear spring in the pitch degree of freedom. The multisegmented nonlinearity is associated with the pitch degree of freedom and contains two different boundaries. The results show that the presence of this multi-segmented nonlinearity results in the presence of a subcritical instability. It is also shown that there are four main transitions or sudden jumps in the system's response when increasing the freestream velocity. It is demonstrated that the first and second sudden jumps are accompanied by the appearance and disappearance of quadratic nonlinearity induced by discontinuity and static positions. The results show that the first transition is due to a near grazing bifurcation that occurs near the first boundary of the multi-segmented nonlinearity. As for the second transition, it is demonstrated that the sudden jump at this transition is associated with a tangential contact between the trajectory and the first boundary of the multisegmented nonlinearity and with a zero-pitch velocity incidence which is a characteristic of a grazing bifurcation. In the third and fourth transitions, it is demonstrated that there are changes in the response of the system from simply periodic to two periods having the main oscillating frequency and its superharmonic of order 3 and from chaotic to two periods having the main oscillating frequency and its superharmonic of order 3. Using modern methods of nonlinear dynamics, it is shown that this transition is due to a grazing bifurcation at the second boundary of the multisegmented nonlinearity.
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spelling On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedomA nonlinear characterization based on modern methods of nonlinear dynamics is performed to identify the effects of a multisegmented nonlinearity on the response of an aeroelastic system. This system consists of a plunging and pitching rigid airfoil supported by a linear spring in the plunge degree of freedom and a nonlinear spring in the pitch degree of freedom. The multisegmented nonlinearity is associated with the pitch degree of freedom and contains two different boundaries. The results show that the presence of this multi-segmented nonlinearity results in the presence of a subcritical instability. It is also shown that there are four main transitions or sudden jumps in the system's response when increasing the freestream velocity. It is demonstrated that the first and second sudden jumps are accompanied by the appearance and disappearance of quadratic nonlinearity induced by discontinuity and static positions. The results show that the first transition is due to a near grazing bifurcation that occurs near the first boundary of the multi-segmented nonlinearity. As for the second transition, it is demonstrated that the sudden jump at this transition is associated with a tangential contact between the trajectory and the first boundary of the multisegmented nonlinearity and with a zero-pitch velocity incidence which is a characteristic of a grazing bifurcation. In the third and fourth transitions, it is demonstrated that there are changes in the response of the system from simply periodic to two periods having the main oscillating frequency and its superharmonic of order 3 and from chaotic to two periods having the main oscillating frequency and its superharmonic of order 3. Using modern methods of nonlinear dynamics, it is shown that this transition is due to a grazing bifurcation at the second boundary of the multisegmented nonlinearity.São Paulo State University (UNESP), Câmpus de São João da Boa VistaDepartment of Engineering Science and Mechanics, MC 0219, Virginia TechSão Paulo State University (UNESP), Câmpus de São João da Boa VistaUniversidade Estadual Paulista (Unesp)Vasconcellos, Rui [UNESP]Abdelkefi, Abdessattar2018-12-11T16:38:21Z2018-12-11T16:38:21Z2014-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObjecthttp://dx.doi.org/10.1115/DETC201435144Proceedings of the ASME Design Engineering Technical Conference, v. 6.http://hdl.handle.net/11449/16779610.1115/DETC2014351442-s2.0-84926058261Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengProceedings of the ASME Design Engineering Technical Conferenceinfo:eu-repo/semantics/openAccess2021-10-23T21:44:37Zoai:repositorio.unesp.br:11449/167796Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462021-10-23T21:44:37Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
title On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
spellingShingle On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
Vasconcellos, Rui [UNESP]
title_short On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
title_full On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
title_fullStr On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
title_full_unstemmed On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
title_sort On grazing bifurcations in an aeroelastic system with multi-segmented nonlinearity in the pitch degree of freedom
author Vasconcellos, Rui [UNESP]
author_facet Vasconcellos, Rui [UNESP]
Abdelkefi, Abdessattar
author_role author
author2 Abdelkefi, Abdessattar
author2_role author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Vasconcellos, Rui [UNESP]
Abdelkefi, Abdessattar
description A nonlinear characterization based on modern methods of nonlinear dynamics is performed to identify the effects of a multisegmented nonlinearity on the response of an aeroelastic system. This system consists of a plunging and pitching rigid airfoil supported by a linear spring in the plunge degree of freedom and a nonlinear spring in the pitch degree of freedom. The multisegmented nonlinearity is associated with the pitch degree of freedom and contains two different boundaries. The results show that the presence of this multi-segmented nonlinearity results in the presence of a subcritical instability. It is also shown that there are four main transitions or sudden jumps in the system's response when increasing the freestream velocity. It is demonstrated that the first and second sudden jumps are accompanied by the appearance and disappearance of quadratic nonlinearity induced by discontinuity and static positions. The results show that the first transition is due to a near grazing bifurcation that occurs near the first boundary of the multi-segmented nonlinearity. As for the second transition, it is demonstrated that the sudden jump at this transition is associated with a tangential contact between the trajectory and the first boundary of the multisegmented nonlinearity and with a zero-pitch velocity incidence which is a characteristic of a grazing bifurcation. In the third and fourth transitions, it is demonstrated that there are changes in the response of the system from simply periodic to two periods having the main oscillating frequency and its superharmonic of order 3 and from chaotic to two periods having the main oscillating frequency and its superharmonic of order 3. Using modern methods of nonlinear dynamics, it is shown that this transition is due to a grazing bifurcation at the second boundary of the multisegmented nonlinearity.
publishDate 2014
dc.date.none.fl_str_mv 2014-01-01
2018-12-11T16:38:21Z
2018-12-11T16:38:21Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/conferenceObject
format conferenceObject
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.1115/DETC201435144
Proceedings of the ASME Design Engineering Technical Conference, v. 6.
http://hdl.handle.net/11449/167796
10.1115/DETC201435144
2-s2.0-84926058261
url http://dx.doi.org/10.1115/DETC201435144
http://hdl.handle.net/11449/167796
identifier_str_mv Proceedings of the ASME Design Engineering Technical Conference, v. 6.
10.1115/DETC201435144
2-s2.0-84926058261
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Proceedings of the ASME Design Engineering Technical Conference
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
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reponame:Repositório Institucional da UNESP
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instname_str Universidade Estadual Paulista (UNESP)
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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)
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