A reduced order state space model for aeroelastic analysis in time domain

Detalhes bibliográficos
Autor(a) principal: Marqui, Clayton R.
Data de Publicação: 2017
Outros Autores: Bueno, Douglas D. [UNESP], Goes, Luiz C.S., Gonçalves, Paulo J.P. [UNESP]
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1016/j.jfluidstructs.2017.01.010
http://hdl.handle.net/11449/178600
Resumo: The objective of this paper is to describe a new method for modeling aeroelastic system in time domain based on a modification of the Laguerre Polynomials to represent complex quantities. These polynomials are used to approximate the unsteady aerodynamics forces which are defined in the frequency domain using the Doublet Lattice Method (DLM). In this approach, the size of the matrices representing the aeroelastic system remains the same as the matrices representing the structural dynamics behavior. It is an important point since classical state space aeroelastic models include lag states increasing the size of the matrices used to represent the system. The applicability of the method is demonstrated by numerical simulation performed on the benchmark wing structure. The approach offers promise mainly for complex systems such as real aircraft.
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spelling A reduced order state space model for aeroelastic analysis in time domainAeroelasticityLaguerre polynomialsReduced state space modelTime-domain representationThe objective of this paper is to describe a new method for modeling aeroelastic system in time domain based on a modification of the Laguerre Polynomials to represent complex quantities. These polynomials are used to approximate the unsteady aerodynamics forces which are defined in the frequency domain using the Doublet Lattice Method (DLM). In this approach, the size of the matrices representing the aeroelastic system remains the same as the matrices representing the structural dynamics behavior. It is an important point since classical state space aeroelastic models include lag states increasing the size of the matrices used to represent the system. The applicability of the method is demonstrated by numerical simulation performed on the benchmark wing structure. The approach offers promise mainly for complex systems such as real aircraft.ITA Aeronautical Institute of TechnologyUNESP - State University of São Paulo Fac. Eng. Ilha SolteiraUNESP - State University of São Paulo Fac. Eng. BauruUNESP - State University of São Paulo Fac. Eng. Ilha SolteiraUNESP - State University of São Paulo Fac. Eng. BauruITA Aeronautical Institute of TechnologyUniversidade Estadual Paulista (Unesp)Marqui, Clayton R.Bueno, Douglas D. [UNESP]Goes, Luiz C.S.Gonçalves, Paulo J.P. [UNESP]2018-12-11T17:31:15Z2018-12-11T17:31:15Z2017-02-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article428-440application/pdfhttp://dx.doi.org/10.1016/j.jfluidstructs.2017.01.010Journal of Fluids and Structures, v. 69, p. 428-440.1095-86220889-9746http://hdl.handle.net/11449/17860010.1016/j.jfluidstructs.2017.01.0102-s2.0-850103046532-s2.0-85010304653.pdfScopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengJournal of Fluids and Structures1,4811,481info:eu-repo/semantics/openAccess2024-06-13T19:29:09Zoai:repositorio.unesp.br:11449/178600Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T18:15:10.538481Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv A reduced order state space model for aeroelastic analysis in time domain
title A reduced order state space model for aeroelastic analysis in time domain
spellingShingle A reduced order state space model for aeroelastic analysis in time domain
Marqui, Clayton R.
Aeroelasticity
Laguerre polynomials
Reduced state space model
Time-domain representation
title_short A reduced order state space model for aeroelastic analysis in time domain
title_full A reduced order state space model for aeroelastic analysis in time domain
title_fullStr A reduced order state space model for aeroelastic analysis in time domain
title_full_unstemmed A reduced order state space model for aeroelastic analysis in time domain
title_sort A reduced order state space model for aeroelastic analysis in time domain
author Marqui, Clayton R.
author_facet Marqui, Clayton R.
Bueno, Douglas D. [UNESP]
Goes, Luiz C.S.
Gonçalves, Paulo J.P. [UNESP]
author_role author
author2 Bueno, Douglas D. [UNESP]
Goes, Luiz C.S.
Gonçalves, Paulo J.P. [UNESP]
author2_role author
author
author
dc.contributor.none.fl_str_mv ITA Aeronautical Institute of Technology
Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Marqui, Clayton R.
Bueno, Douglas D. [UNESP]
Goes, Luiz C.S.
Gonçalves, Paulo J.P. [UNESP]
dc.subject.por.fl_str_mv Aeroelasticity
Laguerre polynomials
Reduced state space model
Time-domain representation
topic Aeroelasticity
Laguerre polynomials
Reduced state space model
Time-domain representation
description The objective of this paper is to describe a new method for modeling aeroelastic system in time domain based on a modification of the Laguerre Polynomials to represent complex quantities. These polynomials are used to approximate the unsteady aerodynamics forces which are defined in the frequency domain using the Doublet Lattice Method (DLM). In this approach, the size of the matrices representing the aeroelastic system remains the same as the matrices representing the structural dynamics behavior. It is an important point since classical state space aeroelastic models include lag states increasing the size of the matrices used to represent the system. The applicability of the method is demonstrated by numerical simulation performed on the benchmark wing structure. The approach offers promise mainly for complex systems such as real aircraft.
publishDate 2017
dc.date.none.fl_str_mv 2017-02-01
2018-12-11T17:31:15Z
2018-12-11T17:31:15Z
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/10.1016/j.jfluidstructs.2017.01.010
Journal of Fluids and Structures, v. 69, p. 428-440.
1095-8622
0889-9746
http://hdl.handle.net/11449/178600
10.1016/j.jfluidstructs.2017.01.010
2-s2.0-85010304653
2-s2.0-85010304653.pdf
url http://dx.doi.org/10.1016/j.jfluidstructs.2017.01.010
http://hdl.handle.net/11449/178600
identifier_str_mv Journal of Fluids and Structures, v. 69, p. 428-440.
1095-8622
0889-9746
10.1016/j.jfluidstructs.2017.01.010
2-s2.0-85010304653
2-s2.0-85010304653.pdf
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Journal of Fluids and Structures
1,481
1,481
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 428-440
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
_version_ 1808128910940962816

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