A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.

The design of structures submitted to aerodynamic loads usually requires the development of specific computational models considering fluid-structure interactions. Models using structural frame elements are developed in several relevant applications such as, the design of advanced aircraft wings, wi...

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Main Author: Vanzulli, Mauricio C. (author)
Other Authors: Pérez Zerpa, Jorge M. (author)
Format: article
Language:English
Published: 2023
Subjects:
Online Access:https://hdl.handle.net/20.500.12008/41731
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author Vanzulli, Mauricio C.
author2 Pérez Zerpa, Jorge M.
author2_role author
author_browse Pérez Zerpa, Jorge M.
Vanzulli, Mauricio C.
author_facet Vanzulli, Mauricio C.
Pérez Zerpa, Jorge M.
author_role author
collection COLIBRI
dc.contributor.none.fl_str_mv Vanzulli Mauricio C., Universidad de la República (Uruguay). Facultad de Ingeniería.
Pérez Zerpa Jorge M., Universidad de la República (Uruguay). Facultad de Ingeniería.
dc.creator.none.fl_str_mv Vanzulli, Mauricio C.
Pérez Zerpa, Jorge M.
dc.date.none.fl_str_mv 2023-12-08T16:19:35Z
2023-12-08T16:19:35Z
2023
dc.format.none.fl_str_mv 18 p.
application/pdf
dc.identifier.none.fl_str_mv Vanzulli, M. y Pérez Zerpa, J. "A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures" Heliyon, vol.9, no.9 (2023) e19990. [en línea] 18 p.
https://hdl.handle.net/20.500.12008/41731
10.1016/j.heliyon.2023.e19990
dc.language.none.fl_str_mv en
eng
dc.publisher.none.fl_str_mv Cell Press
dc.relation.none.fl_str_mv Heliyon, vol.9, no.9 (2023) e19990.
dc.rights.none.fl_str_mv info:eu-repo/semantics/openAccess
Licencia Creative Commons Atribución (CC - By 4.0)
dc.source.none.fl_str_mv reponame:COLIBRI
instname:Universidad de la República
instacron:Universidad de la República
dc.subject.none.fl_str_mv Co-rotational formulation
Nonlinear dynamics
Quasi-steady theory
Finite element method
dc.title.none.fl_str_mv A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
dc.type.none.fl_str_mv Artículo
info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
description The design of structures submitted to aerodynamic loads usually requires the development of specific computational models considering fluid-structure interactions. Models using structural frame elements are developed in several relevant applications such as, the design of advanced aircraft wings, wind turbine blades or power transmission lines. In the case of flexible frame structures submitted to fluid flows, the computation of inertial and aerodynamic forces for large displacements and rotations is a challenging task. In this article, we present a novel formulation for the efficient computation of aerodynamic forces in frame structures, coupling the co-rotational framework with the quasi-steady theory. A numerical procedure is provided considering a tangent matrix for the aerodynamic forces. This formulation is implemented in the open-source library ONSAS, allowing users to reproduce the results or solve other frame nonlinear dynamic problems. The proposed formulation and its implementation are validated through the resolution of four numerical examples. The formulation and the numerical procedure proposed efficiently provide accurate solutions for these challenging problems with large displacements and rotations.
eu_rights_str_mv openAccess
format article
id anni_7699574ada4278cd13eb3db65cef6bf0
identifier_str_mv Vanzulli, M. y Pérez Zerpa, J. "A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures" Heliyon, vol.9, no.9 (2023) e19990. [en línea] 18 p.
10.1016/j.heliyon.2023.e19990
instacron_str Universidad de la República
institution Universidad de la República
instname_str Universidad de la República
language eng
language_invalid_str_mv en
network_acronym_str anni
network_name_str oai-lr-anni
oai_identifier_str oai:colibri.udelar.edu.uy:20.500.12008/41731
publishDate 2023
publishDateSort 2023
publisher.none.fl_str_mv Cell Press
reponame_str COLIBRI
repository.mail.fl_str_mv
repository.name.fl_str_mv
repository_id_str
rights_invalid_str_mv Licencia Creative Commons Atribución (CC - By 4.0)
spelling A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.Vanzulli, Mauricio C.Pérez Zerpa, Jorge M.Co-rotational formulationNonlinear dynamicsQuasi-steady theoryFinite element methodThe design of structures submitted to aerodynamic loads usually requires the development of specific computational models considering fluid-structure interactions. Models using structural frame elements are developed in several relevant applications such as, the design of advanced aircraft wings, wind turbine blades or power transmission lines. In the case of flexible frame structures submitted to fluid flows, the computation of inertial and aerodynamic forces for large displacements and rotations is a challenging task. In this article, we present a novel formulation for the efficient computation of aerodynamic forces in frame structures, coupling the co-rotational framework with the quasi-steady theory. A numerical procedure is provided considering a tangent matrix for the aerodynamic forces. This formulation is implemented in the open-source library ONSAS, allowing users to reproduce the results or solve other frame nonlinear dynamic problems. The proposed formulation and its implementation are validated through the resolution of four numerical examples. The formulation and the numerical procedure proposed efficiently provide accurate solutions for these challenging problems with large displacements and rotations.Los autores desean agradecer a la Comisión Sectorial de Investigación Científica de la Universidad de la República y a la Comisión Académica de Posgrado por su apoyo financiero y a la Agencia Nacional de Investigación e Innovación por el apoyo financiero a través del proyecto FSE_1_2016_1_131837.Cell PressVanzulli Mauricio C., Universidad de la República (Uruguay). Facultad de Ingeniería.Pérez Zerpa Jorge M., Universidad de la República (Uruguay). Facultad de Ingeniería.2023-12-08T16:19:35Z2023-12-08T16:19:35Z2023Artículoinfo:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersion18 p.application/pdfVanzulli, M. y Pérez Zerpa, J. "A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures" Heliyon, vol.9, no.9 (2023) e19990. [en línea] 18 p.https://hdl.handle.net/20.500.12008/4173110.1016/j.heliyon.2023.e19990reponame:COLIBRIinstname:Universidad de la Repúblicainstacron:Universidad de la RepúblicaenengHeliyon, vol.9, no.9 (2023) e19990.Las obras depositadas en el Repositorio se rigen por la Ordenanza de los Derechos de la Propiedad Intelectual de la Universidad de la República.(Res. Nº 91 de C.D.C. de 8/III/1994 – D.O. 7/IV/1994) y por la Ordenanza del Repositorio Abierto de la Universidad de la República (Res. Nº 16 de C.D.C. de 07/10/2014)info:eu-repo/semantics/openAccessLicencia Creative Commons Atribución (CC - By 4.0)oai:colibri.udelar.edu.uy:20.500.12008/417312026-04-14T10:41:06Z
spellingShingle A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
Vanzulli, Mauricio C.
Co-rotational formulation
Nonlinear dynamics
Quasi-steady theory
Finite element method
status_str publishedVersion
title A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
title_full A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
title_fullStr A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
title_full_unstemmed A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
title_short A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
title_sort A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
topic Co-rotational formulation
Nonlinear dynamics
Quasi-steady theory
Finite element method
url https://hdl.handle.net/20.500.12008/41731