Determination of the instantaneous forces on flapping wings from a localized fluid velocity field
- Autores
- Minotti, Fernando Oscar
- Año de publicación
- 2011
- Idioma
- inglés
- Tipo de recurso
- artículo
- Estado
- versión publicada
- Descripción
- Expressions are derived to relate the instantaneous pressure force on a flapping wing to the velocity field on a plane at the trailing edge and on a highly localized region around and near the wing, valid when the vortex sheet is thin. In its more practical version, the formalism is applicable to wings with close to two-dimensional geometry and has the advantage of not using spatial derivatives, but only a time derivative of a surface integral of the velocity. In the purely two-dimensional case, the expression obtained is used to justify a much simpler one that only requires the evaluation of the time derivative of the wing circulation. A comparison with a numerical simulation in a two-dimensional case shows a good representation of the forces, even with the most simplified expression, when the condition of a thin wake is met. Other examples are shown in which the wake is not thin in order to explore the limitations of the formalism. It is found in these cases that the thrust is sometimes not so well reproduced, with a tendency to be overestimated, while the lift is generally better reproduced. Remarkably, the simpler expression reproduces rather acceptably the phase and amplitude of both thrust and lift in all cases. © 2011 American Institute of Physics.
Fil: Minotti, Fernando Oscar. Consejo Nacional de Investigaciones Científicas y Técnicas. Oficina de Coordinación Administrativa Ciudad Universitaria. Instituto de Física del Plasma. Universidad de Buenos Aires. Facultad de Ciencias Exactas y Naturales. Instituto de Física del Plasma; Argentina - Materia
-
FLUID FORCES
FLAPPING WINGS - Nivel de accesibilidad
- acceso abierto
- Condiciones de uso
- https://creativecommons.org/licenses/by-nc-sa/2.5/ar/
- Repositorio
- Institución
- Consejo Nacional de Investigaciones Científicas y Técnicas
- OAI Identificador
- oai:ri.conicet.gov.ar:11336/61490
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Determination of the instantaneous forces on flapping wings from a localized fluid velocity fieldMinotti, Fernando OscarFLUID FORCESFLAPPING WINGShttps://purl.org/becyt/ford/1.3https://purl.org/becyt/ford/1Expressions are derived to relate the instantaneous pressure force on a flapping wing to the velocity field on a plane at the trailing edge and on a highly localized region around and near the wing, valid when the vortex sheet is thin. In its more practical version, the formalism is applicable to wings with close to two-dimensional geometry and has the advantage of not using spatial derivatives, but only a time derivative of a surface integral of the velocity. In the purely two-dimensional case, the expression obtained is used to justify a much simpler one that only requires the evaluation of the time derivative of the wing circulation. A comparison with a numerical simulation in a two-dimensional case shows a good representation of the forces, even with the most simplified expression, when the condition of a thin wake is met. Other examples are shown in which the wake is not thin in order to explore the limitations of the formalism. It is found in these cases that the thrust is sometimes not so well reproduced, with a tendency to be overestimated, while the lift is generally better reproduced. Remarkably, the simpler expression reproduces rather acceptably the phase and amplitude of both thrust and lift in all cases. © 2011 American Institute of Physics.Fil: Minotti, Fernando Oscar. Consejo Nacional de Investigaciones Científicas y Técnicas. Oficina de Coordinación Administrativa Ciudad Universitaria. Instituto de Física del Plasma. Universidad de Buenos Aires. Facultad de Ciencias Exactas y Naturales. Instituto de Física del Plasma; ArgentinaAmerican Institute of Physics2011-11info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/61490Minotti, Fernando Oscar; Determination of the instantaneous forces on flapping wings from a localized fluid velocity field; American Institute of Physics; Physics of Fluids; 23; 11; 11-2011; 111902-1119121070-6631CONICET DigitalCONICETenginfo:eu-repo/semantics/altIdentifier/doi/10.1063/1.3659496info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by-nc-sa/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-09-29T10:26:06Zoai:ri.conicet.gov.ar:11336/61490instacron:CONICETInstitucionalhttp://ri.conicet.gov.ar/Organismo científico-tecnológicoNo correspondehttp://ri.conicet.gov.ar/oai/requestdasensio@conicet.gov.ar; lcarlino@conicet.gov.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:34982025-09-29 10:26:06.415CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse |
dc.title.none.fl_str_mv |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field |
title |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field |
spellingShingle |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field Minotti, Fernando Oscar FLUID FORCES FLAPPING WINGS |
title_short |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field |
title_full |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field |
title_fullStr |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field |
title_full_unstemmed |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field |
title_sort |
Determination of the instantaneous forces on flapping wings from a localized fluid velocity field |
dc.creator.none.fl_str_mv |
Minotti, Fernando Oscar |
author |
Minotti, Fernando Oscar |
author_facet |
Minotti, Fernando Oscar |
author_role |
author |
dc.subject.none.fl_str_mv |
FLUID FORCES FLAPPING WINGS |
topic |
FLUID FORCES FLAPPING WINGS |
purl_subject.fl_str_mv |
https://purl.org/becyt/ford/1.3 https://purl.org/becyt/ford/1 |
dc.description.none.fl_txt_mv |
Expressions are derived to relate the instantaneous pressure force on a flapping wing to the velocity field on a plane at the trailing edge and on a highly localized region around and near the wing, valid when the vortex sheet is thin. In its more practical version, the formalism is applicable to wings with close to two-dimensional geometry and has the advantage of not using spatial derivatives, but only a time derivative of a surface integral of the velocity. In the purely two-dimensional case, the expression obtained is used to justify a much simpler one that only requires the evaluation of the time derivative of the wing circulation. A comparison with a numerical simulation in a two-dimensional case shows a good representation of the forces, even with the most simplified expression, when the condition of a thin wake is met. Other examples are shown in which the wake is not thin in order to explore the limitations of the formalism. It is found in these cases that the thrust is sometimes not so well reproduced, with a tendency to be overestimated, while the lift is generally better reproduced. Remarkably, the simpler expression reproduces rather acceptably the phase and amplitude of both thrust and lift in all cases. © 2011 American Institute of Physics. Fil: Minotti, Fernando Oscar. Consejo Nacional de Investigaciones Científicas y Técnicas. Oficina de Coordinación Administrativa Ciudad Universitaria. Instituto de Física del Plasma. Universidad de Buenos Aires. Facultad de Ciencias Exactas y Naturales. Instituto de Física del Plasma; Argentina |
description |
Expressions are derived to relate the instantaneous pressure force on a flapping wing to the velocity field on a plane at the trailing edge and on a highly localized region around and near the wing, valid when the vortex sheet is thin. In its more practical version, the formalism is applicable to wings with close to two-dimensional geometry and has the advantage of not using spatial derivatives, but only a time derivative of a surface integral of the velocity. In the purely two-dimensional case, the expression obtained is used to justify a much simpler one that only requires the evaluation of the time derivative of the wing circulation. A comparison with a numerical simulation in a two-dimensional case shows a good representation of the forces, even with the most simplified expression, when the condition of a thin wake is met. Other examples are shown in which the wake is not thin in order to explore the limitations of the formalism. It is found in these cases that the thrust is sometimes not so well reproduced, with a tendency to be overestimated, while the lift is generally better reproduced. Remarkably, the simpler expression reproduces rather acceptably the phase and amplitude of both thrust and lift in all cases. © 2011 American Institute of Physics. |
publishDate |
2011 |
dc.date.none.fl_str_mv |
2011-11 |
dc.type.none.fl_str_mv |
info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion http://purl.org/coar/resource_type/c_6501 info:ar-repo/semantics/articulo |
format |
article |
status_str |
publishedVersion |
dc.identifier.none.fl_str_mv |
http://hdl.handle.net/11336/61490 Minotti, Fernando Oscar; Determination of the instantaneous forces on flapping wings from a localized fluid velocity field; American Institute of Physics; Physics of Fluids; 23; 11; 11-2011; 111902-111912 1070-6631 CONICET Digital CONICET |
url |
http://hdl.handle.net/11336/61490 |
identifier_str_mv |
Minotti, Fernando Oscar; Determination of the instantaneous forces on flapping wings from a localized fluid velocity field; American Institute of Physics; Physics of Fluids; 23; 11; 11-2011; 111902-111912 1070-6631 CONICET Digital CONICET |
dc.language.none.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
info:eu-repo/semantics/altIdentifier/doi/10.1063/1.3659496 |
dc.rights.none.fl_str_mv |
info:eu-repo/semantics/openAccess https://creativecommons.org/licenses/by-nc-sa/2.5/ar/ |
eu_rights_str_mv |
openAccess |
rights_invalid_str_mv |
https://creativecommons.org/licenses/by-nc-sa/2.5/ar/ |
dc.format.none.fl_str_mv |
application/pdf application/pdf |
dc.publisher.none.fl_str_mv |
American Institute of Physics |
publisher.none.fl_str_mv |
American Institute of Physics |
dc.source.none.fl_str_mv |
reponame:CONICET Digital (CONICET) instname:Consejo Nacional de Investigaciones Científicas y Técnicas |
reponame_str |
CONICET Digital (CONICET) |
collection |
CONICET Digital (CONICET) |
instname_str |
Consejo Nacional de Investigaciones Científicas y Técnicas |
repository.name.fl_str_mv |
CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicas |
repository.mail.fl_str_mv |
dasensio@conicet.gov.ar; lcarlino@conicet.gov.ar |
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13.070432 |