A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications
- Autores
- Cliff, E.M.; Liu, Z.; Spies, Ruben Daniel
- Año de publicación
- 2008
- Idioma
- inglés
- Tipo de recurso
- artículo
- Estado
- versión publicada
- Descripción
- Rigidizable-Inflatable (RI) materials offer the possibility of deployable large space structures (C.H.M. Jenkins (ed.), Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications, Progress in Aeronautics and Astronautics, 191, AIAA Pubs., 2001) and so are of interest in applications where large optical or RF apertures are needed. In particular, in recent years there has been renewed interest in inflatablerigidizable truss-structures because of the efficiency they offer in packaging during boost-to-orbit. However, much research is still needed to better understand dynamic response characteristics, including inherent damping, of truss structures fabricated with these advanced material systems. One of the most important characteristics of such space systems is their response to changing thermal loads, as they move in and out of the Earth?s shadow. We study a model for the thermoelastic behavior of a basic truss componentconsisting of two RI beams connected through a joint subject to solar heating. Axial and transverse motions as well as thermal response of the beams with thermoelastic damping are taking into account. The model results in a couple PDE-ODE system. Well-posedness and stability results are shown and analyzed.
Fil: Cliff, E.M.. Virginia Polytechnic Institute and State University; Estados Unidos
Fil: Liu, Z.. University of Minnesota Duluth; Estados Unidos
Fil: Spies, Ruben Daniel. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - Santa Fe. Instituto de Matemática Aplicada del Litoral. Universidad Nacional del Litoral. Instituto de Matemática Aplicada del Litoral; Argentina - Materia
-
Thermoelasticity
Beams
Inflatable-Rigidizable Structures - 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:11336/84093
Ver los metadatos del registro completo
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A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space ApplicationsCliff, E.M.Liu, Z.Spies, Ruben DanielThermoelasticityBeamsInflatable-Rigidizable Structureshttps://purl.org/becyt/ford/1.1https://purl.org/becyt/ford/1Rigidizable-Inflatable (RI) materials offer the possibility of deployable large space structures (C.H.M. Jenkins (ed.), Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications, Progress in Aeronautics and Astronautics, 191, AIAA Pubs., 2001) and so are of interest in applications where large optical or RF apertures are needed. In particular, in recent years there has been renewed interest in inflatablerigidizable truss-structures because of the efficiency they offer in packaging during boost-to-orbit. However, much research is still needed to better understand dynamic response characteristics, including inherent damping, of truss structures fabricated with these advanced material systems. One of the most important characteristics of such space systems is their response to changing thermal loads, as they move in and out of the Earth?s shadow. We study a model for the thermoelastic behavior of a basic truss componentconsisting of two RI beams connected through a joint subject to solar heating. Axial and transverse motions as well as thermal response of the beams with thermoelastic damping are taking into account. The model results in a couple PDE-ODE system. Well-posedness and stability results are shown and analyzed.Fil: Cliff, E.M.. Virginia Polytechnic Institute and State University; Estados UnidosFil: Liu, Z.. University of Minnesota Duluth; Estados UnidosFil: Spies, Ruben Daniel. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - Santa Fe. Instituto de Matemática Aplicada del Litoral. Universidad Nacional del Litoral. Instituto de Matemática Aplicada del Litoral; ArgentinaUnión Matemática Argentina2008-02info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/84093Cliff, E.M.; Liu, Z.; Spies, Ruben Daniel; A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications; Unión Matemática Argentina; Revista de la Unión Matemática Argentina; 49; 2; 2-2008; 55-660041-69321669-9637CONICET DigitalCONICETenginfo:eu-repo/semantics/altIdentifier/url/http://inmabb.criba.edu.ar/revuma/pdf/v49n2/v49n2a07.pdfinfo:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by-nc-sa/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-09-29T09:50:09Zoai:ri.conicet.gov.ar:11336/84093instacron: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 09:50:09.355CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse |
dc.title.none.fl_str_mv |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications |
title |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications |
spellingShingle |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications Cliff, E.M. Thermoelasticity Beams Inflatable-Rigidizable Structures |
title_short |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications |
title_full |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications |
title_fullStr |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications |
title_full_unstemmed |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications |
title_sort |
A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications |
dc.creator.none.fl_str_mv |
Cliff, E.M. Liu, Z. Spies, Ruben Daniel |
author |
Cliff, E.M. |
author_facet |
Cliff, E.M. Liu, Z. Spies, Ruben Daniel |
author_role |
author |
author2 |
Liu, Z. Spies, Ruben Daniel |
author2_role |
author author |
dc.subject.none.fl_str_mv |
Thermoelasticity Beams Inflatable-Rigidizable Structures |
topic |
Thermoelasticity Beams Inflatable-Rigidizable Structures |
purl_subject.fl_str_mv |
https://purl.org/becyt/ford/1.1 https://purl.org/becyt/ford/1 |
dc.description.none.fl_txt_mv |
Rigidizable-Inflatable (RI) materials offer the possibility of deployable large space structures (C.H.M. Jenkins (ed.), Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications, Progress in Aeronautics and Astronautics, 191, AIAA Pubs., 2001) and so are of interest in applications where large optical or RF apertures are needed. In particular, in recent years there has been renewed interest in inflatablerigidizable truss-structures because of the efficiency they offer in packaging during boost-to-orbit. However, much research is still needed to better understand dynamic response characteristics, including inherent damping, of truss structures fabricated with these advanced material systems. One of the most important characteristics of such space systems is their response to changing thermal loads, as they move in and out of the Earth?s shadow. We study a model for the thermoelastic behavior of a basic truss componentconsisting of two RI beams connected through a joint subject to solar heating. Axial and transverse motions as well as thermal response of the beams with thermoelastic damping are taking into account. The model results in a couple PDE-ODE system. Well-posedness and stability results are shown and analyzed. Fil: Cliff, E.M.. Virginia Polytechnic Institute and State University; Estados Unidos Fil: Liu, Z.. University of Minnesota Duluth; Estados Unidos Fil: Spies, Ruben Daniel. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - Santa Fe. Instituto de Matemática Aplicada del Litoral. Universidad Nacional del Litoral. Instituto de Matemática Aplicada del Litoral; Argentina |
description |
Rigidizable-Inflatable (RI) materials offer the possibility of deployable large space structures (C.H.M. Jenkins (ed.), Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications, Progress in Aeronautics and Astronautics, 191, AIAA Pubs., 2001) and so are of interest in applications where large optical or RF apertures are needed. In particular, in recent years there has been renewed interest in inflatablerigidizable truss-structures because of the efficiency they offer in packaging during boost-to-orbit. However, much research is still needed to better understand dynamic response characteristics, including inherent damping, of truss structures fabricated with these advanced material systems. One of the most important characteristics of such space systems is their response to changing thermal loads, as they move in and out of the Earth?s shadow. We study a model for the thermoelastic behavior of a basic truss componentconsisting of two RI beams connected through a joint subject to solar heating. Axial and transverse motions as well as thermal response of the beams with thermoelastic damping are taking into account. The model results in a couple PDE-ODE system. Well-posedness and stability results are shown and analyzed. |
publishDate |
2008 |
dc.date.none.fl_str_mv |
2008-02 |
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/11336/84093 Cliff, E.M.; Liu, Z.; Spies, Ruben Daniel; A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications; Unión Matemática Argentina; Revista de la Unión Matemática Argentina; 49; 2; 2-2008; 55-66 0041-6932 1669-9637 CONICET Digital CONICET |
url |
http://hdl.handle.net/11336/84093 |
identifier_str_mv |
Cliff, E.M.; Liu, Z.; Spies, Ruben Daniel; A Model for the Thermoelastic Behavior of a Joint-Leg-Beam System for Space Applications; Unión Matemática Argentina; Revista de la Unión Matemática Argentina; 49; 2; 2-2008; 55-66 0041-6932 1669-9637 CONICET Digital CONICET |
dc.language.none.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
info:eu-repo/semantics/altIdentifier/url/http://inmabb.criba.edu.ar/revuma/pdf/v49n2/v49n2a07.pdf |
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 |
Unión Matemática Argentina |
publisher.none.fl_str_mv |
Unión Matemática Argentina |
dc.source.none.fl_str_mv |
reponame:CONICET Digital (CONICET) instname:Consejo Nacional de Investigaciones Científicas y Técnicas |
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CONICET Digital (CONICET) |
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CONICET Digital (CONICET) |
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Consejo Nacional de Investigaciones Científicas y Técnicas |
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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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