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Structural analyses of orthogrid fuselage panel for integrated Ku-band SatCom antenna
dc.contributor.author | Turon Pujol, Francesc |
dc.contributor.author | Otero Gruer, Fermín Enrique |
dc.contributor.author | Martínez García, Javier |
dc.contributor.other | Universitat Politècnica de Catalunya. Doctorat en Anàlisi Estructural |
dc.contributor.other | Universitat Politècnica de Catalunya. Departament de Ciència i Enginyeria Nàutiques |
dc.date.accessioned | 2020-10-20T13:43:18Z |
dc.date.available | 2020-10-20T13:43:18Z |
dc.date.issued | 2019 |
dc.identifier.citation | Turon, F.; Otero, F.; Martinez, X. Structural analyses of orthogrid fuselage panel for integrated Ku-band SatCom antenna. A: European Conference on Multifuncional Structures. "EMuS 2019: European Conference on Multifunctional Structures". Barcelona: International Centre for Numerical Methods in Engineering (CIMNE), 2019, p. 62-67. ISBN 978-84-949194-4-2. |
dc.identifier.isbn | 978-84-949194-4-2 |
dc.identifier.uri | http://hdl.handle.net/2117/330503 |
dc.description.abstract | The aim of this work is to describe the structural analysis of a multifunctional aircraft fuselage panel. The structure of the panel has an embedded antenna tiles. The panel consists of UniDirectional (UD) carbon fibre reinforced composite skin stiffened with ortho-grid ribs, and a transparent skin window made using UD glass fibre reinforced composite. The orthogrid structure is a structural reinforcement but also the antenna tiles support. The presented work proposes a numerical multiscale strategy. The laminate is simulated with solid elements, in order to capture the real kinematics of the material, but several laminas are condensed in a single finite element. The performance of each lamina is obtained using the Serial-Parallel (SP) mixing theory. The specific formulations developed have been very useful to identify and study the mechanical performance of these new structures and the localization of unknown and un-predicted hot-spots in the structure. |
dc.format.extent | 6 p. |
dc.language.iso | eng |
dc.publisher | International Centre for Numerical Methods in Engineering (CIMNE) |
dc.subject | Àrees temàtiques de la UPC::Enginyeria civil::Materials i estructures |
dc.subject | Àrees temàtiques de la UPC::Matemàtiques i estadística::Anàlisi numèrica::Mètodes numèrics |
dc.subject.lcsh | Airplanes--Design and construction--Mathematical models |
dc.subject.other | Composites |
dc.subject.other | Numerical Methods |
dc.subject.other | Antenna |
dc.subject.other | Panel |
dc.subject.other | Multifunctional |
dc.subject.other | Serial-Parallel Mixing Theory |
dc.title | Structural analyses of orthogrid fuselage panel for integrated Ku-band SatCom antenna |
dc.type | Conference lecture |
dc.subject.lemac | Avions -- Disseny i construcció -- Models matemàtics |
dc.contributor.group | Universitat Politècnica de Catalunya. RMEE - Grup de Resistència de Materials i Estructures en l'Enginyeria |
dc.relation.publisherversion | http://congress.cimne.com/emus2019/admin/files/fileabstract/a18.pdf |
dc.rights.access | Open Access |
local.identifier.drac | 29434903 |
dc.description.version | Postprint (published version) |
local.citation.author | Turon, F.; Otero, F.; Martinez, X. |
local.citation.contributor | European Conference on Multifuncional Structures |
local.citation.pubplace | Barcelona |
local.citation.publicationName | EMuS 2019: European Conference on Multifunctional Structures |
local.citation.startingPage | 62 |
local.citation.endingPage | 67 |