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dc.contributor.authorFlores Le Roux, Roberto Maurice
dc.contributor.authorOrtega, Enrique
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Física
dc.date.accessioned2019-11-13T13:08:39Z
dc.date.issued2019
dc.identifier.citationFlores, R.; Ortega, E. Efficient aeroelastic analysis of wind loads on inflatable hangars. A: International Conference Form and Force / Symposium of the International Association for Shell and Spatial structures / International Conference on Textile Composites and Inflatable Structures. "IASS Symposium 2019, 60th Anniversary Symposium of the International Association for Shell and Spatial Structures Structural Membranes 2019, 9th International Conference on Textile Composites and Inflatable Structures FORM and FORCE: Barcelona, Spain, October 7-10, 2019". Barcelona: International Centre for Numerical Methods in Engineering (CIMNE), 2019, p. 1164-1171.
dc.identifier.isbn978-84-121101-0-4
dc.identifier.urihttp://hdl.handle.net/2117/172315
dc.description.abstractWind loads play a crucial role in inflatable structures. Unfortunately, design loads from safety regulations grossly overestimate the real aerodynamic forces. Thus, a more accurate estimation of wind loads is desirable. Conventional CFD approaches (e.g. LES) struggle with the complexities of the flow field (intricate geometry and massive flow separation) and require a very high computational effort. We present a cost-efficient tool for the aeroelastic analysis of inflatable hangars. It uses a staggered solution scheme with an explicit finite-element structural solver and potential flow aerodynamics. To account for large areas of separated flow typical of blunt shapes, a semi-empirical correction is applied to the inviscid solution. The streamlines of the potential solution are computed and, for each one, the separation point is predicted with Stratford’s criterion. Finally, an empirical correction is applied to the inviscid pressure field. We present validation benchmarks as well as a real life application example. Over the majority of the flow field, the pressure field agrees well with high-fidelity computations, yielding similar global loads for structural sizing. This is achieved with a small fraction of the computational effort required by conventional CFD approaches.
dc.format.extent8 p.
dc.language.isoeng
dc.publisherInternational Centre for Numerical Methods in Engineering (CIMNE)
dc.subjectÀrees temàtiques de la UPC::Enginyeria mecànica
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica
dc.subject.lcshAeroelasticity
dc.subject.lcshWind-pressure
dc.subject.lcshAir-supported structures
dc.subject.otherInflatable structures
dc.subject.otherAeroelasticity
dc.subject.otherWind loads
dc.subject.otherLow-fidelity methods
dc.titleEfficient aeroelastic analysis of wind loads on inflatable hangars
dc.typeConference report
dc.subject.lemacAeroelasticitat
dc.subject.lemacPressió del vent
dc.subject.lemacEstructures pneumàtiques
dc.contributor.groupUniversitat Politècnica de Catalunya. GMNE - Grup de Mètodes Numèrics en Enginyeria
dc.contributor.groupUniversitat Politècnica de Catalunya. L'AIRE - Laboratori Aeronàutic i Industrial de Recerca i Estudis
dc.rights.accessOpen Access
local.identifier.drac25884290
dc.description.versionPostprint (published version)
dc.date.lift10000-01-01
local.citation.authorFlores, R.; Ortega, E.
local.citation.contributorInternational Conference Form and Force / Symposium of the International Association for Shell and Spatial structures / International Conference on Textile Composites and Inflatable Structures
local.citation.pubplaceBarcelona
local.citation.publicationNameIASS Symposium 2019, 60th Anniversary Symposium of the International Association for Shell and Spatial Structures Structural Membranes 2019, 9th International Conference on Textile Composites and Inflatable Structures FORM and FORCE: Barcelona, Spain, October 7-10, 2019
local.citation.startingPage1164
local.citation.endingPage1171


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