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Authordc.contributor.authorGuttag, M. 
Authordc.contributor.authorKarimi, H. H. 
Authordc.contributor.authorFalcón Beas, Claudio 
Authordc.contributor.authorReis, P. M. 
Admission datedc.date.accessioned2018-08-07T20:54:33Z
Available datedc.date.available2018-08-07T20:54:33Z
Publication datedc.date.issued2018
Cita de ítemdc.identifier.citationPhysical Review Fluids Volumen: 3 Número: 1 Número de artículo: 014003es_ES
Identifierdc.identifier.other10.1103/PhysRevFluids.3.014003
Identifierdc.identifier.urihttps://repositorio.uchile.cl/handle/2250/150736
Abstractdc.description.abstractWe perform a combined experimental and numerical investigation into the static deformation of perforated elastic strips under uniform aerodynamic loading at high-Reynoldsnumber conditions. The static shape of the porous strips, clamped either horizontally or vertically, is quantified as they are deformed by wind loading, induced by a horizontal flow. The experimental profiles are compared to numerical simulations using a reduced model that takes into account the normal drag force on the deformed surface. For both configurations (vertical and horizontal clamping), we compute the drag coefficient of the strip, by fitting the experimental data to the model, and find that it decreases as a function of porosity. Surprisingly, we find that, for every value of porosity, the drag coefficients for the horizontal configuration are larger than those of the vertical configuration. For all data in both configurations, with the exception of the continuous strip clamped vertically, a linear relation is found between the porosity and drag. Making use of this linearity, we can rescale the drag coefficient in a way that it becomes constant as a function of the Cauchy number, which relates the force due to fluid loading on the elastic strip to its bending rigidity, independently of the material properties and porosity of the strip and the flow speed. Our findings on flexible strips are contrasted to previous work on rigid perforated plates. These results highlight some open questions regarding the usage of reduced models to describe the deformation of flexible structures subjected to aerodynamic loading.es_ES
Patrocinadordc.description.sponsorshipDepartment of Defense (DoD) through the National Defense Science & Engineering Graduate Fellowship (NDSEG) Program National Science Foundation (CAREER) CMMI-1351449es_ES
Lenguagedc.language.isoenes_ES
Publisherdc.publisherAmer Physical Soces_ES
Type of licensedc.rightsAttribution-NonCommercial-NoDerivs 3.0 Chile*
Link to Licensedc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/cl/*
Sourcedc.sourcePhysical Review Fluidses_ES
Keywordsdc.subjectDrag Reductiones_ES
Keywordsdc.subjectFlexible Plateses_ES
Keywordsdc.subjectFlowes_ES
Keywordsdc.subjectReconfigurationes_ES
Keywordsdc.subjectFutteres_ES
Keywordsdc.subjectScreenses_ES
Keywordsdc.subjectFishes_ES
Títulodc.titleAeroelastic deformation of a perforated stripes_ES
Document typedc.typeArtículo de revista
Catalogueruchile.catalogadorrgfes_ES
Indexationuchile.indexArtículo de publicación ISIes_ES


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Attribution-NonCommercial-NoDerivs 3.0 Chile
Except where otherwise noted, this item's license is described as Attribution-NonCommercial-NoDerivs 3.0 Chile