Mostrar el registro sencillo del ítem

dc.contributor.authorDel-Pino-Peñas, Carlos Manuel 
dc.contributor.authorBlanco-Rodríguez, Francisco José
dc.contributor.authorGarrido-Martín, Manuel
dc.contributor.authorParras-Anguita, Luis 
dc.date.accessioned2023-06-26T09:38:24Z
dc.date.available2023-06-26T09:38:24Z
dc.date.created2023-06-26
dc.date.issued2023
dc.identifier.urihttps://hdl.handle.net/10630/27065
dc.description.abstractWe carried out a frequency response analysis of Batchelor vortex model in two different spatial configurations: punctual and annular jet. The theoretical base flow corresponds to the experimental setting of a wing model with airfoil NACA0012 for a chord-based Reynolds number Rec=40000 and angle of attack of α=9◦. We found that Batchelor model presents a gain in the annular jet configuration higher than the punctual jet for a pair of parameters k and ωf . The results of this research work will be used to propose future candidates of active control.es_ES
dc.description.sponsorshipUniversidad de Málaga. Campus de Excelencia Internacional Andalucía Tech. Ministerio de Ciencia e Innvocación, Proyecto Nacional PID2021-124692OA-I00es_ES
dc.language.isoenges_ES
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacional*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectMecánica de fluidoses_ES
dc.subjectMovimiento de vórticeses_ES
dc.subject.otherTrailing vorticeses_ES
dc.subject.otherBatchelor modeles_ES
dc.subject.otherActive controles_ES
dc.subject.otherFrequency responsees_ES
dc.titleFrequency response of Batchelor vortex.es_ES
dc.typeconference outputes_ES
dc.centroEscuela de Ingenierías Industrialeses_ES
dc.relation.eventtitleSpanish Fluid Mechanics Conferencees_ES
dc.relation.eventplaceBarcelonaes_ES
dc.relation.eventdate02/07/2023es_ES
dc.departamentoIngeniería Mecánica, Térmica y de Fluidos
dc.rights.accessRightsopen accesses_ES


Ficheros en el ítem

Este ítem aparece en la(s) siguiente(s) colección(ones)

Mostrar el registro sencillo del ítem