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Numerical Investigation on the Effect of Active Injection Location on the Frequency Response of a Batchelor Vortex.

dc.contributor.authorGarrido-Martín, Manuel
dc.contributor.authorBlanco-Rodríguez, Francisco José
dc.contributor.authorGutiérrez-Castillo, Paloma 
dc.contributor.authorDel-Pino-Peñas, Carlos Manuel 
dc.date.accessioned2023-07-03T09:19:25Z
dc.date.available2023-07-03T09:19:25Z
dc.date.issued2023
dc.identifier.urihttps://hdl.handle.net/10630/27144
dc.description.abstractThis study investigates the effect of the variation of the active control application distance on the frequency response of a Batchelor vortex. The theoretical base flow pertains to the experimental configuration of a wing model with a NACA0012 airfoil at an angle of attack of α=9◦ and a chordbased Reynolds number of Rec=40000. The injection was implemented using punctual and annular jet configurations. The findings of this research will serve as a basis for the optimization of the experimental parameters that characterize potential candidates for active control.es_ES
dc.description.sponsorshipUniversidad de Málaga. Campus de Excelencia Internacional Andalucía Tech.es_ES
dc.language.isoenges_ES
dc.rightsinfo:eu-repo/semantics/openAccesses_ES
dc.subjectMecánica de fluidoses_ES
dc.subjectMovimiento de vórticeses_ES
dc.subject.otherBatchelor vortexes_ES
dc.titleNumerical Investigation on the Effect of Active Injection Location on the Frequency Response of a Batchelor Vortex.es_ES
dc.typeinfo:eu-repo/semantics/conferenceObjectes_ES
dc.centroEscuela de Ingenierías Industrialeses_ES
dc.relation.eventtitle2nd Spanish Fluid Mechanics Conferencees_ES
dc.relation.eventplaceBarcelona, Españaes_ES
dc.relation.eventdate3 de julio de 2023es_ES


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