2026-06-06T04:01:18Zhttps://riuma.uma.es/rest/oai/request

oai:riuma.uma.es:10630/271442026-02-03T11:48:26Zcom_10630_2254col_10630_37959

00925njm 22002777a 4500 dc Garrido-Martín, Manuel author Blanco-Rodríguez, Francisco José author Gutiérrez-Castillo, Paloma author Del-Pino-Peñas, Carlos Manuel author 2023 This 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. https://hdl.handle.net/10630/27144 Mecánica de fluidos Movimiento de vórtices Numerical Investigation on the Effect of Active Injection Location on the Frequency Response of a Batchelor Vortex.