2026-05-31T08:22:58Zhttps://riuma.uma.es/rest/oai/request

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

Garrido-Martín, Manuel Blanco-Rodríguez, Francisco José Gutiérrez-Castillo, Paloma Del-Pino-Peñas, Carlos Manuel 2023-07-03T09:19:25Z 2023-07-03T09:19:25Z 2023 https://hdl.handle.net/10630/27144 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. eng open access Mecánica de fluidos Movimiento de vórtices Numerical Investigation on the Effect of Active Injection Location on the Frequency Response of a Batchelor Vortex. conference output