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      <dc:title>Numerical Investigation on the Effect of Active Injection Location on the Frequency Response of a Batchelor Vortex.</dc:title>
      <dc:creator>Garrido-Martín, Manuel</dc:creator>
      <dc:creator>Blanco-Rodríguez, Francisco José</dc:creator>
      <dc:creator>Gutiérrez-Castillo, Paloma</dc:creator>
      <dc:creator>Del-Pino-Peñas, Carlos Manuel</dc:creator>
      <dc:subject>Mecánica de fluidos</dc:subject>
      <dc:subject>Movimiento de vórtices</dc:subject>
      <dc:description>This study investigates the effect of the variation of the active control application distance on the&#xd;
frequency response of a Batchelor vortex. The theoretical base flow pertains to the experimental&#xd;
configuration of a wing model with a NACA0012 airfoil at an angle of attack of α=9◦ and a chordbased&#xd;
Reynolds number of Rec=40000. The injection was implemented using punctual and annular&#xd;
jet configurations. The findings of this research will serve as a basis for the optimization of the&#xd;
experimental parameters that characterize potential candidates for active control.</dc:description>
      <dc:date>2023-07-03T09:19:25Z</dc:date>
      <dc:date>2023-07-03T09:19:25Z</dc:date>
      <dc:date>2023</dc:date>
      <dc:type>conference output</dc:type>
      <dc:identifier>https://hdl.handle.net/10630/27144</dc:identifier>
      <dc:language>eng</dc:language>
      <dc:relation>2nd Spanish Fluid Mechanics Conference</dc:relation>
      <dc:relation>Barcelona, España</dc:relation>
      <dc:relation>3 de julio de 2023</dc:relation>
      <dc:rights>open access</dc:rights>
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