VORTEX FLOWS
   THERMAL FLOWS
   NUMERICAL METHODS
   ACOUSTICS
   AERODYNAMICS
    ACOUSTICS
Scattering by Vorticity

O
ur goal is to use high frequency sound waves to characterize vortex structures in motion. Sound scattering occurs when an incoming plane sound wave hits a vortex distribution as shown in the figure at right. The scattered wave pressure in the far field region is proportional to the Fourier transform of the vorticity target (in the first Born approximation). We can measure some properties of the vortex distribution like its characteristic size l and the average flow velocity by virtue of a Doppler effect.

 


A target vortex distribution can be a Karman vortex street behind a bluff body, a fluctuating wake/jet, or a more compact structure like a vortex pair. A Sell type flat sound emitter creates a plane sound wave of high frequency which interacts with the vortex field and then scatters sound in all directions. We look at a given direction by installing a Sell type flat receiver at a known scattering angle. A heterodyne detection give us the amplitude and phase of scattered pressure signals.

 

  Universidad de Chile, Facultad de Ciencas Físicas y Matemáticas