Affiliations: Department of Aerospace Engineering, Pennsylvania
State University, University Park, PA 16802, USA.
Note: [] Currently at Department of Mechanical Engineering, Johns Hopkins
University, Baltimore MD 21218, USA.
Abstract: PIV measurements and computational simulations (2D, unsteady
Navier-Stokes) are performed to visualize the inherently unsteady jet
oscillation inside a fluidic oscillator. Both the measurements and computations
are obtained for a jet exit Reynolds number of 321, based on the maximum
velocity and the nozzle width at the jet exit plane. The computed jet
oscillation frequency is in close agreement with the measured PIV frequency.
Formation of a pressure gradient across the jet is observed from the
computations. The variation of the jet oscillation frequency with jet exit
Reynolds number is also determined by single sensor hot-wire measurements
inside the oscillation chamber.