Fluid Dynamics of a Bistable Diverter Under Ultrasonic Excitation-Part II: Flow Visualization and Fundamental Mechanisms

The switching mechanism and underlying flow physics of an actively controlled fluidic device are investigated using both large eddy simulation (LES) and particle imaging velocimetry (PIV). The fluidic device considered herein uses acoustic excitation of inherent flow instabilities to control the movement of the jet. Acoustic excitation at the preferred frequency is shown to yield high saturation amplitudes resulting in the formation of large vortical structures that do not undergo pairing. Basic flow features including the shear layer instabilities are further examined to explain why the excitation mode that triggers the switching process changes from a shear layer-based mode (St(theta) = 0.012) to a jet orifice mode (St(h) = 0.25) as the Reynolds number increases.

Automated summary

The switching mechanism and flow physics of an actively controlled fluidic device using acoustic excitation to control jet movement are investigated. Acoustic excitation at the preferred frequency results in high saturation amplitudes and the formation of large vortical structures. The change in excitation mode triggering the switching process from a shear layer-based mode to a jet orifice mode with increasing Reynolds number is explained by examining basic flow features, including shear layer instabilities.