Numerical Investigation of Boundary-Layer Height and Actuation-Parameter Effects of a Circular Synthetic Jet Actuator in Crossflow
Howard Ho, Ebenezer Essel, Pierre Sullivan

TL;DR
This study uses numerical simulations to analyze how various actuation parameters of a circular synthetic jet in crossflow influence boundary-layer behavior and vortex structures, providing insights for flow control applications.
Contribution
It systematically investigates the effects of blowing ratio, stroke ratio, and boundary-layer height ratio on synthetic jet performance in crossflow, which was not comprehensively explored before.
Findings
Low to moderate boundary-layer height ratios enhance separation control.
Higher actuation frequencies produce closely packed vortical structures.
Boundary-layer profiles show increased near-wall momentum with optimal parameters.
Abstract
Three-dimensional unsteady numerical simulations are performed to investigate the effects of blowing ratio (), stroke ratio (), and boundary-layer height ratio () on circular synthetic jet actuator (SJA) performance in crossflow. Nine cases are examined at constant free-stream velocity , with systematic independent variation of averaged jet velocity , actuation frequency (-), and boundary-layer momentum thickness Reynolds number () to isolate the individual effects of these parameters on a circular-nozzle SJA with fixed nozzle diameter in crossflow. Instantaneous vortical structures exhibited tilted vortex rings with a trailing vortex pair at low actuation frequency; closely packed expelled vortical…
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Taxonomy
TopicsPlasma and Flow Control in Aerodynamics · Fluid Dynamics and Turbulent Flows · Aerodynamics and Acoustics in Jet Flows
