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Journal ArticleDOI

Lumped Element Modeling of Piezoelectric-Driven Synthetic Jet Actuators

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TLDR
In this paper, a lumped element model of a piezoelectric-driven synthetic jet actuator is presented, where the individual components of a synthetic jet are modeled as elements of an equivalent electrical circuit using conjugate power variables.
Abstract
: This paper presents a lumped element model of a piezoelectric-driven synthetic jet actuator. A synthetic jet, also known as a zero net mass-flux device, uses a vibrating diaphragm to generate an oscillatory flow through a small orifice or slot. In lumped element modeling (LEM), the individual components of a synthetic jet are modeled as elements of an equivalent electrical circuit using conjugate power variables. The frequency response function of the circuit is derived to obtain an expression for Q(sub out)/V(sub AC), the volume flow rate per applied voltage. The circuit is analyzed to provide physical insight into the dependence of the device behavior on geometry and material properties. Methods to estimate the model parameters are discussed, and experimental verification is presented. In addition, the model is used to estimate the performance of two prototypical synthetic jets, and the results are compared with experiment.

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Citations
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Journal ArticleDOI

Actuators for Active Flow Control

TL;DR: This review provides a framework for the discussion of actuator specifications, characteristics, selection, design, and classification for aeronautical applications and attempts to highlight the strengths and inevitable drawbacks of each and highlight potential future research directions.
Journal ArticleDOI

Formation Criterion for Synthetic Jets

TL;DR: In this article, the Strouhal number is defined as the appearance of a time-averaged outward velocity along the jet axis and corresponds to the generation and subsequent convection or escape of a vortex ring.
Journal ArticleDOI

Active control of flow-induced cavity oscillations

TL;DR: A review of active control of flow-induced cavity oscillations is presented in this paper, with emphasis on experimental implementation of open-and closed-loop control approaches, as well as the characteristics of various actuators, flow sensing and measurement, and control methodologies employed to date.

Review of Active Control of Flow-Induced Cavity Resonance

TL;DR: A review of active control of flow-induced cavity oscillations is presented in this article, with emphasis on experimental implementation of open-and closed-loop control approaches, and the characteristics of various actuators, flow sensing and measurement, and control methodologies employed to date.
References
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Journal ArticleDOI

The formation and evolution of synthetic jets

TL;DR: In this article, a nominally plane turbulent jet is synthesized by the interactions of a train of counter-rotating vortex pairs that are formed at the edge of an orifice by the time-periodic motion of a flexible diaphragm in a sealed cavity.
Book

Fundamentals of Physical Acoustics

TL;DR: In this paper, the authors present a detailed development of the acoustical wave equation, including propagation in Stratified media and propagation in Dissipative Fluids: Absorption and Dispersion.
Journal ArticleDOI

Acoustic Nonlinearity of an Orifice

TL;DR: In this article, the phase relationship between the fundamental harmonic components of pressure and velocity has been investigated by measuring simultaneously the oscillatory flow velocity in the orifice and the acoustic pressure fluctuations producing the flow.
Journal ArticleDOI

Numerical investigation of synthetic-jet flowfields

TL;DR: In this article, the flowflelds surrounding a synthetic-jet actuating device are investigated numerically by direct simulation, and solutions are obtained to the unsteady compressible Navier-Stokes equations for both the interior of the actuator cavity and for the external jet flowfield.
Proceedings ArticleDOI

Aerodynamic Flow Control Using Synthetic Jet Technology

TL;DR: In this article, the manipulation of global aerodynamic forces on bluff bodies using surface fluidic actuators based on synthetic jets technology is demonstrated in wind tunnel experiments using a 2-D cylinder model.
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