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Journal ArticleDOI

Spatially Distributed Forcing and Jet Vectoring with a Plasma Actuator

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TLDR
In this article, the authors used particle image velocimetry data to show that spatially varying, steady jets could be created with the use of only one actuator by varying the width of the buried electrode in a quiescent flow.
Abstract
volume momentum balance was used. By shaping the buried electrode along the span of the actuator, the local volume of plasma generated can be controlled, which is related to the local body force. Pressure measurements were takenintheboundarylayerbehindtheactuatortocalculatethemomentumimpartedtothe flowatvariousspanwise locations corresponding to different electrode widths. Particle image velocimetry data were then used to show that spatially varying, steady jets could be created with the use of only one actuator by varying the width of the buried electrode in a quiescent flow. The angle of the jet created, relative to the dielectric, by a plasma synthetic jet is also investigated. By pointing two plasma actuators at each other, an inverted impinging jet can be created as a result of the two independent jets colliding. By altering the strength of one of the jets relative to the other, the angle of separation can be changed. Particle image velocimetry data were taken to show the effects of altering the voltage (strength)appliedtooneoftheactuatorsrelativetotheother.Itwasfoundthat,withthismethod,jetvectoringcould beachieved.Theangleofthejetcouldbecontrolledafull180degthroughsmallchangesinthevoltageappliedtothe electrodes, also in a quiescent flow. Nomenclature D = diameter FB = body force FS = shear force P = power qd;off = dynamic pressure downstream of the actuator (0.035 m) with the plasma off qd;on = dynamic pressure downstream of the actuator (0.035 m) with the plasma on Re = Reynolds number St = Strouhal number U = freestream velocity ud;off = velocity downstream of the actuator (0.035 m) with the plasma off ud;on = velocity downstream of the actuator (0.035 m) with the plasma on W = waviness amplitude � = angle of jet measured counterclockwise � V = voltage differential between exposed electrodes relative to ground � = wavelength

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Citations
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Journal ArticleDOI

Recent developments in DBD plasma flow control

TL;DR: A review of the recent trend of plasma actuator design and to summarise aerodynamic control techniques can be found in this article, where the starting vortex that leads to formation of a plasma wall jet is discussed.
Journal ArticleDOI

High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator

TL;DR: In this paper, a single dielectric barrier discharge (DBD) actuator near the flap shoulder is used to increase or reduce the size of the time-averaged separated region over the flap depending on the frequency of actuation.
Journal ArticleDOI

Power consumption, discharge capacitance and light emission as measures for thrust production of dielectric barrier discharge plasma actuators

TL;DR: In this article, the capacitance of a plasma actuator is measured using a simple diagnostic tool that provides insight into the phenomenological behavior of plasma actuators. But, the authors do not consider the effect of the presence of the plasma in the actuator.
Journal ArticleDOI

Diagnostics for characterisation of plasma actuators

TL;DR: In this paper, the authors present an overview of experimental investigations employing diagnostic techniques specifically aimed at AC dielectric barrier discharge, DC corona and nanosecond pulse plasma actuators.
References
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Book

Flow Control: Passive, Active, and Reactive Flow Management

TL;DR: The present work focuses on the development of coherent structures for flow control in microelectromechanical systems, which combine Reynolds number effects with self-consistency to form coherent structures.
Journal ArticleDOI

Passive and Active Flow Control by Swimming Fishes and Mammals

TL;DR: The vortex wake shed by the tail differs between eel-like fishes and fishes with a discrete narrowing of the body in front of the tail, and three-dimensional effects may play a major role in determining wake structure in most fishes.
Journal ArticleDOI

Mechanisms and Responses of a Dielectric Barrier Plasma Actuator: Geometric Effects

TL;DR: The single dielectric barrier discharge plasma, a plasma sustainable at atmospheric pressure, has shown considerable promise as a flow control device operating at modest (tens of watts) power levels as mentioned in this paper.
Journal ArticleDOI

Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control

TL;DR: In this paper, a parametric study has been performed in order to increase the velocity of the ionic wind induced by surface dielectric barrier discharge (DBD) actuators.
Journal ArticleDOI

Plasma Actuators for Separation Control of Low-Pressure Turbine Blades

TL;DR: In this paper, a linear cascade was used to study the flow field over a generic LPT cascade consisting of Pratt and Whitney Pak B shaped blades, and the center blade in the cascade was instrumented to measure the surface-pressure coefficient distribution.
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