Variable-Frequency Fluidic Oscillator Driven by a Piezoelectric Bender

§This paper describes a new actuator for flow control applications ‐ the piezo-fluidic oscillator. The actuator is a fluidic device based on wall-attachment of a fluid jet, and modulated by piezoelectric devices. The piezo-fluidic oscillator successfully decouples the operating frequency from the flow characteristics of the device. The frequency is specified by an input electrical signal that is independent of pressure, making this actuator ideal for closed-loop control applications. The oscillator exhibits high bandwidth (up to 1.2 kHz), modulation rates up to 100%, and a velocity range reaching sonic conditions. Furthermore, the bi-stable actuator may be operated in a steady state, with momentum flux in one of two desired directions. The piezo-fluidic oscillator may be used in flow control applications where synthetic jets cannot provide enough momentum for control authority. The actuator can also be used as an alternative to traditional aircraft control surfaces while operating in the steady bi-directional mode. This paper details the design and characterization of the piezo-fluidic oscillator. The dynamic response characteristics are evaluated with flow visualization and hot film probe measurements on the output. **

[1]  Rui Chen,et al.  Piezo-fluidic Gaseous Fuel MPI System for Natural Gas Fuelled IC Engines , 2001 .

[2]  Eric J. Jumper,et al.  Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology , 2004 .

[3]  Ari Glezer,et al.  Characterization of the Internal Flow Dynamics of Combustion Powered Actuators , 2008 .

[4]  Ari Glezer,et al.  Direct excitation of small-scale motions in free shear flows , 1998 .

[5]  Ganesh Raman,et al.  Evaluation of Flip-Flop Jet Nozzles for Use as Practical Excitation Devices , 1994 .

[6]  Václav Tesař,et al.  Experimental investigation of a fluidic actuator generating hybrid-synthetic jets , 2007 .

[7]  Ari Glezer,et al.  Characterization of Combustion Powered Actuators for Flow Control , 2006 .

[8]  Timothy J. Bencic,et al.  Cavity Resonance Suppression Using Miniature Fluidic Oscillators , 1999 .

[9]  E. Jumper,et al.  Mechanisms and Responses of a Dielectric Barrier Plasma Actuator: Geometric Effects , 2004 .

[10]  K. Asai,et al.  A review of pressure-sensitive paint for high-speed and unsteady aerodynamics , 2008 .

[11]  J. Bell,et al.  Surface Pressure Measurements Using Luminescent Coatings , 2003 .

[12]  James W. Gregory,et al.  Switching Behavior of a Plasma-Fluidic Actuator , 2007 .

[13]  James W. Gregory,et al.  CHARACTERIZATION OF HARTMANN TUBE FLOW WITH POROUS PRESSURE-SENSITIVE PAINT , 2003 .

[14]  Ganesh Raman,et al.  Using Controlled Unsteady Fluid Mass Addition to Enhance Jet Mixing , 1997 .

[15]  J. Roth,et al.  Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma , 2000 .

[16]  William S. Saric,et al.  Effect of suction and weak mass injection on boundary-layer transition , 1986 .

[17]  Hermann Viets,et al.  Flip-Flop Jet Nozzle , 1975 .

[18]  Václav Tesař Configurations of fluidic actuators for generating hybrid-synthetic jets , 2007 .

[19]  Joseph Katz,et al.  Experimental Characterization of a Supersonic Flow Control Actuator , 2006 .

[20]  Ganesh Raman,et al.  Cavity Resonance Suppression Using Miniature Fluidic Oscillators , 2004 .

[21]  Emad Gharaibah,et al.  Unsteady Separation Control for Wind Turbine Applications at Full Scale Reynolds Number , 2009 .

[22]  Samer Khanafseh,et al.  Development of high bandwidth powered resonance tube actuators with feedback control , 2004 .

[23]  M. Michard,et al.  Control of a Plane Jet by Fluidic Wall Pulsing , 2003 .

[24]  T. Corke,et al.  SDBD plasma enhanced aerodynamics: concepts, optimization and applications , 2007 .

[25]  Avi Seifert,et al.  Suction and Oscillatory Blowing Actuator Modeling and Validation , 2008 .

[26]  Ganesh Raman,et al.  Using Controlled Unsteady Fluid Mass Addition , 1997 .

[27]  Lutz Taubert,et al.  Discrete Sweeping Jets as Tools for Separation Control , 2008 .

[28]  James W. Gregory,et al.  Variable-Frequency Fluidic Oscillator Driven by a Piezoelectric Bender , 2005 .

[29]  Luca Cortelezzi,et al.  The actively controlled jet in crossflow , 2001, Journal of Fluid Mechanics.

[30]  Guillermo Artana,et al.  Flow Control with Electrohydrodynamic Actuators , 2001 .

[31]  James W. Gregory,et al.  POROUS PRESSURE-SENSITIVE PAINT FOR MEASUREMENT OF UNSTEADY PRESSURES IN TURBOMACHINERY , 2004 .

[32]  Rui Chen,et al.  An Investigation into the Use of Piezo-Fluidic Combined Units as Fuel Injectors for Natural Gas Engines , 1996 .

[33]  Václav Tesař,et al.  No-moving-part hybrid-synthetic jet actuator , 2006 .

[34]  Ari Glezer,et al.  Manipulation of free shear flows using piezoelectric actuators , 1993, Journal of Fluid Mechanics.

[35]  C. K. Taft,et al.  A Proportional Piezoelectric Electro-Fluidic Pneumatic Value Design , 1981 .

[36]  G. Papadopoulos,et al.  Jet thrust vectoring using a miniature fluidic oscillator , 2005, The Aeronautical Journal (1968).

[37]  R. B. Beale,et al.  Development of a wall-attachment fluidic oscillator applied to volume flow metering , 1974 .

[38]  Ganesh Raman,et al.  Flip-Flop Jet Nozzle Extended to Supersonic Flows , 1993 .

[39]  J. Gregory,et al.  Pressure-sensitive paint as a distributed optical microphone array. , 2006, The Journal of the Acoustical Society of America.

[40]  Noel Malcolm Morris,et al.  An introduction to fluid logic , 1973 .

[41]  J. Gregory,et al.  Characterization of the Microfluidic Oscillator , 2007 .

[42]  Robert Bonine Beale The design of a liquid fluidic reaction jet system. , 1969 .

[43]  Emad Gharaibah,et al.  An Experimental and Numerical Investigation on Fluidic Oscillators For Flow Control , 2007 .

[44]  John Magill,et al.  Exploring the Feasibility of Pulsed Jet Separation Control for Aircraft Configurations , 2001 .

[45]  Mo Samimy,et al.  Development and Characterization of Hartmann Tube Fluidic Actuators for High-Speed Flow Control , 2002 .

[46]  Ricardo A. Burdisso,et al.  Experimental Demonstration of Active Flow Control to Reduce Unsteady Stator-Rotor Interaction , 2001 .

[47]  Brian R. Smith,et al.  A computational investigation of pulsed injection into a confined, expanding crossflow , 2001 .

[48]  W.V. Miller Experimental Feasibility Study of an Analog Electrical-to-Fluidic Transducer , 1969, IEEE Transactions on Industrial Electronics and Control Instrumentation.

[49]  Joseph M. Kirshner,et al.  Design Theory of Fluidic Components , 1975 .

[50]  Eric Moreau,et al.  Airflow control by non-thermal plasma actuators , 2007 .

[51]  Dennis E. Culley,et al.  Computational Fluid Dynamic Modeling of a Fluidic Actuator for Flow Control , 2008 .

[52]  Joseph M. Kirshner Chapter 5 – JET DYNAMICS , 1975 .

[53]  Calin Tarau,et al.  Sound Attenuation by Glow Discharge Plasma , 2004 .

[54]  James W. Gregory,et al.  Effect of Quenching Kinetics on Unsteady Response of Pressure-Sensitive Paint , 2006 .

[55]  James W. Gregory,et al.  Visualization of jet mixing in a fluidic oscillator , 2005, J. Vis..

[56]  Stephen B. M. Beck,et al.  Fluidic Pressure Pulse Transmitting Flowmeter , 1997 .