FLUIDIC OSCILLATOR AS A DYNAMIC CALIBRATION TOOL

A fluidic oscillator is proposed as an improved dynamic calibration device for pressure instrumentation such as pressure-sensitive paint (PSP). The fluidic oscillator is a device that generates an oscillating jet when supplied with a pressurized fluid. The jet oscillation frequency ranges up to 6.5 kHz, depending on supply pressure. The flowfield of the oscillating jet has higher-order frequency content of at least 40 kHz, making it ideal for high-frequency calibrations. The fluidic oscillator demonstrated in these experiments is small, simple to use, portable, and inexpensive. The fluidic oscillator calibration tool may be used to calibrate the frequency response of hot-film or hot-wire probes, as well as pressure instrumentation such as pressure transducers or pressure-sensitive paint (PSP). In this work, the fluidic oscillator is used to calibrate the response time of several PSP formulations. Pressure-sensitive paints with anodized aluminum, polymer/ceramic, and thin-layer chromatography binders are calibrated and compared to previous calibration results. Full-field measurements and pointmeasurements with PSP are presented. Typical response times of porous PSPs are on the order of 40 kHz.

[1]  C. Klein,et al.  Pressure sensitive paint for oscillating pressure fields measurements , 1999, ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025).

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

[3]  Hirotaka Sakaue,et al.  Anodized Aluminum Pressure Sensitive Paint in a Cryogenic Wind Tunnel , 1999 .

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

[5]  Hiroshi Kanda,et al.  Surface pressure measurement in a cryogenic wind tunnel by using luminescent coating , 1997, ICIASF'97 Record. International Congress on Instrumentation in Aerospace Simulation Facilities.

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

[7]  Ganesh Raman,et al.  Axisymmetric jet forced by fundamental and subharmonic tones , 1991 .

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

[9]  John P. Sullivan,et al.  Time Response of Anodized Aluminum Pressure-Sensitive Paint , 2001 .

[10]  Bryan Campbell,et al.  Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics , 1997 .

[11]  J. Sullivan,et al.  Porous Polymer/Ceramic Composites for Luminescence-Based Temperature and Pressure Measurement , 1999 .

[12]  James W. Gregory,et al.  Porous Pressure-Sensitive Paint for Characterizing Unsteady Flowfields , 2002 .

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

[14]  H. L. Boerrigter,et al.  Design and calibration of an unsteady pressure measurement system , 1997, ICIASF'97 Record. International Congress on Instrumentation in Aerospace Simulation Facilities.

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

[16]  Tianshu Liu,et al.  A scanning laser system for temperature and pressure sensitive paint , 1994 .

[17]  Y. Ikeda,et al.  Optical measurements of high-frequency pressure fluctuations using PSP and Cassegrain optics , 2002 .

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

[19]  Martin Morris,et al.  Step response of pressure-sensitive paints , 1996 .

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

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

[22]  Othon K. Rediniotis,et al.  Development of unsteady calibration facilities and techniques for fast-response pressure probes , 2002 .

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

[24]  K. Schanze,et al.  Pressure sensitive paint: application to a sinusoidal pressure fluctuation , 1995, ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities.

[25]  J. Callis,et al.  Submillisecond response times of oxygen‐quenched luminescent coatings , 1993 .

[26]  Marvine Hamner Demystifying luminescent paint technology - A guide for non-developers , 2001 .

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

[28]  P. Davis,et al.  High frequency dynamic pressure calibration technique , 1985 .