Femtosecond Laser Tagging Characterization of a Sweeping Jet Actuator Operating in the Compressible Regime

A sweeping jet (SWJ) actuator operating over a range of nozzle pressure ratios (NPRs) was characterized with femtosecond laser electronic excitation tagging (FLEET), single hot-wire anemometry (HWA) and high-speed/phase-averaged schlieren. FLEET velocimetry was successfully demonstrated in a highly unsteady, oscillatory flow containing subsonic through supersonic velocities. Qualitative comparisons between FLEET and HWA (which measured mass flux since the flow was compressible) showed relatively good agreement in the external flow profiles. The spreading rate was found to vary from 0.5 to 1.2 depending on the pressure ratio. The precision of FLEET velocity measurements in the external flow field was poorer (is approximately equal to 25 m/s) than reported in a previous study due to the use of relatively low laser fluences, impacting the velocity fluctuation measurements. FLEET enabled velocity measurements inside the device and showed that choking likely occurred for NPR 2.0, and no internal shockwaves were present. Qualitative oxygen concentration measurements using FLEET were explored in an effort to gauge the jet's mixing with the ambient. The jet was shown to mix well within roughly four throat diameters and mix fully within roughly eight throat diameters. Schlieren provided visualization of the internal and external flow fields and showed that the qualitative structure of the internal flow does not vary with pressure ratio and the sweeping mechanism observed for incompressible NPRs also probably holds for compressible NPRs.

[1]  Nathan D. Calvert,et al.  FLEET Boundary Layer Velocity Profile Measurements , 2013 .

[2]  P. Danehy,et al.  Femtosecond-Laser-Based Measurements of Velocity and Density in the NASA Langley 0.3-m Transonic Cryogenic Tunnel , 2016 .

[3]  Daniel R. Richardson,et al.  Application of FLEET Velocimetry in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel , 2015 .

[4]  Mixture-fraction measurements with femtosecond-laser electronic-excitation tagging. , 2017, Applied optics.

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

[6]  J. M. Bergadà,et al.  Experimental study of the internal flow structures inside a fluidic oscillator , 2013 .

[7]  Ehab Fares,et al.  Numerical Simulation of Fluidic Actuators for Flow Control Applications , 2012 .

[8]  Richard B Miles,et al.  Femtosecond laser electronic excitation tagging for quantitative velocity imaging in air. , 2011, Applied optics.

[9]  William E. Milholen,et al.  Using Computational Fluid Dynamics and Experiments to Design Sweeping Jets for High Reynolds Number Cruise Configurations , 2016 .

[10]  L. Kovasznay,et al.  The Hot-Wire Anemometer in Supersonic Flow , 1950 .

[11]  Christian Oliver Paschereit,et al.  The Time-Resolved Internal and External Flow Field Properties of a Fluidic Oscillator , 2014 .

[12]  Dennis E. Culley,et al.  Numerical Studies of a Supersonic Fluidic Diverter Actuator for Flow Control , 2010 .

[13]  R. Miles Femtosecond Laser Electronic Excitation Tagging (FLEET) for Imaging Flow Structure in Unseeded Hot or Cold Air or Nitrogen , 2013 .

[14]  S. Raghu Fluidic oscillators for flow control , 2013, Experiments in Fluids.

[15]  Gregory S. Jones,et al.  Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility , 2013 .

[16]  LaTunia G. Pack Melton,et al.  Sweeping Jet Actuator in a Quiescent Environment , 2013 .

[17]  Christian Oliver Paschereit,et al.  Numerical Investigations on Geometric Parameters Affecting the Oscillation Properties of a Fluidic Oscillator , 2013 .

[18]  Julio Soria,et al.  An assessment of high-power light-emitting diodes for high frame rate schlieren imaging , 2012 .

[19]  M. R. Edwards,et al.  Limitations on High-Spatial Resolution Measurements of Turbulence Using Femtosecond Laser Tagging , 2015 .

[20]  Nathan D. Calvert,et al.  Precision of FLEET Velocimetry Using High-Speed CMOS Camera Systems , 2015 .

[21]  I. Wygnanski,et al.  Performance Enhancement of a Vertical Tail Model with Sweeping Jet Actuators , 2013 .

[22]  Yiannis Andreopoulos,et al.  Shock Wave—Turbulence Interactions , 2000 .

[23]  C. O. Paschereit,et al.  Numerical Modeling and Validation of the Flow in a Fluidic Oscillator , 2013 .