Active control of a high reynolds number Mach 0.9 axisymmetric Jet

AIAA Journal

Volumn 47, Issue 1, 2009, Pages 116-128

  Kim, J H ^a,b   Kastner, J ^a,c   Samimy, M ^a,d  

^a OHIO STATE UNIVERSITY   (United States)

^b Gas Dynamics and Turbulence Laboratory

^c UNIVERSITY OF CINCINNATI   (United States)

^d NONE

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE CONTROLS; ARC FILAMENT PLASMA ACTUATORS; AXISYMMETRIC; AZIMUTHAL MODES; CIRCULAR JETS; CONVECTION VELOCITIES; HIGH REYNOLDS NUMBERS; INDUCED VELOCITIES; LARGE SCALE STRUCTURES; NOZZLE EXITS; PARTICLE IMAGE VELOCIMETRY MEASUREMENTS; REYNOLDS; SCALE STRUCTURES; SPATIAL CORRELATIONS; SPEED FLOWS; VELOCITY CONTOURS; VELOCITY FIELDS;

ACTUATORS; CONTROL SYSTEM ANALYSIS; CONTROL THEORY; FLOW VISUALIZATION; REYNOLDS NUMBER; STROUHAL NUMBER; VELOCITY;

JETS;

EID: 58149382197     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.36801     Document Type: Article

References (23)

1. Zaman, K. B. M. Q., and Hussain, A. K. M. F., "Turbulence Suppression in Free Shear Flows by Controlled Excitation," Journal of Fluid Mechanics, Vol. 103, 1981, pp. 133-159. doi:10.1017/S0022112081001274
2. Freymuth, P., "On Transition in a Separated Laminar Boundary Layer," Journal of Fluid Mechanics, Vol. 25, 1966, pp. 683-704. doi:10.1017/S002211206600034X
3. Michalke, A., "On Spatially Growing Disturbances in an Inviscid Shear Layer," Journal of Fluid Mechanics, Vol. 23, 1965, pp. 521-544. doi:10.1017/S0022112065001520
4. Cho, S. K., Yoo, J. Y., and Choi, H., "Vortex Pairing in an Axisymmetric Jet Using Two-Frequency Acoustic Forcing at Low to Moderate Strouhal Numbers," Experiments in Fluids, Vol. 25, No. 4, 1998, pp. 305-315. doi:10.1007/s003480050234
5. Crow, S. C., and Champagne, F. H., "Orderly Structure in Jet Turbulences," Journal of Fluid Mechanics, Vol. 48, 1971, pp. 547-591. doi:10.1017/S0022112071001745
6. Gutmark, E., and Ho, C. M., "Preferred Modes and the Spreading Rated of Jets," Physics of Fluids, Vol. 26, No. 10, 1983, pp. 2932-2938. doi:10.1063/1.864058
7. Ho, C.-M., and Huerre, P., "Perturbed Free Shear Layers," Annual Review of Fluid Mechanics, Vol. 16, Jan. 1984, pp. 365-424. doi:10.1146/annurev.fl.16.010184.002053
8. Samimy, M., Adamovich, I., Webb, B., Kastner, J., Hileman, J., Keshav, S., and Palm, P., "Development and Characterization of Plasma Actuators for High Speed and Reynolds Number Jet Control," Experiments in Fluids. Vol. 37. No. 4, 2004. pp. 577-588. doi:10.1007/s00348-004-0854-7
9. Samimy, M. J., Kim. J.-H., Kastner, J., Adamovich, I., and Ulkin, Y., "Active Control of a Mach 0.9 Jet for Noise Mitigation Using Plasma Actuators," AIAA Journal. Vol. 45. No. 4, 2007. pp. 890-901. doi:10.2514/1.27499
10. Samimy, M., Kim. J.-H., Kastner, J. Adamovich, I., and Utkin. Y., "Active Control of High Speed and High Reynolds Number Jets Using Plasma Actuators," Journal of Fluid Mechanics, Vol. 578. May 2007. pp. 305-330. doi:10.1017/S0022112007004867
11. Utkin, Y., Keshav, S. Kim. J.-H., Kastner, J., Adamovich, I. and Samimy, M., "Use of Localized Arc Filament Plasma Actuators for High Speed Jet Control," Journal of Physics D: Applied Physics. Vol. 40. Feb. 2007. pp. 685-694. doi:10.1088/0022-3727/40/3/S06
12. Samimy, M., Kastner, J., Kim.J.-H., Utkin. Y.,Adamovich, I., Bridges, J., and Brown. C., "Flow and Noise Control in High Speed and High Reynolds Number Jets Using Plasma Actuators," AIAA Paper 2006-2846, 2006.
13. Kastner. J. Hileman. J., and Samimy. M., "Exploring High-Speed Axisymmetric Jet Noise Control Using Hartmann Tube Fluidic Actuators." AIAA Paper 2004-0186, 2004.
14. Melling, A. "Tracer Particles and Seeding or Particle Image Vclocimetry." Measurement Science and Technology. Vol. 8. No. 12, 1997, pp. 1406-1416. doi:10.1088/0957-0233/8/12/005
15. Bridges. J., and Wernet, M. P., "Turbulence Measurements of Separated Flow Nozzles with Mixing Enhancement Features." AIAA Paper 2002-2484, 2002.
16. Adrian, R., Christensen, K. and Liu, Z., "Analysis and Interpretation of Instantaneous Turbulent Velocity Fields," Experiments in Fluids, Vol. 29, No. 3, 2000, pp. 275-290. doi:10.1007/s003489900087
17. Kline, S. J., and Robinson, S. K., "Quasi-Coherent Structures in the Turbulent Boundary Layer. I: Status Report on a Community-Wide Summary of the Data," Near-Wall Turbulence: 1988 Zoran Zaric Memorial Conference, edited by S. J. Kline, and N. H. Afgan, Hemisphere, New York. 1990, pp. 200-217.
18. Robinson, S. K., Kline, S. J., and Spalart. P. R., "A Review of Quasi-Coherent Structures in a Numerically Simulated Turbulent Boundary Layer," NASA TM 102191, 1989.
19. Konstantinidis, E. Balabani, S., and Yianneskis, M., "Conditional Averaging of PIV Plane Wake Data Using a Cross-Correlation Approach." Experiments in Fluids. Vol. 39, No. 1, 2005, pp. 38-47. doi:10.1007/s00348-005-0963-y
20. Kästner, J., Kim. J.-H., and Samimy, M., "Toward Better Understanding of Far-Field Radiated Noise Mechanisms in a High Reynolds Number Mach 0.9 Axisymmetric Jet." AIAA Paper 2008-0007, Jan. 2008.
21. Troutt, T. R., and McLaughlin. D. K., "Experiments on the Flow and Acoustic Properties of a Moderate-Reynolds Number Supersonic Jet," Journal of Fluid Mechanics, Vol. 116, 1982, pp. 123-156. doi:10.1017/S0022112082000408
22. Petitjean. B. P. McLaughlin. D. K. and Morris. P. J., "An Experimental Investigation of Density Gradient Fluctuations in High-Speed Jets Using Optical Deflectometry," AIAA Paper 2006-2533, 2006.
23. Bridges, J., "Effect of Heat on Space-Time Correlations in Jets," AIAA Paper 2006-2534, 2006.