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Experiments in Fluids
Erschienen in: Experiments in Fluids 4/2004

01.10.2004 | Original Paper

Development and characterization of plasma actuators for high-speed jet control

verfasst von: M. Samimy, I. Adamovich, B. Webb, J. Kastner, J. Hileman, S. Keshav, P. Palm

Erschienen in: Experiments in Fluids | Ausgabe 4/2004

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Abstract

Active control of high Reynolds number and high-speed jets has been hampered due to the lack of suitable actuators. Some of the attributes that would make an actuator suitable for such flows are: high amplitude and bandwidth; small size for distribution around the jet; phase-locking ability for jet azimuthal mode forcing; and sufficient ruggedness for hot jets. We have been developing a class of actuators termed ‘localized arc filament plasma actuators,’ which possess such characteristics. In this paper, we present the development and characterization of these actuators as well as preliminary results on their applications in high Reynolds number Mach 0.9 and ideally expanded Mach 1.3 jets.
Vorheriger Artikel Mixing efficiency measurements using a modified cold chemistry technique
Nächster Artikel Axial development of subcooled boiling flow in an internally heated annulus

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Literatur
Adamovich IV (2001) Control of electron recombination rate and electron density in optically pumped nonequilibrium plasmas. J Phys D Appl Phys 34:319–325CrossRef
Adelgren RG, Elliott GS, Knight D (2001) Energy deposition in supersonic flows. Am Inst Aeronaut Astronaut Paper 2001-0885
Adelgren RG, Elliott GS, Crawford JB (2002) Axisymmetric jet shear layer excitation induced by electric arc discharge and focused laser energy deposition. Am Inst Aeronaut Astronaut Paper 2002-0729
Ahuja KK, Lepicovsky J, Burrin RH (1982) Noise and flow structure of a tone-excited jet. Am Inst Aeronaut Astronaut J 20(12):1700–1706
Ahuja KK, Brown WH (1989) Shear flow control by mechanical tabs. Am Inst Aeronaut Astronaut Paper 1989-0994
Alvi FS, Elavarasan R, Shih C, Garg G, Krothapalli A (2000) Active control of supersonic impinging jets using microjets. Am Inst Aeronaut Astronaut Paper 2000-2236
Arakeri VH, Krothapalli A, Siddavaram V, Alkislar MB, Lourenco LM (2003) On the use of microjets to suppress turbulence in a Mach 0.9 axisymmetric jet. J Fluid Mech 490:75–98CrossRef
Artana G, Adamo J, Léger L, Moreau E, Touchard G (2001) Flow control with electrohydrodynamic actuators. Am Inst Aeronaut Astronaut Paper 2001-0351
Bechert D, Pfizenmaier E (1975) On the amplification of broad band jet noise by a pure tone excitation. J Sound Vib 43(3):581–587CrossRef
Bobashev SV, D’yakonova EA, Erofeev AV, Lapushikina TA, Maslennikov VG, Poniaev SA, Sacharov AA, Vasil’eva RV (2000) Shock-tube facility for MGD supersonic flow control. Am Inst Aeronaut Astronaut Paper 2000-2647
Cohen J, Wygnanski I (1987) The evolution of instabilities in the axisymmetric jet, Part 1: The linear growth of disturbances near the nozzle. J Fluid Mech 176:191–219
Corke TC, Matlis E (2000) Phased plasma arrays for unsteady flow control. Am Inst Aeronaut Astronaut Paper 2000-2323
Crow SC, Champagne FH (1971) Orderly structure in jet turbulence. J Fluid Mech 48:547–591
Gutmark E, Ho C-M (1983) Preferred modes and the spreading rate of jets. Phys Fluids 26(10):2932–2938CrossRef
Hileman J, Samimy M (2003) Effects of vortex generating tabs on noise sources in an ideally expanded Mach 1.3 Jet. Int J Aeroacoustics 2(1):35–63CrossRef
Ho C-M, Huerre P (1984) Perturbed free shear layers. Ann Rev Fluid Mech 16:365–424CrossRef
Kastner J, Hileman J, Samimy S (2004) Exploring high-speed axisymmetric jet noise control using hartmann tube fluidic actuators. Am Inst Aeronaut Astronaut Paper 2004-0186
Kerechanin C, Samimy M, Kim J-H (2001) Effects of nozzle trailing edges on acoustic field of supersonic rectangular jet. Am Inst Aeronaut Astronaut J 39(6):1065
Kibens V (1979) Discrete noise spectrum generated by an acoustically excited jet. Am Inst Aeronaut Astronaut J 18:434–451
Kibens V, Dorris J III, Smith DM (1999) Active flow control technology transition: The Boeing ACE program. Am Inst Aeronaut Astronaut Paper 1999-3507
Kim J-H, Samimy M (1999) Mixing enhancement via nozzle trailing edge modifications in a high-speed rectangular jet. Phys Fluids 11(9):2731CrossRef
Laufer J, Yen T-C (1983) Noise generation by a low-Mach-number jet. J Fluid Mech 134:1–31
Leonov S, Bityurin V, Kolesnichenko Y (2001) Dynamic of a single-electrode HF plasma filament in supersonic airflow. Am Inst Aeronaut Astronaut Paper 2001-0493
Leonov S, Bityurin V, Savelkin K, Yarantsev D (2002) Effect of electrical discharge on separation processes and shocks position in supersonic airflow. Am Inst Aeronaut Astronaut Paper 2002-0355
Lepicovsky J, Brown WH (1987) Effects of nozzle-exit boundary-layer conditions on excitability of heated free jets. Am Inst Aeronaut Astronaut Paper 1987-2723
Long DF, Kim H, Arndt REA (1985) Controlled suppression or amplification of turbulent jet noise. Am Inst Aeronaut Astronaut J 23(6):828–833
Lou H, Alvi FS, Shih C, Choi J, Annaswamy A (2002) Active control of supersonic impinging jets: Flowfield properties and closed-loop strategies. Am Inst Aeronaut Astronaut Paper 2002-2728
Martens S, Kinzie KW, McLaughlin DK (1996) Structure of coherent instabilities in a supersonic shear layer. Am Inst Aeronaut Astronaut J 34(8):1555
Merriman S, Ploenjes E, Palm P, Adamovich IV (2000) Shock wave control by nonequilibrium plasmas in cold supersonic gas flows. Am Inst Aeronaut Astronaut Paper 2000-2327
Merriman S, Christian A, Meyer R, Kowalczyk B, Palm P, Adamovich IV (2001) Studies of conical shock modification by nonequilibrium RF discharge plasma. Am Inst Aeronaut Astronaut Paper 2001-0347
Michalke A (1965) On spatially growing disturbances in an inviscid shear layer. J Fluid Mech 23:521–544
Minucci MAS, Bracken RM, Myrabo LN, Nagamatsu HT, Shanahan KJ (2000) Experimental investigation of an electric arc simulated ‘air spike’ in hypersonic flow. Am Inst Aeronaut Astronaut Paper 2000-0715
Parekh DE, Kibens V, Glezer A, Wiltse JM, Smith DM (1996) Innovative jet flow control: Mixing enhancement experiments. Am Inst Aeronaut Astronaut Paper 1996-0308
Post ML, Corke TC (2003) Separation control on high angle of attack airfoil using plasma actuators. Am Inst Aeronaut Astronaut Paper 2003-1024
Reeder MF, Samimy M (1996) The evolution of a jet with vortex-generating tabs: Real-time visualization and quantitative measurements. J Fluid Mech 311:73
Reynolds WC, Parekh DE, Juvet PJD, Lee MJD (2003) Bifurcating and blooming jets. Annu Rev Fluid Mech 35:295–315CrossRef
Roth JR, Sherman DM, Wilkinson SP (2000) Electrohydrodynamic flow control with a glow-discharge surface plasma. Am Inst Aeronaut Astronaut J 38(7):1166–1172
Samimy M, Zaman KBMQ, Reeder MF (1993) Effect of tabs on the flow and noise field of an axisymmetric jet. Am Inst Aeronaut Astronaut J 31:609
Samimy M, Adamovich I, Kim J-H, Webb B, Keshav S, Utkin Y (2004) Active control of high-speed jets using localized arc filament plasma actuators. Am Inst Aeronaut Astronaut Paper 2004-2130
Saiyed NH, Mikkelsen KL, Bridges JE (2003) Acoustics and thrust of quiet separate-flow high-bypass-ratio nozzles. Am Inst Aeronaut Astronaut J 41(3):372–378
Simonich JC, Narayanan S, Barber TJ, Nishimura, M (2001) Aeroacoustic characterization noise reduction and dimensional scaling effects of high subsonic jets. Am Inst Aeronaut Astronaut J 39(11):2062–2069
Stepaniuk V, Sheverev V, Ötügen MV, Tarau C (2003) Sound attenuation by glow discharge plasma. Am Inst Aeronaut Astronaut Paper 2003-0371
Tret’yakov PK, Garanin AF, Grachev GN, Krainev VL, Ponomarenko AG, Tischenko VN, Yakovlev VI (1996) Control of supersonic flow around bodies by means of high-power recurrent optical breakdown. Phys Doklady 41(11):566
Troutt TR, McLaughlin DK (1982) Experiments on the flow and acoustic properties of a moderate Reynolds number supersonic jet. J Fluid Mech 116:123–156
Yano R, Aithal SM, Subramaniam VV, Contini V, Palm P, Merriman S, Adamovich I, Lempert W, Rich JW (1999) Experimental characterization of shock dispersions in weakly ionized nonequilibrium plasmas. Am Inst Aeronaut Astronaut Paper 1999-3671
Zaman KBMQ, Hussain AKMF (1981) Turbulence suppression in free shear flows by controlled excitation. J Fluid Mech 103:133–159
Zaman KBMQ, Samimy M, Reeder MF (1994) Control of an axisymmetric jet using vortex generators. Phys Fluids 6:778
Metadaten
Titel
Development and characterization of plasma actuators for high-speed jet control
verfasst von
M. Samimy
I. Adamovich
B. Webb
J. Kastner
J. Hileman
S. Keshav
P. Palm
Publikationsdatum
01.10.2004
Verlag
Springer-Verlag
Erschienen in
Experiments in Fluids / Ausgabe 4/2004
Print ISSN: 0723-4864
Elektronische ISSN: 1432-1114
DOI
https://doi.org/10.1007/s00348-004-0854-7

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