Active control of laminar boundary layers with dielectric barrier discharge (DBD) plasma actuators (PAs) has made considerable progress in the last 15 years. First pioneering experiments have motivated numerous researchers to gain a deeper insight into the underlying working principles and corresponding quantification of the actuator performance. These investigations clearly show the strengths but also the weaknesses of the PA as a flow control device. Presently, the boundary-layer control (BLC) with PAs experiences the transition from lab studies to real flight applications. However, the PA community still struggles with the poor fluid mechanic efficiency and the limited momentum flux of the actuator. This review therefore addresses the question how applicable the actuator is as an energy efficient flow control device for future in-flight applications. Since any successful flow control requires detailed knowledge of the actuator’s control authority, this discussion is built upon a careful and comprehensive summary of performance evaluation measures and the interplay with various changes of thermodynamic and kinematic environmental conditions. Consequently, this review for the first time provides a comprehensive discussion of all required steps for successful DBD-based in-flight flow control spanning from the power supply to the achieved flow-control success in one coherent document.
Issue Section:
Review Article
References
1.
Gad-El-Hak
, M.
, 2007
, Flow Control: Passive, Active, and Reactive Flow Management
, Cambridge University Press
, New York
.2.
Schmidt-Nielsen
, K.
, 1972
, “Locomotion: Energy Cost of Swimming, Flying, and Running
,” Science
, 177
(4045
), pp. 222
–228
.3.
Taylor
, G.
, Triantafyllou
, M. S.
, and Tropea
, C.
, 2010
, Animal Locomotion
, Springer
, Heidelberg, Germany
.4.
Valavanis
, K. P.
, 2007
, Advances in Unmanned Aerial Vehicles: State of the Art and the Road to Autonomy
, 1st ed., Springer Publishing Company
, Dordrecht, The Netherlands
.5.
Fish
, F.
, and Lauder
, G.
, 2006
, “Passive and Active Flow Control by Swimming Fishes and Mammals
,” Annu. Rev. Fluid Mech.
, 38
(1
), pp. 193
–224
.6.
Wang
, Z. J.
, 2005
, “Dissecting Insect Flight
,” Annu. Rev. Fluid Mech.
, 37
(1
), pp. 183
–210
.7.
Triantafyllou
, M. S.
, and Hover
, F. S.
, 2002
, Maneuvering and Control of Marine Vehicles
, Massachusetts Institute of Technology
, Cambridge, MA
.8.
Kroo
, I.
, 2001
, “Drag Due to Lift: Concepts for Prediction and Reduction
,” Annu. Rev. Fluid Mech.
, 33
(1
), pp. 587
–617
.9.
Gad-El-Hak
, M.
, 1990
, “Control of Low-Speed Airfoil Aerodynamics
,” AIAA J.
, 28
(9
), pp. 1537
–1552
.10.
Al-Sarkhi
, A.
, 2010
, “Drag Reduction With Polymers in Gas–Liquid/Liquid-Liquid Flows in Pipes: A Literature Review
,” J. Nat. Gas Sci. Eng.
, 2
(1
), pp. 41
–48
.11.
Swamee
, P. K.
, and Sharma
, A. K.
, 2008
, Design of Water Supply Pipe Networks
, Wiley
, Hoboken, NJ
.12.
Tucker
, V. A.
, 1993
, “Gliding Birds: Reduction of Induced Drag by Wing Tip Slots Between the Primary Feathers
,” J. Exp. Biol.
, 180
(1
), pp. 285
–310
.13.
Dean
, B.
, and Bhushan
, B.
, 2010
, “Shark-Skin Surfaces for Fluid-Drag Reduction in Turbulent Flow: A Review
,” Philos. Trans. R. Soc. London A
, 368
(1929
), pp. 4775
–4806
.14.
van Dam
, C. P.
, and Pitts
, B. J. H. C.
, 1981
, “Effect of Winglets on Performance and Handling Qualities of General Aviation Aircraft
,” J. Aircr.
, 18
(7
), pp. 587
–591
.15.
Maughmer
, M. D.
, 2003
, “Design of Winglets for High-Performance Sailplanes
,” J. Aircr.
, 40
(6
), pp. 1099
–1106
.16.
Schlatter
, P.
, and Örlü
, R.
, 2012
, “Turbulent Boundary Layers at Moderate Reynolds Numbers: Inflow Length and Tripping Effects
,” J. Fluid Mech.
, 710
(11
), pp. 5
–34
.17.
Hutchins
, N.
, 2012
, “Caution: Tripping Hazards
,” J. Fluid Mech.
, 710
(11
), pp. 1
–4
.18.
Walsh
, M. J.
, and Anders
, J. B.
, Jr., 1989
, “Riblet/LEBU Research at NASA Langley
,” Appl. Sci. Res.
, 46
(3
), pp. 255
–262
.19.
Viswanath
, P.
, 2002
, “Aircraft Viscous Drag Reduction Using Riblets
,” Prog. Aerosp. Sci.
, 38
(6–7
), pp. 571
–600
.20.
Rothstein
, J. P.
, 2010
, “Slip on Superhydrophobic Surfaces
,” Annu. Rev. Fluid Mech.
, 42
(1
), pp. 89
–109
.21.
Collis
, S. S.
, Joslin
, R. D.
, Seifert
, A.
, and Theofilis
, V.
, 2004
, “Issues in Active Flow Control: Theory, Control, Simulation, and Experiment
,” Prog. Aerosp. Sci.
, 40
(4
), pp. 237
–289
.22.
Cattafesta
, L. N.
, and Sheplak
, M.
, 2011
, “Actuators for Active Flow Control
,” Annu. Rev. Fluid Mech.
, 43
(1
), pp. 247
–272
.23.
Moreau
, E.
, 2007
, “Airflow Control by Non-Thermal Plasma Actuators
,” J. Phys. D: Appl. Phys.
, 40
(3
), pp. 605
–636
.24.
Corke
, T.
, and Post
, M.
, 2005
, “Overview of Plasma Flow Control: Concepts, Optimization, and Applications
,” AIAA
Paper No. 2005-563.25.
Corke
, T. C.
, Post
, M. L.
, and Orlov
, D. M.
, 2007
, “SDBD Plasma Enhanced Aerodynamics: Concepts, Optimization and Applications
,” Prog. Aerosp. Sci.
, 43
(7–8
), pp. 193
–217
.26.
Corke
, T. C.
, Post
, M. L.
, and Orlov
, D. M.
, 2009
, “Single Dielectric Barrier Discharge Plasma Enhanced Aerodynamics: Physics, Modeling and Applications
,” Exp. Fluids
, 46
(1
), pp. 1
–26
.27.
Corke
, T. C.
, Enloe
, C. L.
, and Wilkinson
, S. P.
, 2010
, “Dielectric Barrier Discharge Plasma Actuators for Flow Control
,” Annu. Rev. Fluid Mech.
, 42
(1
), pp. 505
–529
.28.
Wang
, J.-J.
, Choi
, K.-S.
, Feng
, L.-H.
, Jukes
, T. N.
, and Whalley
, R. D.
, 2013
, “Recent Developments in DBD Plasma Flow Control
,” Prog. Aerosp. Sci.
, 62
(1
), pp. 52
–78
.29.
Bletzinger
, P.
, Ganguly
, B. N.
, Wie
, D. V.
, and Garscadden
, A.
, 2005
, “Plasmas in High Speed Aerodynamics
,” J. Phys. D: Appl. Phys.
, 38
(4
), p. R33
.30.
Benard
, N.
, and Moreau
, E.
, 2014
, “Electrical and Mechanical Characteristics of Surface AC Dielectric Barrier Discharge Plasma Actuators Applied to Airflow Control
,” Exp. Fluids
, 55
(11
), pp. 1
–43
.31.
Kotsonis
, M.
, 2015
, “Diagnostics for Characterisation of Plasma Actuators
,” Meas. Sci. Technol.
, 26
(9
), p. 092001
.32.
Kogelschatz
, U.
, Eliasson
, B.
, and Egli
, W.
, 1999
, “From Ozone Generators to Flat Television Screens: History and Future Potential of Dielectric-Barrier Discharges
,” Pure Appl. Chem.
, 71
(10
), pp. 1819
–1828
.33.
Kogelschatz
, U.
, 2003
, “Dielectric-Barrier Discharges: Their History, Discharge Physics, and Industrial Applications
,” Plasma Chem. Plasma Process.
, 23
(1
), pp. 1
–46
.34.
Raizer
, Y. P.
, Shneider
, M. N.
, and Yatsenko
, N. A.
, 1995
, Radio-Frequency Capacitive Discharges
, CRC Press
, Boca Raton, FL
.35.
Eliasson
, B.
, and Kogelschatz
, U.
, 1991
, “Modeling and Applications of Silent Discharge Plasmas
,” IEEE Trans. Plasma Sci.
, 19
(2
), pp. 309
–323
.36.
Jayaraman
, B.
, and Shyy
, W.
, 2008
, “Modeling of Dielectric Barrier Discharge-Induced Fluid Dynamics and Heat Transfer
,” Prog. Aerosp. Sci.
, 44
(3
), pp. 139
–191
.37.
Shneider
, M.
, Likhanskii
, A.
, Macheret
, S.
, Opaits
, D.
, and Miles
, D.
, 2010
, “State-of-the-Art High-Fidelity DBD Plasma Simulations
,” AFOSR DBD Plasma Actuator Workshop, Gainesville, FL, Feb. 24–25.38.
Kriegseis
, J.
, 2011
, “Performance Characterization and Quantification of Dielectric Barrier Discharge Plasma Actuators
,” Ph.D. thesis
, TU Darmstadt, Darmstadt, Germany.39.
Velkoff
, H. R.
, and Ketcham
, J.
, 1968
, “Effect of an Electrostatic Field on Boundary-Layer Transition
,” AIAA J.
, 6
(7), pp. 1381
–1383
.40.
Roth
, J.
, 1995
, “Steady-State Glow Discharge Plasma
,” U.S. Patent No. 5,387,842
.41.
Roth
, J. R.
, Sherman
, D.
, and Wilkinson
, S. P.
, 1998
, “Boundary Layer Flow Control With a One Atmosphere Uniform Glow Discharge Surface Plasma
,” AIAA
Paper No. 1998-0328.42.
Caruana
, D.
, 2010
, “Plasmas for Aerodynamic Control
,” Plasma Phys. Controlled Fusion
, 52
(12
), p. 124045
.43.
Bénard
, N.
, Balcon
, N.
, and Moreau
, E.
, 2008
, “Electric Wind Produced by a Surface Dielectric Barrier Discharge Operating in Air at Different Pressures: Aeronautical Control Insights
,” J. Phys. D: Appl. Phys.
, 41
(4
), p. 042002
.44.
Wu
, Y.
, Li
, Y.
, Jia
, M.
, Song
, H.
, Guo
, Z.
, Zhu
, X.
, and Pu
, Y.
, 2008
, “Influence of Operating Pressure on Surface Dielectric Barrier Discharge Plasma Aerodynamic Actuation Characteristics
,” Appl. Phys. Lett.
, 93
(3
), p. 031503
.45.
Versailles
, P.
, Gingras-Gosselin
, V.
, and Vo
, H.
, 2010
, “Impact of Pressure and Temperature on the Performance of Plasma Actuators
,” AIAA J.
, 48
(4
), pp. 859
–863
.46.
Vo
, H. D.
, Cameron
, J. D.
, and Morris
, S. C.
, 2008
, “Control of Short Length-Scale Rotating Stall Inception on a High-Speed Axial Compressor With Plasma Actuation
,” ASME
Paper No. GT2008-50967.47.
Grundmann
, S.
, Frey
, M.
, and Tropea
, C.
, 2009
, “Unmanned Aerial Vehicle (UAV) With Plasma Actuators for Separation Control
,” AIAA
Paper No. 2009-698.48.
Leonov
, S. B.
, and Yarantsev
, D. A.
, 2008
, “Near-Surface Electrical Discharge in Supersonic Airflow: Properties and Flow Control
,” J. Propul. Power
, 24
(6
), pp. 1168
–1181
.49.
Grundmann
, S.
, and Tropea
, C.
, 2009
, “Experimental Damping of Boundary-Layer Oscillations Using DBD Plasma Actuators
,” Int. J. Heat Fluid Flow
, 30
(3
), pp. 394
–402
.50.
Séraudie
, A.
, Vermeersch
, O.
, and Arnal
, D.
, 2011
, “DBD Plasma Actuator Effect on a 2D Model Laminar Boundary Layer. Transition Delay Under Ionic Wind Effect
,” AIAA
Paper No. 2011-3515.51.
Jolibois
, J.
, Forte
, M.
, and Moreau
, R.
, 2008
, “Application of an AC Barrier Discharge Actuator to Control Airflow Separation Above a NACA 0015 Airfoil: Optimization of the Actuation Location Along the Chord
,” J. Electrost.
, 66
(9–10
), pp. 496
–503
.52.
Patel
, M. P.
, Ng
, T. T.
, Vasudevan
, S.
, Corke
, T.
, Post
, M.
, McLaughlin
, T.
, and Suchomel
, C. F.
, 2008
, “Scaling Effects of an Aerodynamic Plasma Actuator
,” J. Aircr.
, 45
(1
), pp. 223
–236
.53.
Post
, M. L.
, and Corke
, T. C.
, 2004
, “Separation Control on High Angle of Attack Airfoil Using Plasma Actuators
,” AIAA J.
, 42
(11
), pp. 2177
–2184
.54.
Wilkinson
, S. P.
, 2003
, “Investigation of an Oscillating Surface Plasma for Turbulent Drag Reduction
,” AIAA
Paper No. 2003-1023.55.
Soldati
, A.
, 2000
, “Modulation of Turbulent Boundary Layer by EHD Flows
,” ERCOFTAC Bull.
, 44
, pp. 50
–56
.56.
Kozlov
, A. V.
, and Thomas
, F. O.
, 2011
, “Bluff-Body Flow Control Via Two Types of Dielectric Barrier Discharge Plasma Actuation
,” AIAA J.
, 49
(9
), pp. 1919
–1931
.57.
Kozlov
, A. V.
, and Thomas
, F. O.
, 2011
, “Plasma Flow Control of Cylinders in a Tandem Configuration
,” AIAA J.
, 49
(10
), pp. 2183
–2193
.58.
Lemire
, S.
, Vo
, H. D.
, and Benner
, M. W.
, 2009
, “Performance Improvement of Axial Compressors and Fans With Plasma Actuation
,” Int. J. Rotating Mach.
, 2009
, p. 247613
.59.
Li
, Y.-h.
, Wu
, Y.
, Zhou
, M.
, Su
, C.-b.
, Zhang
, X.-w.
, and Zhu
, J.-q.
, 2010
, “Control of the Corner Separation in a Compressor Cascade by Steady and Unsteady Plasma Aerodynamic Actuation
,” Exp. Fluids
, 48
(6
), pp. 1015
–1023
.60.
Grundmann
, S.
, Sayles
, E.
, and Eaton
, J.
, 2011
, “Sensitivity of an Asymmetric 3D Diffuser to Plasma-Actuator Induced Inlet Condition Perturbations
,” Exp. Fluids
, 50
(1), pp. 1
–15
.61.
Kriegseis
, J.
, Möller
, B.
, Grundmann
, S.
, and Tropea
, C.
, 2012
, “On Performance and Efficiency of Dielectric Barrier Discharge Plasma Actuators for Flow Control Applications
,” Int. J. Flow Control
, 4
(3–4
), pp. 125
–131
.62.
Kriegseis
, J.
, Duchmann
, A.
, Tropea
, C.
, and Grundmann
, S.
, 2013
, “On the Classification of Dielectric Barrier Discharge Plasma Actuators: A Comprehensive Performance Evaluation Study
,” J. Appl. Phys.
, 114
(5
), p. 053301
.63.
Roth
, R. J.
, and Dai
, X.
, 2006
, “Optimization of the Aerodynamic Plasma Actuator as an Electrohydrodynamic (EHD) Electrical Device
,” AIAA
Paper No. 2006-1203.64.
Seifert
, A.
, 2015
, “Evaluation Criteria and Performance Comparison of Actuators
,” Instability and Control of Massively Separated Flows
(Fluid Mechanics and Its Applications), Vol. 107
, V.
Theofilis
and J.
Soria
, eds., Springer International Publishing
, Switzerland
, pp. 59
–64
.65.
Weier
, T.
, Gerbeth
, G.
, Mutschke
, G.
, Lielausis
, O.
, and Lammers
, G.
, 2003
, “Control of Flow Separation Using Electromagnetic Forces
,” Flow, Turbul. Combust.
, 71
(1–4
), pp. 5
–17
.66.
Schwier
, W.
, 1943
, “Blasversuche zur Auftriebssteigerung am Profil 23015 mit verschiedenen Klappenformen
,” Zentrale f. wiss. Berichtswesen, Berlin-Adlershof, Technical Report No. 1865.67.
Poisson-Quinton
, P.
, 1956
, Einige physikalische Betrachtungen über das Ausblasen an Tragflügeln
, Jahrbuch der WGL
, 1956
(1
), pp. 29
–51
.68.
Hanson
, R. E.
, Houser
, N. M.
, and Lavoie
, P.
, 2014
, “Dielectric Material Degradation Monitoring of Dielectric Barrier Discharge Plasma Actuators
,” J. Appl. Phys.
, 115
(4
), p. 043301
.69.
Houser
, N.
, Gimeno
, L.
, Hanson
, R.
, Goldhawk
, T.
, Simpson
, T.
, and Lavoie
, P.
, 2013
, “Microfabrication of Dielectric Barrier Discharge Plasma Actuators for Flow Control
,” Sens. Actuators, A
, 201
, pp. 101
–104
.70.
Zito
, J. C.
, Durscher
, R. J.
, Soni
, J.
, Roy
, S.
, and Arnold
, D. P.
, 2012
, “Flow and Force Inducement Using Micron Size Dielectric Barrier Discharge Actuators
,” Appl. Phys. Lett.
, 100
(19
), p. 193502
.71.
Soni
, J.
, and Roy
, S.
, 2013
, “Design and Characterization of a Nano-Newton Resolution Thrust Stand
,” Rev. Sci. Instrum.
, 84
(9
), p. 112908
.72.
Joussot
, R.
, Leroy
, A.
, Weber
, R.
, Rabat
, H.
, Loyer
, S.
, and Hong
, D.
, 2013
, “Plasma Morphology and Induced Airflow Characterization of a DBD Actuator With Serrated Electrode
,” J. Phys. D: Appl. Phys.
, 46
(12
), p. 125204
.73.
Wang
, C.-C.
, Durscher
, R.
, and Roy
, S.
, 2011
, “Three-Dimensional Effects of Curved Plasma Actuators in Quiescent Air
,” J. Appl. Phys.
, 109
(8
), p. 083305
.74.
Berendt
, A.
, Podliński
, J.
, and Mizeraczyk
, J.
, 2011
, “Elongated DBD With Floating Interelectrodes for Actuators
,” Eur. Phys. J.: Appl. Phys.
, 55
(1
), p. 13804
.75.
Bénard
, N.
, Balcon
, N.
, and Moreau
, E.
, 2008
, “Electric Wind Produced by a Single Dielectric Barrier Discharge Actuator Operating in Atmospheric Flight Conditions-Pressure Outcome
,” AIAA
Paper No. 2008-3792.76.
Forte
, M.
, Jolibois
, J.
, Moreau
, E.
, Touchard
, G.
, and Cazalens
, M.
, 2006
, “Optimization of a Dielectric Barrier Discharge Actuator by Stationary and Non-Stationary Measurements of the Induced Flow Velocity-Application to Airflow Control
,” AIAA
Paper No. 2006-2863.77.
Nersisyan
, G.
, and Graham
, W. G.
, 2004
, “Characterization of a Dielectric Barrier Discharge Operating in an Open Reactor With Flowing Helium
,” Plasma Sources Sci. Technol.
, 13
(4
), pp. 582
–587
.78.
Enloe
, C. L.
, McLaughlin
, T. E.
, VanDyken
, R. D.
, Kachner
, K. D.
, Jumper
, E. J.
, and Corke
, T. C.
, 2004
, “Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology
,” AIAA J.
, 42
(3
), pp. 589
–594
.79.
Enloe
, C. L.
, McLaughlin
, T. E.
, Gregory
, J. W.
, Medina
, R. A.
, and Miller
, W. S.
, 2008
, “Surface Potential and Electric Field Structure in the Aerodynamic Plasma Actuator
,” AIAA
Paper No. 2008-1103.80.
Gibalov
, V. I.
, and Pietsch
, G. J.
, 2000
, “The Development of Dielectric Barrier Discharges in Gas Gaps and on Surfaces
,” J. Phys. D: Appl. Phys.
, 33
(20
), p. 2618
.81.
Enloe
, C. L.
, Font
, G. I.
, McLaughlin
, T. E.
, and Orlov
, D. M.
, 2008
, “Surface Potential and Longitudinal Electric Field Measurements in the Aerodynamic Plasma Actuator
,” AIAA J.
, 46
(11
), pp. 2730
–2740
.82.
Orlov
, D. M.
, Font
, G. I.
, and Edelstein
, D.
, 2008
, “Characterization of Discharge Modes of Plasma Actuators
,” AIAA J.
, 46
(12
), pp. 3142
–3148
.83.
Hoskinson
, A. R.
, Oksuz
, L.
, and Hershkowitz
, N.
, 2008
, “Microdischarge Propagation and Expansion in a Surface Dielectric Barrier Discharge
,” Appl. Phys. Lett.
, 93
(22
), p. 221501
.84.
Orlov
, D.
, 2006
, “Modelling and Simulation of Single Dielectric Barrier Discharge Plasma Actuators
,” Ph.D. thesis
, University of Notre Dame, Notre Dame, IN.85.
Orlov
, D.
, Corke
, T.
, and Patel
, M.
, 2006
, “Electric Circuit Model for Aerodynamic Plasma Actuator
,” AIAA
Paper No. 2006-1206.86.
Kriegseis
, J.
, Grundmann
, S.
, and Tropea
, C.
, 2011
, “Power Consumption, Discharge Capacitance and Light Emission as Measures for Thrust Production of Dielectric Barrier Discharge Plasma Actuators
,” J. Appl. Phys.
, 110
(1
), p. 013305
.87.
Porter
, C. O.
, Baughn
, J. W.
, McLaughlin
, T. E.
, Enloe
, C. L.
, and Font
, G. I.
, 2007
, “Plasma Actuator Force Measurements
,” AIAA J.
, 45
(7
), pp. 1562
–1570
.88.
Gregory
, J. W.
, Enloe
, C. L.
, Font
, G. I.
, and McLaughlin
, T. E.
, 2007
, “Force Production Mechanisms of a Dielectric-Barrier Discharge Plasma Actuator
,” AIAA
Paper No. 2007-185.89.
Do
, H.
, Kim
, W.
, Capelli
, M. A.
, and Mungal
, M. G.
, 2008
, “Cross-Talk in Multiple Dielectric Barrier Discharge Actuators
,” Appl. Phys. Lett.
, 92
(7
), p. 071504
.90.
Enloe
, C. L.
, McLaughlin
, T. E.
, VanDyken
, R. D.
, Kachner
, K. D.
, Jumper
, E. J.
, Corke
, T. C.
, Post
, M.
, and Haddad
, O.
, 2004
, “Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Geometric Effects
,” AIAA J.
, 42
(3
), pp. 595
–604
.91.
Kriegseis
, J.
, Möller
, B.
, Grundmann
, S.
, and Tropea
, C.
, 2011
, “Capacitance and Power Consumption Quantification of Dielectric Barrier Discharge (DBD) Plasma Actuators
,” J. Electrost.
, 69
(4
), pp. 302
–312
.92.
Allégraud
, K.
, Guaïtella
, O.
, and Rousseau
, A.
, 2007
, “Spatio-Temporal Breakdown in Surface DBDs: Evidence of Collective Effect
,” J. Phys. D: Appl. Phys.
, 40
(24
), p. 7698
.93.
Dedrick
, J.
, Boswell
, R. W.
, Audier
, P.
, Rabat
, H.
, Hong
, D.
, and Charles
, C.
, 2011
, “Plasma Propagation of a 13.56 MHz Asymmetric Surface Barrier Discharge in Atmospheric Pressure Air
,” J. Phys. D: Appl. Phys.
, 44
(20
), p. 205202
.94.
Takashima
, K.
, Zouzou
, N.
, Moreau
, E.
, Mizuno
, A.
, and Touchard
, G.
, 2007
, “Generation of Extended Surface Barrier Discharge on Dielectric Surface—Electrical Properties
,” Int. J. Plasma Environ. Sci. Technol.
, 1
(1
), pp. 14
–20
.95.
Porter
, C.
, Abbas
, A.
, Cohen
, K.
, McLaughlin
, T.
, and Enloe
, C.
, 2009
, “Spatially Distributed Forcing and Jet Vectoring With a Plasma Actuator
,” AIAA J.
, 47
(6
), pp. 1368
–1378
.96.
Abe
, T.
, Takizawa
, Y.
, and Sato
, S.
, 2008
, “Experimental Study for Momentum Transfer in a Dielectric Barrier Discharge Plasma Actuator
,” AIAA J.
, 46
(9
), pp. 2248
–2256
.97.
Dong
, B.
, Bauchire
, J. M.
, Pouvesle
, J. M.
, Magnier
, P.
, and Hong
, D.
, 2008
, “Experimental Study of a DBD Surface Discharge for the Active Control of Subsonic Airflow
,” J. Phys. D: Appl. Phys.
, 41
(15
), p. 155201
.98.
Forte
, M.
, Jolibois
, J.
, Pons
, J.
, Moreau
, E.
, Touchard
, G.
, and Cazalens
, M.
, 2007
, “Optimization of a Dielectric Barrier Discharge Actuator by Stationary and Non-Stationary Measurements of the Induced Flow Velocity: Application to Airflow Control
,” Exp. Fluids
, 43
(6
), pp. 917
–928
.99.
Pons
, J.
, Moreau
, E.
, and Touchard
, G.
, 2005
, “Asymmetric Surface Dielectric Barrier Discharge in Air at Atmospheric Pressure: Electrical Properties and Induced Airflow Characteristics
,” J. Phys. D: Appl. Phys.
, 38
(19
), p. 3635
.100.
Kriegseis
, J.
, Dehler
, T.
, Pawlik
, M.
, and Tropea
, C.
, 2009
, “Pattern-Identification Study of the Flow in Proximity of a Plasma Actuator
,” AIAA
Paper No. 2009-1001.101.
Grundmann
, S.
, 2008
, “Transition Control Using Dielectric Barrier Discharge Actuators
,” Ph.D. thesis, Technische Universität Darmstadt, Darmstadt, Germany.102.
Bénard
, N.
, Moreau
, E.
, Griffin
, J.
, and Cattafesta
, L. N.
, III, 2009
, “Plasma Flow Control—Autonomous Lift Improvement by Slope-Seeking
,” AIAA
Paper No. 2009-4182.103.
Orlov
, D.
, and Corke
, T. C.
, 2005
, “Numerical Simulation of Aerodynamic Plasma Actuator Effects
,” AIAA
Paper No. 2005-1083.104.
Little
, J.
, Nishihara
, M.
, Adamovich
, I.
, and Samimy
, M.
, 2010
, “High-Lift Airfoil Trailing Edge Separation Control Using a Single Dielectric Barrier Discharge Plasma Actuator
,” Exp. Fluids
, 48
(3
), pp. 521
–537
.105.
Baughn
, J. W.
, Porter
, C. O.
, Peterson
, B. L.
, McLaughlin
, T. E.
, Enloe
, C. L.
, Font
, G. I.
, and Baird
, C.
, 2006
, “Momentum Transfer for an Aerodynamic Plasma Actuator With an Imposed Boundary Layer
,” AIAA
Paper No. 2006-166.106.
Porter
, C. O.
, Baughn
, J. W.
, McLaughlin
, T. E.
, Enloe
, C. L.
, and Font
, G. I.
, 2006
, “Temporal Force Measurements on an Aerodynamic Plasma Actuator
,” AIAA
Paper No. 2006-1206.107.
Abe
, T.
, Takizawa
, Y.
, and Sato
, S.
, 2007
, “A Parametric Experimental Study for Momentum Transfer by Plasma Actuator
,” AIAA
Paper No. 2007-185.108.
Borcia
, G.
, Anderson
, C. A.
, and Brown
, N. M. D.
, 2003
, “Dielectric Barrier Discharge for Surface Treatment: Application to Selected Polymers in Film and Fibre Form
,” Plasma Sources Sci. Technol.
, 12
(3
), pp. 335
–344
.109.
Manley
, T. C.
, 1943
, “The Electric Characteristics of the Ozonator Discharge
,” J. Electrochem. Soc.
, 84
(1
), pp. 83
–96
.110.
Wagner
, H. E.
, Brandenburg
, R.
, Kozlov
, K. V.
, Sonnenfeld
, A.
, Michel
, P.
, and Behnke
, J. F.
, 2003
, “The Barrier Discharge: Basic Properties and Applications to Surface Treatment
,” Vacuum
, 71
(3
), pp. 417
–436
.111.
Falkenstein
, Z.
, and Coogan
, J. J.
, 1997
, “Microdischarge Behaviour in the Silent Discharge of Nitrogen–Oxygen and Water–Air Mixtures
,” J. Phys. D: Appl. Phys.
, 30
(5
), pp. 817
–825
.112.
Bénard
, N.
, Cattafesta
, I. L. N.
, Moreau
, E.
, Griffin
, J.
, and Bonnet
, J. P.
, 2011
, “On the Benefits of Hysteresis Effects for Closed-Loop Separation Control Using Plasma Actuation
,” Phys. Fluids
, 23
(8
), p. 083601
.113.
Takahashi
, Y.
, Rabins
, M.
, and Auslander
, D.
, 1970
, Control and Dynamic Systems
, Addison-Wesley Publishing
, Reading, MA
.114.
Yang
, X.
, Zhitao
, Z.
, Cheng
, L.
, and Yu
, X.
, 2005
, “Effect of Systematic Resonance on DBD Device
,” Plasma Sci. Technol.
, 7
(5
), p. 3030
.115.
Coogan
, J. J.
, 2005
, “Pathogen Control in Complex Fluids With Water-Coupled Excimer Lamps at 282 and 308 nm
,” Photochem. Photobiol.
, 81
(6
), pp. 1511
–1517
.116.
Chen
, Z.
, 2002
, “Impedance Matching for One Atmosphere Uniform Glow Discharge Plasma (OAUGDP) Reactors
,” IEEE Trans. Plasma Sci.
, 30
(5
), pp. 1922
–1930
.117.
Chen
, Z.
, 2007
, “Impedance Matching and PSpice Simulation of One Atmosphere Uniform Glow Discharge Plasma (OAUGDP) Reactor/Actuator Systems
,” Ph.D. thesis
, The University of Tennessee, Knoxville, TN.118.
Singh
, K. P.
, and Roy
, S.
, 2007
, “Impedance Matching for an Asymmetric Dielectric Barrier Discharge Plasma Actuator
,” Appl. Phys. Lett.
, 91
(8
), p. 081504
.119.
Opaits
, D. F.
, Neretti
, G.
, Likhanskii
, A. V.
, Zaidi
, S.
, Shneider
, M. N.
, and Miles
, R. B.
, 2007
, “Experimental Investigation of DBD Plasma Actuators Driven by Repetitive High Voltage Nanosecond Pulses With DC or Low-Frequency Sinusoidal Bias
,” AIAA
Paper No. 2007-4532.120.
Opaits
, D. F.
, Likhanskii
, A. V.
, Neretti
, G.
, Zaidi
, S.
, Shneider
, M. N.
, Miles
, R. B.
, and Macheret
, S. O.
, 2008
, “Experimental Investigation of Dielectric Barrier Discharge Plasma Actuators Driven by Repetitive High-Voltage Nanosecond Pulses With DC or Low Frequency Sinusoidal Bias
,” J. Appl. Phys.
, 104
(4
), p. 043304
.121.
Zito
, J. C.
, Arnold
, D. P.
, Durscher
, R. J.
, and Roy
, S.
, 2010
, “Investigation of Impedance Characteristics and Power Delivery for Dielectric Barrier Discharge Plasma Actuators
,” AIAA
Paper No. 2010-0964.122.
Orlov
, D.
, Apker
, T.
, He
, C.
, Othman
, H.
, and Corke
, T.
, 2007
, “Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators
,” AIAA
Paper No. 2007-0877.123.
Huang
, X.
, Zhang
, X.
, and Li
, Y.
, 2010
, “Broadband Flow-Induced Sound Control Using Plasma Actuators
,” J. Sound Vib.
, 329
(13
), pp. 2477
–2489
.124.
Liu
, S.
, and Neiger
, M.
, 2001
, “Excitation of Dielectric Barrier Discharges by Unipolar Submicrosecond Square Pulses
,” J. Phys. D: Appl. Phys.
, 34
(11
), pp. 1632
–1638
.125.
Enloe
, C. L.
, McHarg
, M. G.
, Font
, G. I.
, and McLaughlin
, T. E.
, 2009
, “Plasma-Induced Force and Self-Induced Drag in the Dielectric Barrier Discharge Aerodynamic Plasma Actuator
,” AIAA
Paper No. 2009-1622.126.
Baird
, C.
, Enloe
, C. L.
, McLaughlin
, T. E.
, and Baughn
, J. W.
, 2005
, “Acoustic Testing of the Dielectric Barrier Discharge (DBD) Plasma Actuator
,” AIAA
Paper No. 2005-565.127.
Font
, G. I.
, and Morgan
, W. L.
, 2005
, “Plasma Discharges in Atmospheric Pressure Oxygen for Boundary Layer Separation Control
,” AIAA
Paper No. 2005-4632.128.
Boeuf
, J. P.
, Lagmich
, Y.
, Unfer
, T.
, Callegari
, T.
, and Pitchford
, L. C.
, 2007
, “Electrohydrodynamic Force in Dielectric Barrier Discharge Plasma Actuators
,” J. Phys. D: Appl. Phys.
, 40
(3
), pp. 652
–662
.129.
Font
, G. I.
, Enloe
, C. L.
, and McLaughlin
, T. E.
, 2010
, “Plasma Volumetric Effects on the Force Production of a Plasma Actuator
,” AIAA J.
, 48
(9
), pp. 1869
–1874
.130.
Likhanskii
, A. V.
, Shneider
, M. N.
, Macheret
, S. O.
, and Miles
, R. B.
, 2006
, “Modeling of Interaction Between Weakly Ionized Near-Surface Plasmas and Gas Flow
,” AIAA
Paper No. 2006-1204.131.
Hoskinson
, A. R.
, Hershkowitz
, N.
, and Ashpis
, D. E.
, 2008
, “Force Measurements of Single and Double Barrier DBD Plasma Actuators in Quiescent Air
,” J. Phys. D: Appl. Phys.
, 41
(24
), p. 245209
.132.
Hoskinson
, A.
, and Hershkowitz
, N.
, 2010
, “Differences Between Dielectric Barrier Discharge Plasma Actuators With Cylindrical and Rectangular Exposed Electrodes
,” J. Phys. D: Appl. Phys.
, 43
(6
), p. 065205
.133.
Debien
, A.
, Benard
, N.
, David
, L.
, and Moreau
, E.
, 2012
, “Unsteady Aspect of the Electrohydrodynamic Force Produced by Surface Dielectric Barrier Discharge Actuators
,” Appl. Phys. Lett.
, 100
(1
), p. 013901
.134.
Durscher
, R.
, and Roy
, S.
, 2012
, “Evaluation of Thrust Measurement Techniques for Dielectric Barrier Discharge Actuators
,” Exp. Fluids
, 53
(4
), pp. 1165
–1176
.135.
Enloe
, C. L.
, McLaughlin
, T. E.
, VanDyken
, R. D.
, Kachner
, K. D.
, Jumper
, E. J.
, and Corke
, T. C.
, 2003
, “Mechanisms and Responses of a Single Dielectric Barrier Plasma
,” AIAA
Paper No. 2003-1021.136.
Kriegseis
, J.
, Möller
, B.
, Grundmann
, S.
, and Tropea
, C.
, 2011
, “Light Emission, Discharge Capacitance and Thrust Production of DBD Plasma Actuators
,” AIAA
Paper No. 2011-155.137.
Van Dyken
, R.
, McLaughlin
, T. E.
, and Enloe
, C. L.
, 2004
, “Parametric Investigations of a Single Dielectric Barrier Plasma Actuator
,” AIAA
Paper No. 2004-0846.138.
Poon
, D.
, Simon
, T.
, Kortshagen
, U.
, and Ernie
, D.
, 2010
, “Experimental Studies of Plasma Actuator Performance for Separation Control
,” AIAA
Paper No. 2010-1219.139.
Thomas
, F. O.
, Corke
, T. C.
, Iqbal
, M.
, Kozlov
, A.
, and Schatzman
, D.
, 2009
, “Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control
,” AIAA J.
, 47
(9
), pp. 2169
–2178
.140.
Takagaki
, M.
, Isono
, S.
, Nagai
, H.
, and Asai
, K.
, 2008
, “Evaluation of Plasma Actuator Performance in Martian Atmosphere for Applications to Mars Airplanes
,” AIAA
Paper No. 2008-3762.141.
Ferry
, J. W.
, and Rovey
, L.
, 2010
, “Thrust Measurement of Dielectric Barrier Discharge Plasma Actuators and Power Requirements for Aerodynamic Control
,” AIAA
Paper No. 2010-4982.142.
Jolibois
, J.
, and Moreau
, E.
, 2009
, “Enhancement of the Electromechanical Performances of a Single Dielectric Barrier Discharge Actuator
,” IEEE Trans. Dielectr. Electr. Insul.
, 16
(3
), pp. 758
–767
.143.
Jolibois
, J.
, Zouzou
, N.
, Moreau
, E.
, and Tatibout
, J.
, 2011
, “Generation of Surface DBD on Rough Dielectric: Electrical Properties, Discharge-Induced Electric Wind and Generated Chemical Species
,” J. Electrost.
, 69
(6
), pp. 522
–528
.144.
Moreau
, E.
, Sosa
, R.
, and Artana
, G.
, 2008
, “Electric Wind Produced by Surface Plasma Actuators: A New Dielectric Barrier Discharge Based on a Three-Electrode Geometry
,” J. Phys. D: Appl. Phys.
, 41
(11), p. 115204
.145.
Glauert
, M. B.
, 1956
, “The Wall Jet
,” J. Fluid Mech.
, 1
(6
), pp. 625
–643
.146.
Jukes
, T.
, Choi
, K.
, Johnson
, G.
, and Scott
, S.
, 2006
, “Characterization of Surface Plasma-Induced Wall Flows Through Velocity and Temperature Measurements
,” AIAA J.
, 44
(4
), pp. 764
–771
.147.
Murphy
, J. P.
, Kriegseis
, J.
, and Lavoie
, P.
, 2013
, “Scaling of Maximum Velocity, Body Force, and Power Consumption of Dielectric Barrier Discharge Plasma Actuators Via Particle Image Velocimetry
,” J. Appl. Phys.
, 113
(24
), p. 243301
.148.
Maden
, I.
, Maduta
, R.
, Kriegseis
, J.
, Jakirlić
, S.
, Schwarz
, C.
, Grundmann
, S.
, and Tropea
, C.
, 2013
, “Experimental and Computational Study of the Flow Induced by a Plasma Actuator
,” Int. J. Heat Fluid Flow
, 41
, pp. 80
–89
.149.
Kriegseis
, J.
, Schwarz
, C.
, Duchmann
, A.
, Grundmann
, S.
, and Tropea
, C.
, 2012
, “PIV-Based Estimation of DBD Plasma-Actuator Force Terms
,” AIAA
Paper No. 2012-0411.150.
Kriegseis
, J.
, Schwarz
, C.
, Tropea
, C.
, and Grundmann
, S.
, 2013
, “Velocity-Information-Based Force-Term Estimation of Dielectric-Barrier Discharge Plasma Actuators
,” J. Phys. D: Appl. Phys.
, 46
(5
), p. 055202
.151.
Jukes
, T. N.
, and Choi
, K.-S.
, 2013
, “On the Formation of Streamwise Vortices by Plasma Vortex Generators
,” J. Fluid Mech.
, 733
(1
), pp. 370
–393
.152.
Kotsonis
, M.
, Ghaemi
, S.
, Veldhuis
, L.
, and Scarano
, F.
, 2011
, “Measurement of the Body Force Field of Plasma Actuators
,” J. Phys. D: Appl. Phys.
, 44
(4
), p. 045204
.153.
Greenblatt
, D.
, Göksel
, B.
, Rechenberg
, I.
, Schüle
, C. Y.
, Romann
, D.
, and Paschereit
, C. O.
, 2008
, “Dielectric Barrier Discharge Flow Control at Very Low Flight Reynolds Numbers
,” AIAA J.
, 46
(6
), pp. 1528
–1541
.154.
Wilke
, B.
, 2009
, “Aerodynamische Strömungssteuerung mittels dielektrischen Barriereentladungs-Plasmaaktuatoren
,” Ph.D. thesis, Technische Universität Darmstadt, DLR Göttingen, Germany.155.
Albrecht
, T.
, Weier
, T.
, Gerbeth
, G.
, Metzkes
, H.
, and Stiller
, J.
, 2011
, “A Method to Estimate the Planar, Instantaneous Body Force Distribution From Velocity Field Measurements
,” Phys. Fluids
, 23
(2
), p. 021702
.156.
Dörr
, P. C.
, and Kloker
, M. J.
, 2015
, “Numerical Investigation of Plasma-Actuator Force-Term Estimations From Flow Experiments
,” J. Phys. D: Appl. Phys.
, 48
(39
), p. 395203
.157.
Benard
, N.
, Debien
, A.
, and Moreau
, E.
, 2013
, “Time-Dependent Volume Force Produced by a Non-Thermal Plasma Actuator From Experimental Velocity Field
,” J. Phys. D: Appl. Phys.
, 46
(24
), p. 245201
.158.
Neumann
, M.
, Friedrich
, C.
, Czarske
, J.
, Kriegseis
, J.
, and Grundmann
, S.
, 2013
, “Determination of the Phase-Resolved Body Force Produced by a Dielectric Barrier Discharge Plasma Actuator
,” J. Phys. D: Appl. Phys.
, 46
(4
), p. 042001
.159.
Lagmich
, Y.
, Callegari
, T.
, Pitchford
, L. C.
, and Boeuf
, J. P.
, 2008
, “Model Description of Surface Dielectric Barrier Discharges for Flow Control
,” J. Phys. D: Appl. Phys.
, 41
(9
), p. 095205
.160.
Likhanskii
, A. V.
, Shneider
, M. N.
, Macheret
, S. O.
, and Miles
, R. B.
, 2008
, “Modeling of Dielectric Barrier Discharge Plasma Actuator in Air
,” J. Appl. Phys.
, 103
(5
), p. 053305
.161.
Singh
, K. P.
, and Roy
, S.
, 2008
, “Force Approximation for a Plasma Actuator Operating in Atmospheric Air
,” J. Appl. Phys.
, 103
(1
), p. 013305
.162.
Enloe
, C. L.
, McLaughlin
, T. E.
, VanDyken
, R. D.
, and Fischer
, J. C.
, 2004
, “Plasma Structure in the Aerodynamic Plasma Actuator
,” AIAA
Paper No. 2004-0844.163.
Giepman
, R. H. M.
, and Kotsonis
, M.
, 2011
, “On the Mechanical Efficiency of Dielectric Barrier Discharge Plasma Actuators
,” Appl. Phys. Lett.
, 98
(22
), p. 221504
.164.
Janssen
, G. M.
, 2000
, “Design of a General Plasma Simulation Model, Fundamental Aspects and Applications
,” Ph.D. thesis
, Technische Universität Eindhoven, Eindhoven, The Netherlands.165.
Léger
, L.
, Moreau
, E.
, and Touchard
, G.
, 2002
, “Electrohydrodynamic Airflow Control Along a Flat Plate by a DC Surface Corona Discharge—Velocity Profile and Wall Pressure Measurements
,” AIAA
Paper No. 2002-2833.166.
Mestiri
, R.
, Hadaji
, R.
, and Nasrallah
, S. B.
, 2010
, “An Experimental Study of a Plasma Actuator in Absence of Free Airflow: Ionic Wind Velocity Profile
,” Phys. Plasmas
, 17
(8
), p. 083503
.167.
Maden
, I.
, Kriegseis
, J.
, Maduta
, R.
, Jakirlic
, S.
, Schwarz
, C.
, Grundmann
, S.
, and Tropea
, C.
, 2012
, “Derivation of a Plasma-Actuator Model Utilizing Quiescent-Air PIV Data
,” 20th Annual Conference of the CFD
Society of Canada
, Canmore, AB, Canada.168.
Kriegseis
, J.
, Maden
, I.
, Schwarz
, C.
, Tropea
, C.
, and Grundmann
, S.
, 2015
, “Addendum to ‘Velocity-Information Based Force-Term Estimation of Dielectric Barrier Discharge Plasma Actuators’
,” J. Phys. D: Appl. Phys.
, 48
(32
), p. 329401
.169.
Shyy
, W.
, Jayaraman
, B.
, and Andersson
, A.
, 2002
, “Modeling of Glow Discharge-Induced Fluid Dynamics
,” J. Appl. Phys.
, 92
(11
), p. 6434
.170.
Suzen
, Y. B.
, Huang
, P. G.
, and Ashpis
, D. E.
, 2007
, “Numerical Simulations of Flow Separation Control in Low-Pressure Turbines Using Plasma Actuators
,” AIAA
Paper No. 2007-937.171.
Suzen
, Y. B.
, Huang
, P. G.
, Jacob
, J. D.
, and Ashpis
, D. E.
, 2005
, “Numerical Simulations of Plasma Based Flow Control Applications
,” AIAA
Paper No. 2005-4633.172.
Ibrahim
, I.
, and Skote
, M.
, 2012
, “Simulations of the Linear Plasma Synthetic Jet Actuator Utilizing a Modified Suzen–Huang Model
,” Phys. Fluids (1994-Present)
, 24
(11
), p. 113602
.173.
Politz
, C.
, Lawson
, N.
, Konrath
, R.
, Agocs
, J.
, and Schröder
, A.
, 2013
, “Development of Particle Image Velocimetry for In-Flight Flow Measurement
,” Advanced In-Flight Measurement Techniques
(Research Topics in Aerospace), F.
Boden
, N.
Lawson
, H. W.
Jentink
, and J.
Kompenhans
, eds., Springer
, Berlin/Heidelberg, Germany
, pp. 269
–289
.174.
Politz
, C.
, Roloff
, C.
, Geisler
, R.
, and Schröder
, A.
, 2014
, “Free Flight Boundary Layer Investigations by Means of Particle Image Velocimetry
,” 17th International Symposium on Applications of Laser Techniques to Fluid Mechanics
, Lisbon
, Portugal
, July 7–10.175.
Paschen
, F.
, 1889
, “Ueber die zum Funkenübergang in Luft, Wasserstoff und kohlensäure bei verschiedenen Drucken erforderliche Potentialdifferenz
,” Ann. Phys.
, 273
(5
), pp. 69
–96
.176.
Vollrath
, K.
, 1967
, “Funkenlichtquellen und Hochfrequenz-Funkenkinematographie
,” Kurzzeitphysik
, K.
Vollrath
and G.
Thomer
, eds., Springer
, Wien, Austria
, pp. 76
–165
.177.
Raju
, G. G.
, 2003
, Dielectrics in Electric Fields
, Marcel Dekker
, New York
.178.
Nichols
, T.
, and Rovey
, J.
, 2013
, “Surface Potential and Electric Field Measurements in Plasma Actuators at Low Pressures
,” AIAA J.
, 51
(5
), pp. 1054
–1065
.179.
Kriegseis
, J.
, Barckmann
, K.
, Frey
, J.
, Tropea
, C.
, and Grundmann
, S.
, 2014
, “Competition Between Pressure Effects and Airflow Influence for the Performance of Plasma Actuators
,” Phys. Plasmas (1994-Present)
, 21
(5
), p. 053511
.180.
Pavon
, S.
, Ott
, P.
, Leyland
, P.
, Dorier
, J.-L.
, and Hollenstein
, C.
, 2009
, “Effects of a Surface Dielectric Barrier Discharge on Transonic Flows Around an Airfoil
,” AIAA
Paper No. 2009-649.181.
Friz
, P. D.
, and Rovey
, J. L.
, 2014
, “The Effects of Electrode Size and Configuration on Plasma Actuator Thrust and Effectiveness at Low Pressure
,” Int. J. Flow Control
, 6
(2
), pp. 75
–86
.182.
Soni
, J.
, and Roy
, S.
, 2013
, “Low Pressure Characterization of Dielectric Barrier Discharge Actuators
,” Appl. Phys. Lett.
, 102
(11
), p. 112908
.183.
Schuele
, C. Y.
, and Corke
, T.
, 2008
, “Characteristics of Single Dielectric Barrier Discharge Plasma Actuators at Sub-Atmospheric Pressures
,” 61st Annual Meeting of the APS Division of Fluid Dynamics
, San Antonio, TX, APS Paper No. BAPS.2008.DFD.ET.9
.184.
Valerioti
, J. A.
, and Corke
, T. C.
, 2012
, “Pressure Dependence of Dielectric Barrier Discharge Plasma Flow Actuators
,” AIAA J.
, 50
(7
), pp. 1490
–1502
.185.
Bénard
, N.
, and Moreau
, E.
, 2010
, “Effects of Altitude on the Electromechanical Characteristics of a Single Dielectric Barrier Discharge Plasma Actuator
,” AIAA
Paper No. 2010-4633.186.
Ashpis
, D.
, and Thurman
, D.
, 2011
, “DBD Plasma Actuators for Flow Control in Air Vehicles and Jet Engines—Simulation of Flight Conditions in Test Chambers by Density Matching
,” AIAA
Paper No. 2011-3730.187.
Anderson
, R.
, and Roy
, S.
, 2006
, “Preliminary Experiments of Barrier Discharge Plasma Actuators Using Dry and Humid Air
,” AIAA
Paper No. 2006-0369.188.
Bénard
, N.
, Balcon
, N.
, and Moreau
, E.
, 2009
, “Electric Wind Produced by a Surface Dielectric Barrier Discharge Operating Over a Wide Range of Relative Humidity
,” AIAA
Paper No. 2009-488.189.
Ashpis
, D.
, and Laun
, M.
, 2014
, “Dielectric Barrier Discharge (DBD) Plasma Actuators Thrust—Measurement Methodology Incorporating New Anti-Thrust Hypothesis
,” AIAA
Paper No. 2014-0486.190.
Wicks
, M.
, and Thomas
, F. O.
, 2015
, “Effect of Relative Humidity on Dielectric Barrier Discharge Plasma Actuator Body Force
,” AIAA J.
, 53
(9
), pp. 2801
–2804
.191.
Opaits
, D. F.
, Neretti
, G.
, Zaidi
, S. H.
, Shneider
, M. N.
, Miles
, R. B.
, Likhanskii
, A. V.
, and Macheret
, S. O.
, 2008
, “DBD Plasma Actuators Driven by a Combination of Low Frequency Bias Voltage and Nanosecond Pulses
,” AIAA
Paper No. 2008-1372.192.
Font
, G. I.
, Enloe
, C. L.
, Newcomb
, J. Y.
, Teague
, A. L.
, Vasso
, A. R.
, and McLaughlin
, T. E.
, 2011
, “Effects of Oxygen Content on Dielectric Barrier Discharge Plasma Actuator Behavior
,” AIAA J.
, 49
(7
), pp. 1366
–1373
.193.
Enloe
, C.
, Baughn
, J.
, Font
, G.
, and McLaughlin
, T.
, 2006
, “Parameterization of Temporal Structure in the Single-Dielectric-Barrier Aerodynamic Plasma Actuator
,” AIAA J.
, 44
(6
), pp. 1127
–1136
.194.
Boeuf
, J. P.
, Lagmich
, Y.
, and Pitchford
, L. C.
, 2009
, “Contribution of Positive and Negative Ions to the Electrohydrodynamic Force in a Dielectric Barrier Discharge Plasma Actuator Operating in Air
,” J. Appl. Phys.
, 106
(2
), p. 023115
.195.
Pavon
, S.
, Dorier
, J.-L.
, Hollenstein
, C.
, Ott
, P.
, and Leyland
, P.
, 2007
, “Effects of High-Speed Airflows on a Surface Dielectric Barrier Discharge
,” J. Phys. D: Appl. Phys.
, 40
(6
), pp. 1733
–1741
.196.
Kriegseis
, J.
, Grundmann
, S.
, and Tropea
, C.
, 2012
, “Airflow Influence on the Discharge Performance of Dielectric Barrier Discharge Plasma Actuators
,” Phys. Plasmas
, 19
(7
), p. 073509
.197.
Soldati
, A.
, and Banerjee
, S.
, 1998
, “Turbulence Modification by Large-Scale Organized Electrohydrodynamic Flows
,” Phys. Fluids
, 10
(7
), pp. 1742
–1756
.198.
Moreau
, E.
, Léger
, L.
, and Touchard
, G.
, 2006
, “Effect of a DC Surface-Corona Discharge on a Flat Plate Boundary Layer for Air Flow Velocity up to 25 m/s
,” J. Electrost.
, 64
(3–4
), pp. 215
–225
.199.
Davidson
, J.
, and Shaughnessy
, E.
, 1986
, “Turbulence Generation by Electric Body Forces
,” Exp. Fluids
, 4
(1
), pp. 17
–26
.200.
Nelson
, D.
, Benhenni
, M.
, Eichwald
, O.
, and Yousfi
, M.
, 2003
, “Ion Swarm Data for Electrical Discharge Modeling in Air and Flue Gas Mixtures
,” J. Appl. Phys.
, 94
(1
), p. 96
.201.
Asano
, K.
, Ajima
, T.
, and Higashiyama
, Y.
, 1995
, “The Measurement of Ion Mobility by Using an Axisymmetric Ion-Flow Anemometer
,” 1995 IEEE Industry Applications Conference Thirtieth IAS Annual Meeting
, IAS’95
, Orlando, FL, Oct. 8–12, Vol. 2
, pp. 1206
–1210
.202.
Cross
, J.
, 1987
, Electrostatics: Principles, Problems and Applications
, Hilger
, Bristol, UK
.203.
Ryzko
, H.
, 1965
, “Drift Velocity of Electrons and Ions in Dry and Humid Air and in Water Vapour
,” Proc. Phys. Soc.
, 85
(6
), p. 1283
.204.
Kriegseis
, J.
, Schröter
, D.
, Grundmann
, S.
, and Tropea
, C.
, 2011
, “Online-Characterization of Dielectric Barrier Discharge Plasma Actuators for Optimized Efficiency of Aerodynamical Flow Control Applications
,” J. Phys.: Conf. Ser.
, 301
(1
), p. 012020
.205.
Kriegseis
, J.
, Schröter
, D.
, Duchmann
, A.
, Barckmann
, K.
, Grundmann
, S.
, and Tropea
, C.
, 2013
, “Closed-Loop Performance Control of DBD Plasma Actuators
,” AIAA J.
, 51
(4
), pp. 961
–967
.206.
Duchmann
, A.
, Simon
, B.
, Tropea
, C.
, and Grundmann
, S.
, 2014
, “Dielectric Barrier Discharge Plasma Actuators for In-Flight Transition Delay
,” AIAA J.
, 52
(2
), pp. 358
–367
.207.
Duchmann
, A.
, 2012
, “Boundary-Layer Stabilization With Dielectric Barrier Discharge Plasmas for Free-Flight Application
,” Ph.D. thesis
, TU Darmstadt, Darmstadt, Germany.208.
Benard
, N.
, and Moreau
, E.
, 2010
, “Capabilities of the Dielectric Barrier Discharge Plasma Actuator for Multi-Frequency Excitations
,” J. Phys. D: Appl. Phys.
, 43
(14
), p. 145201
.209.
Kotsonis
, M.
, and Veldhuis
, L.
, 2010
, “Experimental Study on Dielectric Barrier Discharge Actuators Operating in Pulse Mode
,” J. Appl. Phys.
, 108
(11
), p. 113304
.210.
Jukes
, T. N.
, and Choi
, K.-S.
, 2009
, “Flow Control Around a Circular Cylinder Using Pulsed Dielectric Barrier Discharge Surface Plasma
,” Phys. Fluids
, 21
(8
), p. 084103
.211.
Kurz
, A.
, Goldin
, N.
, King
, R.
, Tropea
, C.
, and Grundmann
, S.
, 2013
, “Hybrid Transition Control Approach for Plasma Actuators
,” Exp. Fluids
, 54
(11
), pp. 1
–4
.212.
Brutscher, J., 2014, “Minipuls 2.1,” GBS Elektronik GmbH, Großerkmannsdorf, Germany, http://www.gbs-elektronik.de/fileadmin/download/datasheets/minipuls2.1e.pdf
213.
Choi
, K.-S.
, Jukes
, T.
, and Whalley
, R.
, 2011
, “Turbulent Boundary-Layer Control With Plasma Actuators
,” Philos. Trans. R. Soc., A
, 369
(1940
), pp. 1443
–1458
.214.
Joussot
, R.
, Hong
, D.
, Weber-Rozenbaum
, R.
, and Leroy-Chesneau
, A.
, 2010
, “Modification of the Laminar-to-Turbulent Transition on a Flat Plate Using a DBD Plasma Actuator
,” AIAA
paper No. 2010-4708.215.
Joussot
, R.
, Weber
, R.
, Leroy
, A.
, and Hong
, D.
, 2013
, “Transition Control Using a Single Plasma Actuator
,” Int. J. Aerodyn.
, 3
(1
), pp. 26
–46
.216.
Magnier
, P.
, Boucinha
, V.
, Dong
, B.
, Weber
, R.
, Leroy-Chesneau
, A.
, and Hong
, D.
, 2009
, “Experimental Study of the Flow Induced by a Sinusoidal Dielectric Barrier Discharge Actuator and Its Effects on a Flat Plate Natural Boundary Layer
,” ASME J. Fluids Eng.
, 131
(1
), p. 011203
.217.
Schlichting
, H.
, 1968
, Boundary-Layer Theory
, McGraw-Hill
, New York
.218.
Szulga
, N.
, Vermeersch
, O.
, Forte
, M.
, and Casalis
, G.
, 2015
, “Experimental and Numerical Study of Boundary Layer Transition Control Over an Airfoil Using a DBD Plasma Actuator
,” Procedia IUTAM
, 14
, pp. 403
–412
.219.
Duchmann
, A.
, Grundmann
, S.
, and Tropea
, C.
, 2013
, “Delay of Natural Transition With Dielectric Barrier Discharges
,” Exp. Fluids
, 54
(3
), pp. 1
–12
.220.
Widmann
, A.
, Kurz
, A.
, Simon
, B.
, Grundmann
, S.
, and Tropea
, C.
, 2013
, “Characterization of the Interaction Between Tollmien–Schlichting Waves and a DBD Plasma Actuator Using Phase-Locked PIV
,” 10th International Symposium on Particle Image Velocimetry
—PIV13
, Delft, The Netherlands.221.
Duchmann
, A.
, Reeh
, A.
, Quadros
, R.
, Kriegseis
, J.
, and Tropea
, C.
, 2010
, “Linear Stability Analysis for Manipulated Boundary-Layer Flows Using Plasma Actuators
,” Seventh IUTAM Symposium on Laminar-Turbulent Transition
(IUTAM Bookseries), Vol. 18
, G. M. L.
Gladwell
, R.
Moreau
, P.
Schlatter
, and D. S.
Henningson
, eds., Springer, Dordrecht
, The Netherlands
, pp. 153
–158
.222.
Vieira
, D.
, Kriegseis
, J.
, Grundmann
, S.
, and Schäfer
, M.
, 2012
, “Numerical Simulation of Boundary Layer Stabilization Using Plasma Actuators
,” European Congress on Computational Methods in Applied Sciences and Engineering
, Vienna, Austria, pp. 4354
–4364
.223.
Duchmann
, A.
, Tropea
, C.
, and Grundmann
, S.
, 2013
, “Linear Stability Analysis of DBD Boundary-Layer Flow-Control Experiments and Simulations
,” Int. J. Flow Control
, 5
(2
), pp. 111
–120
.224.
Fransson
, J. H.
, and Alfredsson
, P.
, 2003
, “On the Disturbance Growth in an Asymptotic Suction Boundary Layer
,” J. Fluid Mech.
, 482
(5
), pp. 51
–90
.225.
Riherd
, M.
, and Roy
, S.
, 2013
, “Damping Tollmien–Schlichting Waves in a Boundary Layer Using Plasma Actuators
,” J. Phys. D: Appl. Phys.
, 46
(48
), p. 485203
.226.
Riherd
, M.
, Roy
, S.
, and Balachandar
, S.
, 2014
, “Local Stability Effects of Plasma Actuation on a Zero Pressure Gradient Boundary Layer
,” Theor. Comput. Fluid Dyn.
, 28
(1
), pp. 65
–87
.227.
Simon
, B.
, Schnabel
, P.
, and Grundmann
, S.
, 2015
, “IR Measurements for Quantification of Laminar Boundary Layer Stabilization With DBD Plasma Actuators
,” New Results in Numerical and Experimental Fluid Mechanics IX
, Springer
, Switzerland
.228.
Rizzetta
, D. P.
, and Visbal
, M. R.
, “Plasma-Based Control of Transition on a Wing With Leading-Edge Excrescence
,” AIAA J.
, 54
(1
), pp. 129
–140
.229.
Rizzetta
, D. P.
, and Visbal
, M. R.
, 2015
, “Delay of Finite-Span Excrescence-Induced Transition Using Plasma-Based Control
,” Int. J. Comput. Fluid Dyn.
, 29
(2
), pp. 161
–179
.230.
Rizzetta
, D. P.
, and Visbal
, M. R.
, 2015
, “Plasma-Based Flow Control for Delay of Excrescence-Generated Transition
,” AIAA J.
, 53
(6
), pp. 1455
–1467
.231.
Drake
, A.
, and Bender
, A.
, 2009
, “Surface Excrescence Transition Study Delivery Order 0053
,” DTIC Document, Technical Report No. 579
.232.
Riherd
, M.
, and Roy
, S.
, 2014
, “Stabilization of Boundary Layer Streaks by Plasma Actuators
,” J. Phys. D: Appl. Phys.
, 47
(12
), p. 125203
.233.
Fransson
, J. H.
, Talamelli
, A.
, Brandt
, L.
, and Cossu
, C.
, 2006
, “Delaying Transition to Turbulence by a Passive Mechanism
,” Phys. Rev. Lett.
, 96
(6
), p. 064501
.234.
Shahinfar
, S.
, Sattarzadeh
, S. S.
, and Fransson
, J. H.
, 2014
, “Passive Boundary Layer Control of Oblique Disturbances by Finite-Amplitude Streaks
,” J. Fluid Mech.
, 749
(6
), pp. 1
–36
.235.
Barckmann
, K.
, Tropea
, C.
, and Grundmann
, S.
, 2015
, “Attenuation of Tollmien–Schlichting Waves Using Plasma Actuator Vortex Generators
,” AIAA J.
, 53
(5
), pp. 1384
–1388
.236.
Barckmann
, K.
, 2014
, “Active Vortex Generation Using Dielectric Barrier Discharge Plasma Actuators in Laminar Boundary Layers
,” Ph.D. thesis
, TU Darmstadt, Darmstadt, Germany.237.
Jukes
, T. N.
, and Choi
, K.-S.
, 2012
, “Dielectric-Barrier-Discharge Vortex Generators: Characterisation and Optimisation for Flow Separation Control
,” Exp. Fluids
, 52
(2
), pp. 329
–345
.238.
Whalley
, R.
, and Choi
, K.-S.
, 2014
, “Turbulent Boundary-Layer Control With Plasma Spanwise Travelling Waves
,” Exp. Fluids
, 55
(8
), p. 1796
.239.
Saric
, W. S.
, Carpenter
, A. L.
, and Reed
, H. L.
, 2011
, “Passive Control of Transition in Three-Dimensional Boundary Layers, With Emphasis on Discrete Roughness Elements
,” Philos. Trans. R. Soc., A
, 369
(1940
), pp. 1352
–1364
.240.
Schuele
, C. Y.
, Corke
, T. C.
, and Matlis
, E.
, 2013
, “Control of Stationary Cross-Flow Modes in a Mach 3.5 Boundary Layer Using Patterned Passive and Active Roughness
,” J. Fluid Mech.
, 718
(3
), pp. 5
–38
.241.
Chernyshev
, S.
, Kuryachii
, A.
, Manuilovich
, S.
, Rusyanov
, D.
, and Skvortsov
, V.
, 2013
, “Attenuation of Cross-Flow-Type Instability in Compressible Boundary Layer by Means of Plasma Actuators
,” AIAA
Paper No. 2013-321.242.
Dörr
, P. C.
, and Kloker
, M. J.
, 2014
, “Transition Control in a Three-Dimensional Boundary-Layer Flow Using Plasma Actuators
,” Eighth IUTAM
Symposium on Laminar-Turbulent Transition
, Rio de Janeiro, Brazil, pp. 469–478.243.
Dörr
, P. C.
, and Kloker
, M. J.
, 2015
, “Stabilisation of a Three-Dimensional Boundary Layer by Base-Flow Manipulation Using Plasma Actuators
,” J. Phys. D: Appl. Phys.
, 48
(28
), p. 285205
.244.
Saric
, W. S.
, Reed
, H. L.
, and White
, E. B.
, 2003
, “Stability and Transition of Three-Dimensional Boundary Layers
,” Annu. Rev. Fluid Mech.
, 35
(1
), pp. 413
–440
.245.
Hanson
, R. E.
, Lavoie
, P.
, Naguib
, A. M.
, and Morrison
, J. F.
, 2010
, “Transient Growth Instability Cancelation by a Plasma Actuator Array
,” Exp. Fluids
, 49
(6
), pp. 1339
–1348
.246.
Belson
, B. A.
, Meidell
, K.
, Hanson
, R. E.
, Palmeiro
, D.
, Lavoie
, P.
, and Rowley
, C.
, 2012
, “Comparison of Plasma Actuators in Simulations and Experiments for Control of Bypass Transition
,” AIAA
Paper No. 2012-1141.247.
Hanson
, R. E.
, Bade
, K. M.
, Belson
, B. A.
, Lavoie
, P.
, Naguib
, A. M.
, and Rowley
, C. W.
, 2014
, “Feedback Control of Slowly-Varying Transient Growth by an Array of Plasma Actuators
,” Phys. Fluids (1994-Present)
, 26
(2
), p. 024102
.248.
Osmokrovic
, L. P.
, Hanson
, R. E.
, and Lavoie
, P.
, 2015
, “Laminar Boundary-Layer Response to Spanwise Periodic Forcing by Dielectric-Barrier-Discharge Plasma-Actuator Arrays
,” AIAA J.
, 53
(3
), pp. 617
–628
.249.
Thomas
, A. S.
, 1983
, “The Control of Boundary-Layer Transition Using a Wave-Superposition Principle
,” J. Fluid Mech.
, 137
(12
), pp. 233
–250
.250.
Bower
, W.
, Kegelman
, J.
, Pal
, A.
, and Meyer
, G.
, 1987
, “A Numerical Study of Two-Dimensional Instability-Wave Control Based on the ORR–Sommerfeld Equation
,” Phys. Fluids
, 30
(4
), pp. 998
–1004
.251.
Baumann
, M.
, 1999
, Aktive Dämpfung von Tollmien-Schlichting Wellen in einer Flügelgrenzschicht
(Fortschritt-Berichte), Vol. 7
, VDI
, Düsseldorf, Germany
.252.
Sturzebecher
, D.
, and Nitsche
, W.
, 2003
, “Active Cancellation of Tollmien–Schlichting Instabilities on a Wing Using Multi-Channel Sensor Actuator Systems
,” Int. J. Heat Fluid Flow
, 24
(4
), pp. 572
–583
.253.
Pätzold
, A.
, Peltzer
, I.
, Nitsche
, W.
, Goldin
, N.
, King
, R.
, Haller
, D.
, and Woias
, P.
, 2013
, “Active Transition Delay by Spatial Surface Actuation With Model Predictive Control
,” New Results in Numerical and Experimental Fluid Mechanics VIII
, Springer
, Berlin, Heidelberg
, pp. 261
–269
.254.
Wehrmann
, O.
, 1965
, “Tollmien–Schlichting Waves Under the Influence of a Flexible Wall
,” Phys. Fluids
, 8
(7
), p. 1389
.255.
Grundmann
, S.
, and Tropea
, C.
, 2007
, “Active Cancellation of Artificially Introduced Tollmien–Schlichting Waves Using Plasma Actuators
,” Exp. Fluids
, 44
(5), pp. 795
–806
.256.
Elliott
, S.
, 2000
, Signal Processing for Active Control
, Academic Press
, London
.257.
Fabbiane
, N.
, Semeraro
, O.
, Bagheri
, S.
, and Henningson
, D. S.
, 2014
, “Adaptive and Model-Based Control Theory Applied to Convectively Unstable Flows
,” ASME Appl. Mech. Rev.
, 66
(6
), p. 060801
.258.
Fabbiane
, N.
, Simon
, B.
, Fischer
, F.
, Grundmann
, S.
, Bagheri
, S.
, and Henningson
, D. S.
, 2015
, “On the Role of Adaptivity for Robust Laminar Flow Control
,” J. Fluid Mech.
, 767
(3
), p. R1.259.
Kurz
, A.
, Simon
, B.
, Tropea
, C.
, and Grundmann
, S.
, 2014
, “Active Wave Cancelation Using Plasma Actuators in Flight
,” AIAA
Paper No. 2014-1249.260.
Dadfar
, R.
, Semeraro
, O.
, Hanifi
, A.
, and Henningson
, D. S.
, 2013
, “Output Feedback Control of Blasius Flow With Leading Edge Using Plasma Actuator
,” AIAA J.
, 51
(9
), pp. 2192
–2207
.261.
Dadfar
, R.
, Hanifi
, A.
, and Henningson
, D. S.
, 2015
, “Feedback Control for Laminarization of Flow Over Wings
,” Flow, Turbul. Combust.
, 94
(1
), pp. 43
–62
.262.
Kotsonis
, M.
, Giepman
, R.
, Hulshoff
, S.
, and Veldhuis
, L.
, 2013
, “Numerical Study of the Control of Tollmien–Schlichting Waves Using Plasma Actuators
,” AIAA J.
, 51
(10
), pp. 2353
–2364
.263.
Simon
, B.
, Nemitz
, T.
, Rohlfing
, J.
, Fischer
, F.
, Mayer
, D.
, and Grundmann
, S.
, 2015
, “Active Flow Control of Laminar Boundary Layers for Variable Flow Conditions
,” Int. J. Heat Fluid Flow
, 56
(1
), pp. 344
–354
.264.
Semeraro
, O.
, Bagheri
, S.
, Brandt
, L.
, and Henningson
, D. S.
, 2011
, “Feedback Control of Three-Dimensional Optimal Disturbances Using Reduced-Order Models
,” J. Fluid Mech.
, 677
(6
), pp. 63
–102
.265.
Dadfar
, R.
, Fabbiane
, N.
, Bagheri
, S.
, and Henningson
, D. S.
, 2014
, “Centralised Versus Decentralised Active Control of Boundary Layer Instabilities
,” Flow, Turbul. Combust.
, 93
(4
), pp. 537
–553
.266.
Kurz
, A.
, Tropea
, C.
, Grundmann
, S.
, Forte
, M.
, Vermeersch
, O.
, Seraudie
, A.
, Arnal
, D.
, Goldin
, N.
, and King
, R.
, 2012
, “Transition Delay Using DBD Plasma Actuators in Direct Frequency Mode
,” AIAA
Paper No. 2012-2945.267.
Kurz
, A.
, Grundmann
, S.
, Tropea
, C.
, Forte
, M.
, Seraudie
, A.
, Vermeersch
, O.
, Arnal
, D.
, Goldin
, R.
, and King
, R.
, 2013
, “Boundary Layer Transition Control Using DBD Plasma Actuators
,” J. AerospaceLab
, 1
(6
), pp. 1
–8
.268.
Karniadakis
, G.
, and Choi
, K.-S.
, 2003
, “Mechanisms on Transverse Motions in Turbulent Wall Flows
,” Annu. Rev. Fluid Mech.
, 35
(1
), pp. 45
–62
.269.
Ricco
, P.
, and Wu
, S.
, 2004
, “On the Effects of Lateral Wall Oscillations on a Turbulent Boundary Layer
,” Exp. Therm. Fluid Sci.
, 29
(1
), pp. 41
–52
.270.
Quadrio
, M.
, 2011
, “Drag Reduction in Turbulent Boundary Layers by In-Plane Wall Motion
,” Philos. Trans. R. Soc. London A
, 369
(1940
), pp. 1428
–1442
.271.
Skote
, M.
, 2013
, “Comparison Between Spatial and Temporal Wall Oscillations in Turbulent Boundary Layer Flows
,” J. Fluid Mech.
, 730
(9
), pp. 273
–294
.272.
Choi
, K.-S.
, Jukes
, T. N.
, Whalley
, R. D.
, Feng
, L.
, Wang
, J.
, Matsunuma
, T.
, and Segawa
, T.
, 2014
, “Plasma Virtual Actuators for Flow Control
,” J. Flow Control, Meas. Visualization
, 3
(1
), p. 22
.273.
Li
, Z.
, Hu
, B.
, Lan
, S.
, Zhang
, J.
, and Huang
, J.
, 2015
, “Control of Turbulent Channel Flow Using a Plasma-Based Body Force
,” Comput. Fluids
, 119
(9
), pp. 26
–36
.274.
Gaitonde
, D. V.
, Visbal
, M. R.
, and Roy
, S.
, 2005
, “Control of Flow Past a Wing Section With Plasma-Based Body Forces
,” AIAA
Paper No. 2005-5302.275.
Wicks
, M.
, Thomas
, F. O.
, Corke
, T. C.
, Patel
, M.
, and Cain
, A. B.
, 2015
, “Mechanism of Vorticity Generation in Plasma Streamwise Vortex Generators
,” AIAA J.
, 53
(11
), pp. 3404
–3413
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