journal article·2026-02-13Open access

DBD Plasma Actuators for Aerodynamic Flow Control: A Review

Mohammad Saemian, Miguel Cota, Lena Sabidussi, Zeinab Rida, Ahmad Nabhani, Josep M. Bergada

Applied Sciences· Volume 16· Issue 4

Abstract

Dielectric barrier discharge (DBD) plasma actuators (PAs) are devices used to control airflow. DBD actuators generate an electric field that accelerates ionized air particles, inducing localized flow modifications. Among other applications, they are particularly effective for enhancing cooling, for aerodynamic drag reduction, and for lift enhancement, therefore capable of improving stall characteristics. In addition, they offer several distinct advantages, such as rapid response time, low power consumption, and no moving parts. The present review paper aims to summarize the main governing equations associated with the most common phenomenological PA Computational Fluid Dynamics (CFD) models, Shyy and Suzen-Huang, as well as highlight the major applications to flat plates, wind turbine airfoils and entire wind turbines. The application of DBD plasma actuators on individual wind turbine blades, as well as dynamic horizontal and vertical axis wind turbines, is reviewed, drawing from key numerical and experimental investigations. The simulated performance of various configurations of single and multiple PAs on representative airfoils at different chordwise locations is discussed. The overall findings indicate that the chordwise location of the actuators on airfoils and their optimum spanwise placement on small and large wind turbine blades, along with the geometry and excitation parameters of the actuators, play a crucial role in their performance, affecting the boundary layer and the flow pattern. The reader shall obtain an overall idea of the most recent aerodynamic applications of PAs as well as their expected efficiency.
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Research context

OpenAlex topics: Plasma and Flow Control in Aerodynamics · Aerosol Filtration and Electrostatic Precipitation · Icing and De-icing Technologies

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Fluid Mechanics, Universitat Politècnica de Catalunya, Barcelona Tech-UPC, Jordi Girona 31, 08034 Barcelona, Spain

Research and Development Division, YPlasma Actuator Technologies Inc., Pau Vila 1, 08039 Barcelona, Spain

Funding

Spanish Ministerio de Ciencia, Innovacion y Universi- dades

References (100+)

Show source-provided references
1. Passive control of boundary layer flow separation on a wind turbine airfoil using vortex generators and slot10.1016/j.oceaneng.2023.115170 ↗
2. Research on the aerodynamic performance of the wind turbine blades with leading-edge protuberances10.1016/j.oceaneng.2023.114615 ↗
3. Numerical and experimental validation of vortex generator effect on power performance improvement in MW-class wind turbine blade10.1016/j.renene.2023.04.104 ↗
4. On lift enhancement and noise reduction in serrated gurney flap airfoil of wind turbines using proper orthogonal decomposition10.1016/j.oceaneng.2023.115706 ↗
5. Winglet design for vertical axis wind turbines based on a design of experiment and CFD approach10.1016/j.enconman.2019.05.055 ↗
6. Aerodynamic characteristic of wind turbine with the leading edge slat and Microtab
7. Numerical study on effect of boundary layer trips on aerodynamic performance of E216 airfoil
8. Aerodynamic performance enhancement of horizontal axis wind turbines by dimples on blades: Numerical investigation10.1016/j.energy.2020.117056 ↗
9. Pechlivanoglou, G. (2013). Passive and Active flow Control Solutions for Wind Turbine Blades. [Doctor Thesis, Technische Universität Berlin].
10. Actuators for active flow control10.1146/annurev-fluid-122109-160634 ↗
11. Comparison between synthetic jets and continuous jets for active flow control: Application on a NACA 0015 and a compressor stator cascade10.1016/j.ast.2015.03.004 ↗
12. Subedi, D.P., Joshi, U.M., and Wong, C.S. (2017). Dielectric barrier discharge (DBD) plasmas and their applications. Plasma Science and Technology for Emerging Economies: An AAAPT Experience, Springer.10.1007/978-981-10-4217-1_13 ↗
13. Recent developments in DBD plasma flow control10.1016/j.paerosci.2013.05.003 ↗
14. Dielectric barrier discharge plasma actuators for flow control10.1146/annurev-fluid-121108-145550 ↗
15. Optimization of dielectric barrier discharge plasma actuators for active aerodynamic flow control10.2514/1.41588 ↗
16. Boundary-layer instability on sharp cone at Mach 3.5 with controlled input10.2514/2.1744 ↗
17. Demonstration of separation control using dielectric barrier discharge plasma actuators10.2514/1.J056976 ↗
18. Multi-DBD plasma actuator for flow separation control around NACA 0012 and NACA 0015 airfoil models
19. Numerical investigation of plasma actuator effects on flow control over a three-dimensional airfoil with a sinusoidal leading edge10.1115/1.4053847 ↗
20. Active flow control actuators on wind turbines; comprehensive review10.1016/j.oceaneng.2025.121991 ↗
21. Wang, J., and Feng, L. (2019). Flow Control Techniques and Applications, Cambridge University Press.10.1017/9781316676448 ↗
22. Rodrigues, F., Abdollahzadehsangroudi, M., Nunes-Pereira, J., and Páscoa, J. (2022). Recent developments on dielectric barrier discharge (DBD) plasma actuators for icing mitigation. Actuators, 12.10.3390/act12010005 ↗
23. Advancements in flow control using plasma actuators: A comprehensive review10.1088/2631-8695/adabb3 ↗
24. Advances and opportunities in wind energy harvesting using plasma actuators: A review10.1093/ce/zkad085 ↗
25. Role of surface discharge dynamics in the generation of electrohydrodynamic force: Toward performance improvement of dielectric barrier discharge plasma actuators10.1088/1361-6463/adb3af ↗
26. SDBD plasma enhanced aerodynamics: Concepts, optimization and applications10.1016/j.paerosci.2007.06.001 ↗
27. Microdischarge behaviour in the silent discharge of nitrogen-oxygen and water-air mixtures10.1088/0022-3727/30/5/015 ↗
28. Characterization of discharge modes of plasma actuators10.2514/1.37514 ↗
29. Dielectric barrier discharges: Progress on plasma sources and on the understanding of regimes and single filaments10.1088/1361-6595/aa6426 ↗
30. Advancements and challenges of high-speed active flow control: Plasma actuators10.1016/j.ijheatmasstransfer.2025.127481 ↗
31. Separation control with nanosecond-pulse-driven dielectric barrier discharge plasma actuators10.2514/1.J051114 ↗
32. Little, J., Takashima, K., Nishihara, M., Adamovich, I., and Samimy, M. (July, January 28). High lift airfoil leading edge separation control with nanosecond pulse DBD plasma actuators. Proceedings of the 5th Flow Control Conference, Chicago, IL, USA.
33. Experiments on the stability of supersonic laminar boundary layers10.1017/S0022112090003111 ↗
34. Cavalieri, D.A. (1995). On the Experimental Design for Instability Analysis on a Cone at Mach 3.5 and 6.0 Using a Corona Discharge Perturbation Method. [Ph.D. Thesis, Illinois Institute of Technology].
35. Corke, T., Cavalieri, D., Corke, T., and Cavalieri, D. (July, January 29). Controlled experiments on instabilities and transition to turbulence in supersonic boundary layers. Proceedings of the 28th Fluid Dynamics Conference, Snowmass Village, CO, USA.
36. A mathematical model of the modified Paschen’s curve for breakdown in microscale gaps10.1063/1.3380855 ↗
37. Modeling of dielectric barrier discharge-induced fluid dynamics and heat transfer10.1016/j.paerosci.2007.10.004 ↗
38. Modeling of glow discharge-induced fluid dynamics10.1063/1.1515103 ↗
39. Suzen, Y., and Huang, G. (2006, January 9–12). Simulations of flow separation control using plasma actuators. Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.10.2514/6.2006-877 ↗
40. Suzen, Y., Huang, G., Jacob, J., and Ashpis, D. (2005, January 6–9). Numerical simulations of plasma based flow control applications. Proceedings of the 35th AIAA Fluid Dynamics Conference and Exhibit, Ontario, ON, Canada.10.2514/6.2005-4633 ↗
41. Orlov, D.M. (2006). Modelling and Simulation of Single Dielectric Barrier Discharge Plasma Actuators. [Ph.D. Thesis, University of Notre Dame].
42. Numerical simulation of nanosecond-pulse electrical discharges10.1088/0963-0252/22/1/015001 ↗
43. Periodic electrodynamic field of dielectric barrier discharge10.2514/1.J050463 ↗
44. Boundary layer control with atmospheric plasma discharges10.2514/1.18542 ↗
45. Font, G., and Morgan, W. (2005, January 6–9). Plasma discharges in atmospheric pressure oxygen for boundary layer separation control. Proceedings of the 35th AIAA Fluid Dynamics Conference and Exhibit, Ontario, ON, Canada.10.2514/6.2005-4632 ↗
46. Monte Carlo simulation of gas flows10.1146/annurev.fl.10.010178.000303 ↗
47. Transition between different regimes of rf glow discharges10.1103/PhysRevA.41.4447 ↗
48. Particle simulations of radio-frequency glow discharges10.1109/27.106808 ↗
49. Two-dimensional, hybrid model of low-pressure glow discharges10.1103/PhysRevE.49.5607 ↗
50. Grundmann, S., Klumpp, S., and Tropea, C. (2007). Experimental and numerical investigations of boundary-layer influence using plasma-actuators. Proceedings of the Active Flow Control: Papers contributed to the Conference “Active Flow Control 2006”, Berlin, Germany, 27–29 September 2006, Springer.
51. Semiempirical thrust model of dielectric barrier plasma actuator for flow control10.1061/(ASCE)AS.1943-5525.0000353 ↗
52. Suzen, Y., Huang, G., and Ashpis, D. (2007, January 8–11). Numerical simulations of flow separation control in low-pressure turbines using plasma actuators. Proceedings of the 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.10.2514/6.2007-937 ↗
53. Orlov, D., Corke, T., and Patel, M. (2006, January 9–12). Electric circuit model for aerodynamic plasma actuator. Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.10.2514/6.2006-1206 ↗
54. Improving the performance of a numerical model to simulate the EHD interaction effect induced by dielectric barrier discharge10.1016/j.ijheatfluidflow.2017.07.008 ↗
55. Mechanisms and responses of a single dielectric barrier plasma actuator: Plasma morphology10.2514/1.2305 ↗
56. Roth, J. (1998, January 1–4). Electrohydrodynamically induced airflow in a one atmosphere uniform glow discharge surface plasma. Proceedings of the 25th Anniversary, IEEE Conference Record-Abstracts, 1998 IEEE International Conference on Plasma Science (Cat. No. 98CH36221), Raleigh, NC, USA.
57. Stability and transition of a supersonic laminar boundary layer on an insulated flat plate10.1017/S0022112060001092 ↗
58. Wind tunnel experiments relating to supersonic and hypersonic boundary-layer transition10.2514/3.49694 ↗
59. Shock tunnel investigation of boundary-layer transition at M = 5.510.2514/3.4098 ↗
60. Stetson, K., Thompson, E., Donaldson, J., and Siler, L. (1989, January 12–14). Laminar boundary layer stability experiments on a cone at Mach 8. V-Tests with a cooled model. Proceedings of the 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference, Buffalo, NY, USA.10.2514/6.1989-1895 ↗
61. Stetson, K., Thompson, E., Donaldson, J., and Siler, L. (1986, January 12–14). Laminar boundary layer stability experiments on a cone at Mach 8. IV-On unit Reynolds number and environmental effects. Proceedings of the 4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference, Atlanta, GA, USA.10.2514/6.1986-1087 ↗
62. Skramstad, H. (1943). Laminar-Boundary-Layer Oscillations and Transition on a Flat Plate, National Advisory Committee for Aeronautics. Technical Report.
63. Resonant growth of three-dimensional modes in trnsitioning Blasius boundary layers10.1017/S0022112089003058 ↗
64. Dielectric-barrier discharges. Principle and applications
65. Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a one atmosphere uniform glow discharge plasma10.1063/1.1564823 ↗
66. Roth, J., Sherman, D., and Wilkinson, S. (1998, January 12–15). Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma. Proceedings of the 36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.10.2514/6.1998-328 ↗
67. Corke, T., Jumper, E., Post, M., Orlov, D., and McLaughlin, T. (2002, January 14–17). Application of weakly-ionized plasmas as wing flow-control devices. Proceedings of the 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, USA.10.2514/6.2002-350 ↗
68. Modeling of fluid dynamics and heat transfer induced by dielectric barrier plasma actuator10.1115/1.2709659 ↗
69. Enloe, C., McLaughlin, T., Van Dyken, R., and Fischer, J. (2004, January 5–8). Plasma structure in the aerodynamic plasma actuator. Proceedings of the 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.10.2514/6.2004-844 ↗
70. Separation control using plasma actuators: Dynamic stall vortex control on oscillating airfoil10.2514/1.22716 ↗
71. Thompson, R., and Moeller, T. (2010, January 9–12). Numerical investigations of plasma actuator lorentz body forces. Proceedings of the 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, TN, USA.
72. Forte, M., Jolibois, J., Moreau, E., Touchard, G., and Cazalens, M. (2006, January 5–8). Optimization of a Dielectric Barrier Discharge Actuator by Stattionary and Non-stationary Measurements of the Induced Flow Velocity-Application to Airflow Control. Proceedings of the 3rd AIAA Flow Control Conference, San Francisco, CA, USA.10.2514/6.2006-2863 ↗
73. Seraudie, A., Aubert, E., Naudé, N., and Cambronne, J. (2006, January 5–8). Effect of plasma actuators on a flat plate laminar boundary layer in subsonic conditions. Proceedings of the 3rd AIAA Flow Control Conference, San Francisco, CA, USA.10.2514/6.2006-3350 ↗
74. Investigation of the DBD plasma effect on flat plate flow10.1088/1009-0630/16/3/05 ↗
75. Numerical study of the flow structures in flat plate and the wall-mounted hump induced by the unsteady DBD plasma10.1088/1009-0630/19/1/015502 ↗
76. Aerodynamic noise reduction by plasma actuators for a flat plate with blunt trailing edge10.1016/j.jsv.2018.08.029 ↗
77. Control of vortex shedding from a blunt trailing edge using plasma actuators10.1016/j.expthermflusci.2012.12.012 ↗
78. Noise control of blunt flat-plate using slit and dielectric barrier discharge Plasma10.2514/1.J063259 ↗
79. Flat plate drag reduction using plasma-generated streamwise vortices10.1017/jfm.2021.311 ↗
80. Wei, X., and Zhou, Y. (2024, January 25–28). Scaling of drag reduction in a turbulent boundary layer based on plasma-generated streamwise vortices. Proceedings of the 13th International Symposium on Turbulence Shear Flow Phenomena (TSFP13), Montréal, QC, Canada.
81. A sliding discharge device for producing cylindrical shock waves10.1088/0022-3727/20/3/019 ↗
82. Nanosecond pulsed sliding dielectric barrier discharge plasma actuator for airflow control: Electrical, optical, and mechanical characteristics10.1063/1.4927844 ↗
83. Chen, F.F. (1984). Introduction to Plasma Physics and Controlled Fusion, Springer.10.1007/978-1-4757-5595-4 ↗
84. Electric wind produced by surface plasma actuators: A new dielectric barrier discharge based on a three-electrode geometry10.1088/0022-3727/41/11/115204 ↗
85. Lin, N., Reed, H.L., and Saric, W. (1992). Effect of leading-edge geometry on boundary-layer receptivity to freestream sound. Instability, Transition, and Turbulence, Springer.10.1007/978-1-4612-2956-8_42 ↗
86. Experimental investigation of the dynamic characteristics of the flow generated by a sliding dielectric barrier discharge in the flat plate boundary layer flow10.1063/5.0134835 ↗
87. Experimental investigation of influence of sliding discharge DBD plasma on low-speed boundary layer10.1063/1.5134848 ↗
88. Sliding discharge in air at atmospheric pressure: Electrical properties10.1016/j.elstat.2005.03.026 ↗
89. Electric wind induced by sliding discharge in air at atmospheric pressure10.1016/j.elstat.2007.08.011 ↗
90. Improving performance of a sliding dielectric barrier discharge actuator using multiple potentials10.2514/1.J055108 ↗
91. Unsteady vortex structure induced by a trielectrode sliding discharge plasma actuator10.2514/1.J057596 ↗
92. Experimental investigation on the characteristics of sliding discharge plasma aerodynamic actuation10.1088/1009-0630/13/5/19 ↗
93. Elongating the area of plasma/fluid interaction of surface nanosecond pulsed discharges10.1016/j.elstat.2014.12.004 ↗
94. The structure of turbulent boundary layers10.1017/S0022112067001740 ↗
95. Active and passive turbulent boundary-layer drag reduction10.2514/1.J056949 ↗
96. Wilkinson, S.P. (2003, January 6–9). Investigation of an oscillating surface plasma for turbulent drag reduction. Proceedings of the 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. number AIAA Paper 2003-1023.10.2514/6.2003-1023 ↗
97. McGowan, R., Corke, T.C., Matlis, E.H., Kaszeta, R., and Gold, C. (2016, January 4–8). Pulsed-DC plasma actuator characteristics and application in compressor stall control. Proceedings of the 54th AIAA Aerospace Sciences Meeting, San Diego, CA, USA.10.2514/6.2016-0394 ↗
98. Duong, A., Midya, S., Corke, T., Hussain, F., and Thomas, F. (August, January 30). Turbulent boundary layer drag reduction using pulsed-dc plasma actuation. Proceedings of the 11th International Symposium on Turbulence and Shear Flow Phenomena (TSFP11), Southampton, UK.
99. Turbulent drag reduction using pulsed-DC plasma actuation10.1088/1361-6463/ab3388 ↗
100. Characteristics of drag-reduced turbulent boundary layers with pulsed-direct-current plasma actuation10.1017/jfm.2021.167 ↗