Abstract
It is known that surface non-thermal plasma actuators have proved their efficiency for aerodynamics flow control. In this study, a dielectric barrier discharge (DBD) is mounted on the diffuser of an axisymmetric turbulent air jet in order to control the flow separation along a 12-degree diffuser bevel. The momentum created by the actuator is applied to separate an air flow naturally attached to the diffuser for air flow velocity up to 40 m s−1. Laser sheet visualizations and LDV measurements are achieved to characterize the unforced and forced air jet. The flow separation, the induced velocity fluctuations, the jet mixing improvement and vectoring are investigated. The main results of this study demonstrate that DBD actuators are suitable to fully detach the air flow along the bevel for a velocity of 20 m s−1 and that a jet vectoring between 13.5° and 5.5° could be achieved for velocity ranging between 20 and 40 m s−1. Considerations about a potential improvement of the jet mixing are also introduced and the laser sheet visualization attests that induced flow perturbations are highly 3D.
Similar content being viewed by others
References
Artana G, Sosa R, Moreau E, Touchard G (2003) Control of the near-wake flow around a circular cylinder with electrohydrodynamic actuators. Exps Fluids 35:580–588
Ben Chiekh M, Bera JC, Sunyach M (2003) Synthetic jet control for flows in a diffuser: vectoring, spreading and mixing enhancement. J Turb 32:1–12
Boeuf JP, Lagmich Y, Unfer TH, Callegari TH, Pitchford LC (2007) Electrohydrodynamic force in dielectric barrier discharge plasma actuator. J Phys D: Appl Phys 40:652–662
Bohl D, Foss JF (1996) Enhancement of passive mixing tabs by the addition of secondary tabs. AIAA paper 96-054
Bridges J, Wernet M and Brown C (2003) Control of jet noise through mixing enhancement. NASA report, 212335
Cho SK, Yoo JY, Choi H (1998) Vortex pairing in an axisymmetric jet using two-frequency acoustic forcing at low to moderate strouhal numbers. Exps Fluids 25:305–315
Collin E, Breux JM, Rochas A, Sapin S (2005) Contrôle des jets par pilotage dynamique de décollement. Technical report of COS Project, LEA
Corke TC, Mertz B, Patel M (2006) Plasma flow control optimized airfoil. AIAA paper 2006-1208
Corke TC, Matlis E (2000) Phased plasma arrays for unsteady flow control. AIAA paper 2000-2323
Davis S, Glezer A (2000) The manipulation of large and small scales in coaxial jets using synthetic jet actuators. AIAA Paper 2000-0403
Denis S, Delville J, Garem JH, Bonnet JP (1999) Control of jet expansion by impeding jets. In: Proceeding of the GAMM, Metz, France
Enloe CL, McLaughlin TE, VanDyken RD, Kachner KD, Jumper EJ, Corke C (2004) Mechanisms and responses of a single dielectric barrier plasma actuator: Plasma morphology. AIAA J 42:589–594
Forte M, Baudoin F, Moreau E, Touchard G (2006a) Non-stationary measurements of the induced flow velocity for a single dielectric barrier discharge actuator—application to airflow control. In: Proceeding of ISEHD, Buenos Aires, Argentina
Forte M, Jolibois J, Moreau E, Touchard G, Cazalens M (2006b) Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity—application to airflow control. AIAA paper 2006-2863
Fridman A, Chirokov A, Gutsol A (2005) Non-thermal atmospheric pressure discharges. J Phys D: Appl Phys 38:R1–R24
Grundmann S, Klumpp S, Tropea C (2006) Stabilizing a laminar boundary-layer using plasma-actuators. 25th International Congress of the Aeronautical Sciences, Hamburg 2006, September 3–8
Hultgren LS, Ashpis DE (2003) Demonstration of separation delay with glow-discharge plasma actuators. AIAA paper 2003-1025
Jolibois J, Forte M, Moreau E (2006) Separation control along a NACA0015 airfoil using dielectric barrier discharge actuators. In: Proceeding of IUTAM, London, September 2006
Labergue A, Moreau E, Zouzou N, Touchard G (2007) Separation control using plasma actuators: application to a free turbulent jet. J Phys D: Appl Phys 40:674–684
McLaughlin TE, Felker B, Avery JC (2006) Further experiments in cylinder wake modification with dielectric barrier discharge forcing. AIAA paper 2006-1409
Leger L, Moreau E, Artana G, Touchard G (2001) Influence of a DC corona discharge on the airflow along an inclined flat plate. J Electrostatics 51:300–306
Moreau E, Leger L, Touchard G (2006) Effect of a DC surface non-thermal plasma on a flat plane boundary layer for airflow velocity up to 25 m s−1. J Electrostatics 64:215–225
Moreau E (2007) Airflow control by non-thermal plasma actuators. J Phys D: Appl Phys 40:605–636
Ng TT, Bradley TA (1988) Effect of multifrequency forcing on the near-field development of a jet. AIAA J 26:1201–1207
Pack LG, Seifert A (2001) Periodic excitation for jet vectoring and enhanced spreading. J Aircr 38:486–495
Papamoschou D (2004) New method for jet noise reduction in turbofan engines. AIAA J 42:2245–2253
Papamoschou D (2000) Mixing enhancement using axial flow. AIAA paper 2000-0093
Pons J, Moreau E, Touchard G (2005) Asymmetric surface barrier discharge in air at atmospheric pressure: electric properties and induced airflow characteristics. J Phys D: Appl Phys 38:3635–3642
Roth JR, Dai X (2006) Optimization of the aerodynamic plasma actuator as an EHD electrical device. AIAA paper 2006-1203
Roth JR, Sherman DM, Wilkinson SP (2000) Electrohydrodynamic flow control with a glow-discharge surface plasma. AIAA J 38:1166–1172
Schlichting H (1987) Boundary layer theory, 7th edn. McGraw Hill, New York
Smith BL, Glezer A (2002) Jet vectoring using synthetic jets. J Fluid Mech 458:1–34
Sosa R, Artana G, Moreau E, Touchard G (2007) Stall control at high angle of attack with plasma sheet actuators. Exps Fluids 42:143–167
Strykowski PJ, Krothapalli A, Forliti DJ (1996) Counterflow thrust vectoring of supersonic jets. AIAA J 34:2306–2314
Zaman KBMQ, Reeder MF, Saminy M (1994) Control of an axisymmetric jet using vortex generators. Phys Fluids 6:778–793
Acknowledgements
The authors thank AIRBUS for its financial and technical support (contract #D05028043), under the scientific direction of Dr. Stephen Rolston, and J.P. Bonnet and J. Delville (CEAT, Poitiers) for helping us in designing the diffuser geometry and for theirs advices. We also acknowledge J.C. Jouvanneau for the fabrication of the experimental diffusers and P. Braud for the technical assist.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
About this article
Cite this article
Benard, N., Jolibois, J., Forte, M. et al. Control of an axisymmetric subsonic air jet by plasma actuator. Exp Fluids 43, 603–616 (2007). https://doi.org/10.1007/s00348-007-0344-9
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s00348-007-0344-9