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Control of an axisymmetric subsonic air jet by plasma actuator

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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.

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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

    Article  Google Scholar 

  • 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

    Article  Google Scholar 

  • 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

    Article  Google Scholar 

  • 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

    Article  Google Scholar 

  • 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

    Google Scholar 

  • 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

    Article  Google Scholar 

  • 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

    Article  Google Scholar 

  • 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

    Article  Google Scholar 

  • 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

    Article  Google Scholar 

  • Moreau E (2007) Airflow control by non-thermal plasma actuators. J Phys D: Appl Phys 40:605–636

    Article  Google Scholar 

  • Ng TT, Bradley TA (1988) Effect of multifrequency forcing on the near-field development of a jet. AIAA J 26:1201–1207

    Google Scholar 

  • Pack LG, Seifert A (2001) Periodic excitation for jet vectoring and enhanced spreading. J Aircr 38:486–495

    Article  Google Scholar 

  • Papamoschou D (2004) New method for jet noise reduction in turbofan engines. AIAA J 42:2245–2253

    Google Scholar 

  • 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

    Article  Google Scholar 

  • 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

    Article  Google Scholar 

  • Schlichting H (1987) Boundary layer theory, 7th edn. McGraw Hill, New York

    Google Scholar 

  • Smith BL, Glezer A (2002) Jet vectoring using synthetic jets. J Fluid Mech 458:1–34

    Article  MATH  Google Scholar 

  • 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

    Article  Google Scholar 

  • Strykowski PJ, Krothapalli A, Forliti DJ (1996) Counterflow thrust vectoring of supersonic jets. AIAA J 34:2306–2314

    Google Scholar 

  • Zaman KBMQ, Reeder MF, Saminy M (1994) Control of an axisymmetric jet using vortex generators. Phys Fluids 6:778–793

    Article  Google Scholar 

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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.

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Correspondence to N. Benard.

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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

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  • DOI: https://doi.org/10.1007/s00348-007-0344-9

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