In-flight transition delay with DBD plasma actuators

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013

Volumn , Issue , 2013, Pages

  Duchmann, A ^a   Simon, B ^a   Magin, P ^a   Tropea, C ^a   Grundmann, S ^a  

^a DARMSTADT UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AEROSPACE ENGINEERING; BOUNDARY LAYERS; DATA ACQUISITION; DIELECTRIC DEVICES; DIELECTRIC MATERIALS; ELECTRIC DISCHARGES; ENERGY EFFICIENCY; FLOW CONTROL; FREE FLIGHT; LAMINAR FLOW;

ACTUATOR PERFORMANCE; BOUNDARY LAYER TRANSITIONS; CONTROL PERFORMANCE; DATA ACQUISITION HARDWARE; DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATORS; FLOW CONTROL DEVICES; HOT WIRE MEASUREMENTS; NATURAL LAMINAR FLOWS;

HUMIDITY CONTROL;

EID: 85087244782     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2013-900     Document Type: Conference Paper

References (23)

1. Moreau, E., "Airflow Control by Non-Thermal Plasma Actuators, " J. Phys. D: Appl. Phys., Vol. 40, 2007, pp. 605-636.
2. Sidorenko, A. A., Budovsky, A. D., Pushkarev, A. V., and Maslov, A. A., "Flight Testing of DBD Plasma Separation Control System, " 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2008, AIAA 2008-3731.
3. Grundmann, S. and Tropea, C., "Experimental Transition Delay Using Glow-Discharge Plasma Actuators, " Exp. Fluids, Vol. 42, No. 4, April 2007, pp. 653-657.
4. Séraudie, A., Vermeersch, O., and Arnal, D., "DBD Plasma actuator effect on a 2D model laminar boundary layer. Transition delay under ionic wind effect. " 29th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii, 2011, AIAA 2011-3515.
5. Quadros, R., Numerical Optimization of Boundary-Layer Control using Dielectric Barrier Discharge Plasma Actuator, Ph.D. thesis, TU Darmstadt, 2009.
6. Duchmann, A., Reeh, A., Quadros, R., Kriegseis, J., and Tropea, C., "Linear Stability Analysis for Manipulated Boundary-Layer Flows using Plasma Actuators, " Seventh IUTAM Symposium on Laminar-Turbulent Transition, edited by G. M. L. Gladwell, R. Moreau, P. Schlatter, and D. S. Henningson, Vol. 18 of IUTAM Bookseries, Springer Netherlands, 2010, pp. 153-158.
7. Riherd, M. and Roy, S., "Linear Stability Analysis of a Boundary Layer with Plasma Actuators, " 50th AIAA Aerospace Science Meeting and Exhibtion, 09-12 January, Nashville, Tennessee, 2012, AIAA 2012-0290.
8. Bénard, N., Balcon, N., and Moreau, E., "Electric Wind Produced by a Surface Dielectric Barrier Discharge Operating Over a Wide Range of Relative Humidity, " 47th AIAA Aerospace Sciences Meeting, Orlando, Florida, USA, 2009, AIAA 2009-488.
9. Versailles, P., Gingras-Gosselin, V., and Vo, H.-D., "Impact of Pressure and Temperature on the Performance of Plasma Actuators, " AIAA J., Vol. 48, No. 4, 2010, pp. 859-863.
10. Bénard, N., Balcon, N., and Moreau, E., "Electric Wind Produced by a Single Dielectric Barrier Discharge Actuator Operating in Atmospheric Flight Conditions-Pressure Outcome, " 39th Plasmadynamics and Lasers Conference, Seattle, Washington, USA, 2008, AIAA 2008-3792.
11. Bénard, N., Balcon, N., and Moreau, E., "Electric wind produced by a surface dielectric barrier discharge operating in air at different pressures: aeronautical control insights, " J. Phys. D: Appl. Phys., Vol. 41, No. 4, Feb 2008, pp. 042002 (5pp).
12. Nichols, T. and Rovey, J., "Fundamental Processes of DBD Plasma Actuators Operating at High Altitude, " 50th AIAA Aerospace Sciences Meeting, Nashville, Tennessee, USA, 2012, AIAA 2012-822.
13. Barckmann, K., Kriegseis, J., Grundmann, S., and Tropea, C., "Dielectric-Barrier Discharge Plasmas for Flow Control at Higher Mach Numbers, " 5th Flow Control Conference, Chicago, Illinois, USA, 2010, AIAA 2010-4258.
14. Weismüller, M., A new Approach to Aerodynamic Performance of Aircraft under Turbulent Atmospheric Conditions, Ph.D. thesis, TU Darmstadt, June 2011.
15. Gregory, J. W., Enloe, C. L., Font, G. I., and McLaughlin, T. E., "Force Production Mechanisms of a Dielectric-Barrier Discharge Plasma Actuator, " 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 2007, AIAA 2007-185.
16. Ashpis, D., Lobo, M., and Griebler, E., "Progress toward Accurate Measurements of Power Consumption of DBD Plasma Actuators, " 50th AIAA Aerospace Sciences Meeting, Nashville, Tennessee, USA, 2012, AIAA 2012-823.
17. Kriegseis, J., Performance Characterization and Quantification of Dielectric Barrier Discharge Plasma Actuators, Ph.D. thesis, TU Darmstadt, December 2011.
18. Abe, T., Takizawa, Y., and Sato, S., "Experimental Study for Momentum Transfer in a Dielectric Barrier Discharge Plasma Actuator, " AIAA J., Vol. 46, No. 9, 2008, pp. 2248-2256.
19. Bénard, N. and Moreau, E., "Effects of Altitude on the Electromechanical Characteristics of a Single Dielectric Barrier Discharge Plasma Actuator, " 41st Plasmadynamics and Lasers Conference, Chicago, Illinois, USA, Jun. 2010, AIAA 2010-4633.
20. Ziegler, J. G. and Nichols, N. B., "Optimum Settings for Automatic Controllers, " Trans. ASME, Vol. Vol. 64, No. 1, 1942, pp. 759-768.
21. Nitsche, W. and Brunn, A., Strömungsmesstechnik, Vol. 2, Springer Verlag, Berlin, 2006.
22. Arnal, D. and Archambaud, J., "Laminar-turbulent transition control: NLF, LFC, HLFC, " AVT-151 RTO AVT/VKI Lecture Series, Rhode St. Gense, Belgium (RTO-EN-AVT-151-15), 2008, pp. 9-13, ISBN 978-92-837-0900-6.
23. Moreau, E., Léger, L., and Touchard, G., "Effect of a DC surface-corona discharge on a flat plate boundary layer for air flow velocity up to 25 m/s, " J. Electrost., Vol. 64, No. 3-4, 2006, pp. 215-225.