| Citation: | TIAN Yongqiang, CAI Jinsheng, YANG Leilei. Experimental on the thermal effects of pulsed dielectric barrier discharge plasma[J]. Journal of Aerospace Power, 2019, 34(12): 2663-2676. doi: 10.13224/j.cnki.jasp.2019.12.016
|
| [1] |
STARIKOVSKIY A,ALEKSANDROV N.Nonequilibrium plasma aerodynamics［M］∥MULDER M.Aeronautics and Astronautics.Rijeka:In Tech,2011:55-96.
|
| [2] |
ROTH J R.Boundary layer flow control with one atmosphere uniform glow discharge surface plasma［R］.AIAA 98-0328,1998.
|
| [3] |
CORKE T C,ENLOE C L,WILKINSON S P.Dielectric barrier discharge plasma actuators for flow control［J］.Annual Review of Fluid Mechanics,2010,42(1):505-529.
|
| [4] |
SERPIERI J,KOTSONIS M.Conditioning of unsteady cross-flow instability modes using dielectric barrier discharge plasma actuators［J］.Experimental Thermal and Fluid Science,2018(93):305-313.
|
| [5] |
邵涛,严萍.大气压气体放电及其等离子体应用［M］.北京:科学出版社,2015.
|
| [6] |
YANG L,LI J,CAI J,et al.Lift Augmentation based on flap deflection with dielectric barrier discharge plasma flow control over multi-element airfoils［J］.Journal of Fluids Engineering,2016,138(3):365-372.
|
| [7] |
LIU F,LUO S,GAO C,et al.Flow control over a conical forebody using duty-cycled plasma actuators［J］.AIAA Journal,2012,46(11):2969-2973.
|
| [8] |
NISHIHARA M,TAKASHIMA K,RICH J,et al.Mach 5 bow shock control by a nanosecond pulse surface DBD［R］.AIAA 2011-1144,2011.
|
| [9] |
KOZLOV A V,THOMAS F O.Active noise control of bluff-body flows using dielectric barrier discharge plasma actuators［J］.AIAA Journal,2000,46(8):1921-1931.
|
| [10] |
ONO R,OGURA K,MOGI T.Stabilization of premixed lean methane-air combustion using dielectric barrier discharge with low pollutant emissions［J］.Journal of Physics D:Applied Physics,2017(50):365201.1-365201.7.
|
| [11] |
USTINOV M,KOGAN M,LITVINOV V,et al.Natural laminar-turbulent transition delay by dielectric barrier discharge［J］.Journal of Physics:Conference Series,2011(318):022037.1-022037.9.
|
| [12] |
MENG X,CAI J,TIAN Y,et al.Experimental study of anti-icing and deicing on a cylinder by DBD plasma actuation［R］.AIAA 2016-4019,2016.
|
| [13] |
VAN DEN BROECKE J.De-icing using NS-DBD plasma actuators-efficiency and deicing capability of nanosecond pulsed dielectric barrier discharge plasma actuators［D］.Delft:Delft University of Technology,2016.
|
| [14] |
ZHOU W,LIU Y,HU H,et al.Utilization of thermal effect induced by plasma generation for aircraft icing mitigation［J］.AIAA Journal,2018,56(3):1-8.
|
| [15] |
CAI J,TIAN Y,MENG X,et al.An experimental study of icing control using DBD plasma actuator［J］.Experiments in Fluids,2017,58(8):102.1-102.8.
|
| [16] |
TIAN Y,ZHANG Z,CAI J,et al.Experimental study of an anti-icing method over an airfoil based on pulsed dielectric barrier discharge plasma［J］.Chinese Journal of Aeronautics,2018,31(7):1449-1460.
|
| [17] |
JOUSSOT R,HONG D,RABAT H,et al.Thermal characterization of a DBD plasma actuator:dielectirc temperature measurements using infrared thermography［R］.AIAA 2010-5102,2010.
|
| [18] |
STANFIELD S A,MENART J,DEJUSEOH C Jr,et al.Rotational and vibrational temperatures for a dielectric barrier discharge in air usuing emission spectroscopy［J］.AIAA Journal,2009,47(5):1107-1115.
|
| [19] |
DONG B,BAUCHIRE J M,POUVESLE J M,et al.Experimental study of a DBD surface discharge for the active flow control of subsonic airflow［J］.Journal of Physics:D Applied Physics,2008,41(15):1525-1528.
|
| [20] |
ERFANI R,ZARE-BEHTASH H,KONTIS K,et al.Plasma actuators:influence of dielectric surface temperature［J］.Experimental Thermal and Fluid Science,2012,42(5):258-264.
|
| [21] |
RODRIGUES F,PASCOA J,TRANCOSSI M.Heat generation mechanisms of DBD plasma actuators［J］.Experimental Thermal and Fluid Science,2018(90):55-65.
|
| [22] |
武占成,张希军,胡有志.气体放电［M］.北京:国防工业出版社,2012.
|
| [23] |
杨世铭,陶文铨.传热学［M］.北京:高等教育出版社,2006.
|
| [24] |
ROTH J R,DAI X.Optimization of the aerodynamic plasma actuator as an electrohydrodynamic (EHD) electrical device［R］.AIAA 2006-1203,2006.
|
| [25] |
JOLIBOIS J,FORTE M,MOREAU .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］.Journal of Electrostatics,2009,66(9):496-503.
|
| [26] |
MURPHY J P,KRIEGSEIS J,LAVOIE P.Scaling of maximum velocity,body force,and power consumption of dielectric barrier discharge plasma actuators via particle image velocimetry［J］.Journal of Applied Physics,2013,113(24):247-272.
|
| [27] |
ENLOE C L,MCLAUGHLIN T E,DYKEN R D V,et al.Mechanisms and responses of a single dielectric barrier plasma actuator:plasma morphology［J］.AIAA Journal,2004,42(3):589-594.
|
| [28] |
LITTLE J,NISHIHARA M,ADAMOVICH I,et al.High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator［J］.Experiments in Fluids,2010,48(3):521-537.
|
| [29] |
ORLOV D M,CORKE T C.Numerical simulation of aerodynamic plasma actuator effects［R］.AIAA 2005-1083,2005.
|
| [30] |
ABE T,TAKIZAWA Y,SATO S,et al.A parametric experimental study for momentum transfer by plasma actuator［R］.AIAA 2007-187,2007.
|
| [31] |
BAUGHN J W,PORTER C O,PETERSON B L,et al.Momentum transfer for an aerodynamic plasma actuator with an imposed boundary layer［R］.AIAA 2006-168,2006.
|
| [32] |
PORTER C,BAUGHN J,MCLAUGHLIN T,et al.Plasma actuator force measurements［J］.AIAA Journal,2007,45(7):1562-1570.
|
DownLoad: