[1] Moreau E. Airflow control by non-thermal plasma actuators[J]. Journal of Physics D: Applied Physics, 2007, 40(3): 605-636.[2] Wang J J, Choi K S, Feng L H, et al. Recent development in DBD plasma flow control[J]. Progress in Aerospace Sciences, 2013, 62: 52-78.[3] Nie W S, Cheng Y F, Che X K. A review on dielectric barrier discharge plasma flow control[J].Advances in Mechanics, 2012, 42(6): 722-734 (in Chinese). 聂万胜, 程钰锋, 车学科. 介质阻挡放电等离子体流动控制研究进展[J]. 力学进展, 2012, 42(6): 722-734.[4] Gregory J W, Enloe C L, Font G I, et al. Force production mechanisms of a dielectric-barrier discharge plasma actuator, AIAA-2007-0185[R]. Reston: AIAA, 2007.[5] Benard N, Balcon N, Moreau E. Electric wind produced by a surface dielectric barrier discharge operating in air at different pressures: aeronautical control insights[J]. Journal of Physics D: Applied of Physics, 2008, 41(4): 042002.[6] Benard N, Moreau E. Effects of altitude on the electromechanical characteristics of dielectric barrier discharge plasma actuators, AIAA-2010-4633[R]. Reston: AIAA, 2010.[7] Bottelberghe K, Mahmud Z. Low-pressure effects on a single DBD plasma actuator, AIAA-2010-0550[R]. Reston: AIAA, 2010.[8] Versailles P, Gosselin V G, Vo H D. Impact of pressure and temperature on the performance of plasma actuators [J]. AIAA Journal, 2010, 48(4): 859-863.[9] Abe T, Takizawa Y, Sato S, et al. Experimental study for momentum transfer in a dielectric barrier discharge plasma actuator[J]. AIAA Journal, 2008, 46(9): 2248-2256.[10] Valerioti J A, Corke T C. Pressure dependence of dielectric barrier discharge plasma flow actuators[J]. AIAA Journal, 2012, 50(7): 1490-1502.[11] Wu Y, Li Y H, Jia M, et al. Influence of operating pressure on surface dielectric barrier discharge plasma aerodynamic actuation characteristics[J]. Applied Physics Letters, 2008, 93(3): 031503.[12] Rethmel C, Little J, Takashima K, et al. Flow separation control over an airfoil with nanosecond pulse driven DBD plasma actuators, AIAA-2011-0487[R]. Reston: AIAA, 2011.[13] Taleghani A S, Shadaram A, Mirzaei M. Effects of duty cycles of the plasma actuators on improvement of pressure distribution above a NLF0414 airfoil[J]. IEEE Transactions on Plasma Science, 2012, 40(5): 1434-1440.[14] Chen Q, Meng X S, Wang Y S, et al. Comparison of pressures driven by nanosencond pulse to AC results, AIAA-2014-0094[R]. Reston: AIAA, 2014.[15] Wang W B, Zhang R P, Huang Z B, et al. Test research of two-element airfoil lift enhancement by plasma actuator [J]. Acta Aerodynamica Sinica, 2013, 31(1): 64-68 (in Chinese). 王万波, 章荣平, 黄宗波, 等. 等离子体激励用于两段翼型增升的试验研究[J]. 空气动力学学报, 2013, 31(1): 64-68.[16] Du H, Shi Z W, Ni F Y, et al. Aerodynamic moment control of flying wing vehicle using plasma actuators[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(9): 2038-2046 (in Chinese). 杜海, 史志伟, 倪芳原, 等. 基于等离子体激励的飞翼布局飞行器气动力矩控制[J]. 航空学报, 2013, 34(9): 2038-2046.[17] Liang H, Li Y H, Song H M, et al. Experimental investigation on airfoil stall separation suppression by multiphase plasma aerodynamic actuation[J]. Journal of Aerospace Power, 2011, 26(4): 867-873 (in Chinese). 梁华, 李应红, 宋慧敏, 等. 多相等离子体气动激励抑制翼型失速分离的试验[J].航空动力学报, 2011, 26(4): 867-873.[18] Zhang P F, Wang J J, Shi W Y, et al. Experimental study on the separation control by plasma actuator in subsonic flow[J]. Journal of Experiments in Fluid Mechanics, 2007, 21(2): 35-39 (in Chinese). 张攀峰, 王晋军, 施威毅, 等. 等离子体激励低速分离流动控制实验研究[J]. 实验流体力学, 2007, 21(2): 35-39.[19] Ren S G. Experimental aerodynamics[M]. Beijing: China Astronautic Publishing House, 1996 (in Chinese). 任思根. 实验空气动力学[M]. 北京: 中国宇航出版社, 1996.[20] 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): 243301.[21] Pavón S, Ott P, Leyland P, et al. Effects of a surface dielectric barrier discharge on transonic flows around an airfoil, AIAA-2009-0649[R]. Reston: AIAA, 2009.[22] Benard N, Balcon N, Moreau E. Electric wind produced by a surface dielectric barrier discharge operating over a wide range of relative humidity, AIAA-2009-0488[R]. Reston: AIAA, 2009.[23] Benard N, Balcon N, Moreau E. Electric wind produced by a single dielectric barrier discharge actuator operating in atmospheric flight conditions-pressure outcome, AIAA-2008-3792[R]. Reston: AIAA, 2008.[24] Font G I, Enloe C L, Newcomb J Y, et al. Effects of oxygen content on dielectric barrier discharge plasma actuator behavior[J]. AIAA Journal, 2011, 49(7): 1366-1373.[25] Shao T, Zhang D D, Yu Y, et al. A compact repetitive unipolar nanosecond-pulse generator for dielectric barrier discharge application[J]. IEEE Transactions on Plasma Science, 2010, 38(7): 1651-1655. |