[1] |
李应红, 吴云, 梁华等. 等离子体激励气动力学探索与展望. 力学进展, 2022, 52(1): 1-32 (Li Yinghong, Wu Yun, Liang Hua, et al. Exploration and outlook of plasma-actuated gas dynamics. Advances in Mechanics, 2022, 52(1): 1-32 (in Chinese) doi: 10.6052/1000-0992-21-044
|
[2] |
Grossman K, Bohdan C, Vanwie D. Sparkjet actuators for flow control//41st Aerospace Sciences Meeting and Exhibit, 2003
|
[3] |
Zhang Z, Wu Y, Jia M, et al. Influence of the discharge location on the performance of a three-electrode plasma synthetic jet actuator. Sensors and Actuators A: Physical, 2015, 235: 71-79
|
[4] |
Zong HH, Wu Y, Jia M, et al. Influence of geometrical parameters on performance of plasma synthetic jet actuator. Journal of Physics D: Applied Physics, 2016, 49(2): 025504
|
[5] |
Dong H, Geng X, Shi Z, et al. On evolution of flow structures induced by nanosecond pulse discharge inside a plasma synthetic jet actuator. Japanese Journal of Applied Physics, 2019, 58(2): 028002
|
[6] |
Zong H, Kotsonis M. Characterisation of plasma synthetic jet actuators in quiescent flow. Journal of Physics D: Applied Physics, 2016, 49(33): 335202
|
[7] |
Zong H, Kotsonis M. Effect of slotted exit orifice on performance of plasma synthetic jet actuator. Experiments in Fluids, 2017, 58(3): 17
|
[8] |
Zong H, Kotsonis M. Formation, evolution and scaling of plasma synthetic jets. Journal of Fluid Mechanics, 2017, 837: 147-181
|
[9] |
Wang L, Xia ZX, Luo ZB, et al. Three-electrode plasma synthetic jet actuator for high-speed flow control. AIAA Journal, 2014, 52(4): 879-882
|
[10] |
Sarah J Haack TT, Jerry E, et al. Development of an analytical sparkjet model//5th Flow Control Conference, 2010.
|
[11] |
Zong HH, Wu Y, Li YH, et al. Analytic model and frequency characteristics of plasma synthetic jet actuator. Physics of Fluids, 2015, 27(2): 027105
|
[12] |
Ibrahim IH, Skote M. Simulating plasma actuators in a channel flow configuration by utilizing the modified Suzen–Huang model. Computers & Fluids, 2014, 99: 144-155
|
[13] |
Mengxiao T, Yun W, Hongyu W, et al. Characterization of transverse plasma jet and its effects on ramp induced separation. Experimental Thermal and Fluid Science, 2018, 99: 584-594
|
[14] |
Zong H, Kotsonis M. Experimental investigation on frequency characteristics of plasma synthetic jets. Physics of Fluids, 2017, 29(11): 115107
|
[15] |
Geng X, Zhang W, Shi Z, et al. Experimental study on frequency characteristics of the actuations produced by plasma synthetic jet actuator and its geometric effects. Physics of Fluids, 2021, 33(6): 067113
|
[16] |
李铮, 徐聪, 张健等. 等离子体合成射流激励器高速流场逆向喷流控制研究. 航空学报, 2022, 43(S2): 727789-9 (Li Zheng, Xu Cong, Zhang Jian, et al. Study on reverse jet flow control by plasma synthetic jet actuator in high speed flow field. Acta Aeronautica et Astronautica Sinica, 2022, 43(S2): 727789-9 (in Chinese)
|
[17] |
马正雪, 罗振兵, 赵爱红等. 高超声速流场等离子体合成射流逆向喷流特性研究. 航空学报, 2022, 43(S2): 27747-11 (Ma Zhengxue, Luo Zhenbing, Zhao Aihong, et al. Research on the reverse jet of plasma synthetic jet at hypersonic speed. Acta Aeronautica et Astronautica Sinica, 2022, 43(S2): 27747-11 (in Chinese)
|
[18] |
孙志坤, 史志伟, 张伟麟等. 等离子体激励器对高速翼型升阻特性的影响. 航空学报, 2022, 43(S2): 727705-16 (Sun Zhikun, Shi Zhiwei, Zhang Weilin, et al. Effect of plasma actuator on lift-drag characteristics of high-speed airfoil. Acta Aeronautica et Astronautica Sinica, 2022, 43(S2): 727705-16 (in Chinese)
|
[19] |
吴云, 李应红. 等离子体流动控制研究进展与展望. 航空学报, 2015, 36(2): 381-405 (Wu Yun, Li Yinghong. Progress and outlook of plasma flow control. Acta Aeronautica et Astronautica Sinica, 2015, 36(2): 381-405 (in Chinese)
|
[20] |
李洋, 梁华, 贾敏等. 等离子体合成射流改善翼型气动性能实验研究. 推进技术, 2017, 38(9): 1943-1949 (Li Yang, Liang Hua, Jia Min, et al. Experimental investigation of enhancingwing aerodynamic performance by plasma synthetic jet. Journal of Propulsion Technology, 2017, 38(9): 1943-1949 (in Chinese) doi: 10.13675/j.cnki.tjjs.2017.09.004
|
[21] |
苏志, 李军, 梁华等. 多路等离子体合成射流改善翼型性能实验研究. 推进技术, 2018, 39(9): 1928-1937 (Su Zhi, Li Jun, Liang Hua, et al. Experimental investigation of enhancing airfoil aerodynamic performance with multichannel plasma synthetic jet. Journal of Propulsion Technology, 2018, 39(9): 1928-1937 (in Chinese)
|
[22] |
Gao T, Luo Z, Zhou Y, et al. Novel deicing method based on plasma synthetic jet actuator. AIAA Journal, 2020, 58(9): 4181-4188
|
[23] |
Gao T, Luo Z, Zhou Y, et al. Experimental investigation on ice-breaking performance of a novel plasma striker. Chinese Journal of Aeronautics, 2022, 35(1): 307-317
|
[24] |
Laurendeau F, Chedevergne F, Casalis G. Transient ejection phase modeling of a plasma synthetic jet actuator. Physics of Fluids, 2014, 26(12): 125101
|
[25] |
Shin JY, Kim HJ, Kim KH. Development of one-dimensional analytical model for a sparkjet actuator. AIAA Journal, 2021, 59(3): 1055-1074
|
[26] |
Anderson KV, Knight DD. Plasma jet for flight control. AIAA Journal, 2012, 50(9): 1855-1872
|
[27] |
Xie W, Luo Z, Zhou Y, et al. Experimental and numerical investigation on opposing plasma synthetic jet for drag reduction. Chinese Journal of Aeronautics, 2022, 35(8): 75-91
|
[28] |
Narayanaswamy V, Raja LL, Clemens NT. Control of a shock/boundary-layer interaction by using a pulsed-plasma jet actuator. AIAA Journal, 2012, 50(1): 246-249
|
[29] |
Narayanaswamy V, Raja LL, Clemens NT. Control of unsteadiness of a shock wave/turbulent boundary layer interaction by using a pulsed-plasma-jet actuator. Physics of Fluids, 2012, 24(7): 076101
|
[30] |
Greene BR, Clemens NT, Magari P, et al. Control of mean separation in shock boundary layer interaction using pulsed plasma jets. Shock Waves, 2014, 25(5): 495-505
|
[31] |
Liu R, Niu Z, Wang M, et al. Aerodynamic control of NACA 0021 airfoil model with spark discharge plasma synthetic jets. Science China Technological Sciences, 2015, 58(11): 1949-1955
|
[32] |
Sun Z, Shi Z, Zhang W, et al. Numerical investigation on flow control of a hypersonic airfoil by plasma synthetic jet. Journal of Aerospace Engineering, 2022, 35(5): 04022071
|
[33] |
Jin D, Cui W, Li Y, et al. Characteristics of pulsed plasma synthetic jet and its control effect on supersonic flow. Chinese Journal of Aeronautics, 2015, 28(1): 66-76
|
[34] |
Li Z, Shi Z, Du H. Analytical model:characteristics of nanosecond pulsed plasma synthetic jet actuator in multiple-pulsed mode. Advances in Applied Mathematics and Mechanics, 2017, 9(2): 439-462
|
[35] |
Zhang W, Geng X, Shi Z, et al. Study on inner characteristics of plasma synthetic jet actuator and geometric effects. Aerospace Science and Technology, 2020, 105: 106044
|
[36] |
Du H, Shi Z, Cheng K, et al. The study of flow separation control by a nanosecond pulse discharge actuator. Experimental Thermal and Fluid Science, 2016, 74: 110-121
|