Characteristics of a nanosecond pulsed sliding discharge plasma actuator at low pressure

被引:3
作者
Sun, Qijie [1 ]
Geng, Xi [1 ]
Li, Zheng [2 ]
Shi, Zhiwei [1 ]
Sun, Zhikun [1 ]
Cheng, Keming [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Minist Ind & Informat Technol, Key Lab Unsteady Aerodynam & Flow Control, Yudao St 29, Nanjing 210016, Peoples R China
[2] China Acad Launch Vehicle Technol, Sci & Technol Space Phys Lab, Beijing 100076, Peoples R China
关键词
FLOW-CONTROL; AIR; SEPARATION;
D O I
10.1063/5.0160843
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The behavior of a nanosecond pulsed sliding discharge plasma actuator with the ambient pressure from 27 to 101 kPa is experimentally investigated. The electric characteristics, discharge morphologies, and surface temperature distribution of the actuator supplied by constant voltages are studied under different pressure conditions. The threshold pressure for sliding discharge establishment is 54-75 kPa in this paper. The results show that the positive peak value of the current tends to increase as the pressure decreases. Time-integrated discharge images indicate that plasma luminosity and uniformity are enhanced under low-pressure conditions. The discharge morphology of the actuator at 27 kPa displays an alternating distribution of bright and dark stripes. The infrared thermal results demonstrate that decreasing the pressure increases the actuator's surface temperature, intensifies the intensity of spanwise temperature oscillations, and improves the homogeneity in the streamwise direction.
引用
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页数:13
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共 37 条
  • [21] Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge
    Roupassov, D. V.
    Nikipelov, A. A.
    Nudnova, M. M.
    Starikovskii, A. Yu.
    [J]. AIAA JOURNAL, 2009, 47 (01) : 168 - 185
  • [22] Flow control with plasma synthetic jet actuators
    Santhanakrishnan, Arvind
    Jacob, Jamey D.
    [J]. JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2007, 40 (03) : 637 - 651
  • [23] Improving Performance of a Sliding Dielectric Barrier Discharge Actuator Using Multiple Potentials
    Seney, Steven D.
    Huffman, Richard E.
    Bailey, William
    Liu, David
    Reeder, Mark F.
    Stults, Joshua
    [J]. AIAA JOURNAL, 2016, 54 (10) : 3317 - 3320
  • [24] Control of a swept-wing boundary layer using ring-type plasma actuators
    Shahriar, Nima
    Kollert, Matthias R.
    Hanifi, Ardeshir
    [J]. JOURNAL OF FLUID MECHANICS, 2018, 844 : 36 - 60
  • [25] Time behaviour of discharge current in case of nanosecond-pulse surface dielectric barrier discharge
    Shao, Tao
    Jiang, Hui
    Zhang, Cheng
    Yan, Ping
    Lomaev, Mikhail I.
    Tarasenko, Victor F.
    [J]. EPL, 2013, 101 (04)
  • [26] Plasma Sheet Actuator Driven by Repetitive Nanosecond Pulses with a Negative DC Component
    Song Huimin
    Zhang Qiaogen
    Li Yinghong
    Jia Min
    Wu Yun
    Liang Hua
    [J]. PLASMA SCIENCE & TECHNOLOGY, 2012, 14 (04) : 327 - 332
  • [27] Electrical and plasma characteristics of a quasi-steady sliding discharge
    Sosa, R.
    Kelly, H.
    Grondona, D.
    Marquez, A.
    Lago, V.
    Artana, G.
    [J]. JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2008, 41 (03)
  • [28] Effect of electrode geometry on the flow structure induced by plasma actuators
    Sun, Zhikun
    Shi, Zhiwei
    Li, Zheng
    Geng, Xi
    Yin, Zhenquan
    [J]. PHYSICS OF FLUIDS, 2022, 34 (09)
  • [29] Plasma actuators for cylinder flow control and noise reduction
    Thomas, Flint O.
    Kozlov, Alexey
    Corke, Thomas C.
    [J]. AIAA JOURNAL, 2008, 46 (08) : 1921 - 1931
  • [30] Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control
    Thomas, Flint O.
    Corke, Thomas C.
    Iqbal, Muhammad
    Kozlov, Alexey
    Schatzman, David
    [J]. AIAA JOURNAL, 2009, 47 (09) : 2169 - 2178