Processing math: 100%
Advanced Search+
Chen LI, Ruoyu HAN, Yi LIU, Jinlin ZHAO, Yanan WANG, Feng HE, Jiting OUYANG. Discharge and post-explosion behaviors of electrical explosion of conductors from a single wire to planar wire array[J]. Plasma Science and Technology, 2022, 24(1): 015507. DOI: 10.1088/2058-6272/ac3972
Citation: Chen LI, Ruoyu HAN, Yi LIU, Jinlin ZHAO, Yanan WANG, Feng HE, Jiting OUYANG. Discharge and post-explosion behaviors of electrical explosion of conductors from a single wire to planar wire array[J]. Plasma Science and Technology, 2022, 24(1): 015507. DOI: 10.1088/2058-6272/ac3972

Discharge and post-explosion behaviors of electrical explosion of conductors from a single wire to planar wire array

More Information
  • Corresponding author:

    Ruoyu HAN, E-mail: han.ruoyu@hotmail.com

  • Received Date: August 31, 2021
  • Revised Date: November 11, 2021
  • Accepted Date: November 12, 2021
  • Available Online: March 18, 2024
  • Published Date: December 14, 2021
  • This work deals with an experimental study of a Cu planar wire array (PWA) in air and water under the stored energy 300–1200 J. A single Cu wire is adopted as a controlled trial. Four configurations of PWA and a wire with the same mass (cross-section area) but the different specific surface areas (15–223 cm2 g-1) are exploded. The transient process is analyzed using high-speed photography in combination with the results of optical emission and discharge. Discharge characteristics revealed that PWA always has a higher electric power peak, early but higher voltage peak, as well as faster vaporization and ionization process than the single-wire case. Two to three times stronger optical emission could be obtained when replacing the single-wire with PWA, indicating a higher energy-density state is reached. Phenomenologically, in both air and water, single-wire load tends to develop a transverse stratified structure, while PWA is dominated by the uneven energy deposition among wires. Finally, the synchronism and uniformity of the PWA explosion are discussed.

  • Nowadays, the dielectric barrier discharge (DBD) based on sinusoidal alternating current high frequency and high voltage actuation (AC-DBD) and dielectric barrier discharge based on nanosecond pulsed voltage actuation (NS-DBD) are the most studied in the plasma application field [14]. These two discharge methods are widely used in flow field control. The first to attract researchers is AC-DBD, which can induce a wall jet with a speed ranging from 0 to 11 m s-1, and it can control the flow separation of the flow field with an incoming flow velocity up to 100 m s-1 [57]. Later, studies have shown that NS-DBD has stronger flow control capabilities, so in recent years it has also attracted more and more attention from researchers. For NS-DBD, the flow control mechanism is mainly the rapid heat release effect caused by the rapid heating of local air [810].

    During the study of the actuated discharge characteristics of NS-DBD plasma, the influence of the actuation parameters, the configuration of the actuator, the type of the insulating dielectric layer on the energy consumption, the voltage and current waveform, and the discharge modes are mostly discussed. Jiang Hui et al [1114] studied the influence of actuation voltage peak, actuation frequency, electrode width, and electrode spacing on the discharge characteristics of NS-DBD. The results showed that increasing the actuation voltage could make the discharge filament more uniform, and meanwhile the plasma filament length would also increase. Zhou Yang et al [15] compared the discharge characteristics of nanosecond pulsed plasma actuation and microsecond pulsed plasma actuation at different actuation voltages. The results showed that with the actuation voltage amplitude increasing, the current peak value and energy consumption of the surface DBD at the two actuation conditions increase. Ndong et al [16] conducted experimental studies on the voltage and current waveforms and the changes of single pulsed energy at different electrical parameters. Compared with the negative polarity pulsed voltage, the positive polarity pulsed voltage actuation can bring greater energy deposition. Takashima et al [17] used high-speed schlieren technology to observe the flow field characteristics of the NS-DBD plasma actuation from the lateral and longitudinal sides of the actuator respectively and observed the shock wave structure. Zhao et al [18, 19] used a dynamic pressure sensor with a higher response frequency and a two-dimensional phase-locked PIV to measure the flow field characteristics of NS-DBD actuation. The NS-DBD plasma actuation can induce an instantaneous flow of the flow field, and a continuous vortex with a speed less than 0.3 m s-1 will be generated near the wall area. The heat generated by NS-DBD plasma actuation can be divided into two parts: the rapid heating of the air near the wall and the heating of the dielectric layer material. At the same time, there is a process of convective heat transfer between the dielectric layer material and the heated air on the upper layer [20]. Unfer et al [21] simulated and calculated that nanosecond pulsed plasma actuation would instantaneously (at the time scale of a nanosecond) heat the air near the wall to about 1000 K. The simulation results of Zhu Yifei et al [22, 23] showed that the near-wall air would be rapidly heated to 1100 K and then rapidly dropped to 310 K at a speed of k=-225/t Ks-1, and the heating area was approximately equal to the extension area of plasma discharge filaments. The simulation results of Zhu Yifei et al showed that the near-wall air would be rapidly heated to 1100 K and then rapidly dropped to 310 K at a speed of k=−225/t Ks-1 and the heating area was approximately equal to the extension area of plasma discharge filaments. Popov et al [24] proposed a rapid heating model of breakdown discharge in the nitrogen–oxygen mixture environment. Under different reduced field intensities, the physical and chemical reactions that play a major role in gas heating are the dissociation reaction of oxygen caused by electron collision and the dissociation reaction of nitrogen molecules under the action of electron collision.

    Researchers have studied the effects of peak actuation voltage, pulsed actuation frequency, and electrode size of the actuator on the discharge characteristics and induced flow field characteristics of NS-DBD. However, there are few researches on the infrared radiant thermal characteristics of NS-DBD. With the development of NS-DBD plasma actuation, it can not only be used for flow control, but also has application prospects in the field of aircraft anti-icing [25, 26]. Therefore, the law of its thermal effect and induced flow field effect with actuation parameters is worthy of in-depth research.

    In this work, the effects of the pulsed voltage, actuation frequency and the width of the covered electrode on the discharge characteristics, flow field characteristics and infrared radiation thermal characteristics of NS-DBD have been studied, and the influence of various parameters on the actuation characteristics of NS-DBD plasma has been obtained.

    The configuration of the plasma actuator is shown in figure 1, including an upper electrode, a covering electrode, an insulating medium (Kapton), and a base plate. Copper foil with a thickness of 0.027 mm is used as the electrode material of the actuator. The upper electrode is exposed in the air and the width is 5 mm. The width of the covering electrode w is selected as three sizes: 5 mm, 10 mm, and 20 mm respectively. The lengths of the upper electrode and the covering electrode are both 60 mm. The dielectric layer is made of polyimide tape with a thickness of 0.18 mm and a dielectric constant of 3.4. The substrate plate is an aluminum nitride ceramic sheet with an area of 100 mm×100 mm and a thickness of 1 mm.

    Figure  1.  Surface dielectric barrier discharge plasma actuator.

    The nanosecond pulsed power supply (Parametric High-voltage Pulsed Power Supply, Xi'an Smart Maple Electronic Technology Co., Ltd, Xi'an, China) is used in the experiment. The output voltage waveform is shown in figure 2. The peak output voltage range of the power supply is continuously adjustable from 0 to 20 kV. The pulsed repetition frequency is continuously adjustable from 1 Hz to 20 kHz. the pulsed width tp is adjustable from 0 ns to 1 ms, and the rising edge time tr and falling edge time td are both adjustable.

    Figure  2.  Schematic diagram of the output voltage waveform of the nanosecond pulsed power supply.

    The NS-DBD plasma actuation discharge characteristic test system mainly includes a voltage probe, a current probe, an oscilloscope, and a CCD camera, as shown in figure 3. The voltage and current applied to the upper electrode and the covering electrode of the actuator were measured by a voltage probe (Tektronix, P6015A) and a current probe (Tektronix, TCP0030A), respectively. The accuracy of the current probe is 1 mA. A digital oscilloscope (Tektronix, DPO4104) is used to display and store voltage–current signals at a sampling frequency of 5 GHz. The discharge image was taken by a Nikon D7000 digital camera with an exposure time of 0.04 s. The single pulsed energy of NS-DBD was computed by the integration of product the voltage and current acquired through oscilloscope over the single pulsed time: W=v(t)·i(t)·dt.

    Figure  3.  Layout of NS-DBD electrical characteristics test system.

    The high-speed schlieren technology is used to observe the induced flow field of NS-DBD plasma actuation in still air. As shown in figure 4, the high-speed schlieren test system mainly includes a xenon lamp, lens, knife edge, and high-speed camera. The xenon lamp is used as the light source to produce a parallel light path between the two concave lenses. The NS-DBD plasma actuator is placed in the parallel light path to observe the NS-DBD plasma actuation induced flow field. A high-speed camera (Phantom—V2512) was used to capture the schlieren image induced by NS-DBD actuation. The camera frame rate is 40 000 fps. During the experiment, the resolution is 1024×1024 pixel2, and the camera exposure time is 0.000 002 s. The field of view for schlieren is 25 mm high and 30 mm long, and the actuator is perpendicular to it and parallel to the optical path. Through the DG535 time-delay pulsed generator, the high-voltage pulsed power supply, and the high-speed camera are triggered synchronously to shoot.

    Figure  4.  High-speed schlieren experimental system diagram.

    The infrared thermal imager used in the experiment is FLIR SC7300M, and the temperature measurement range is from -20 ℃ to 2000 ℃. The infrared thermal imager is close to the surface of the actuator, so the attenuation of radiated power caused by the absorption and scattering of various components in the air can be ignored. The emissivity of polyimide tape was set as 0.83. The sampling frequency of the infrared thermal imager in the experiment is 25 Hz.

    The pulsed actuation frequency of 2 kHz, rising edge time of 150 ns, a pulsed width of 100 ns, falling edge time of 150 ns, and covering electrode width of 20 mm were selected to remain unchanged, and the output voltage peak value was changed.

    Figure 5 shows the variation of single pulsed energy and the peak value of positive and negative current with the increase of the pulsed voltage peak value. It can be seen that with the increase of the peak value of the pulsed voltage, the peak value of the positive and negative pulsed current and the single pulsed energy both increase nonlinearly, which is consistent with the research results in the literature [27].

    Figure  5.  Schematic diagram of positive and negative peak current and single pulsed energy change with voltage.

    Figure 6 shows the discharge images at different voltage peaks. It can be seen that the voltage peak has a greater impact on the discharge area and discharge pattern. When the peak voltage is 8 kV, the discharge is mainly concentrated in the range less than 2 mm from the edge of the electrode, the discharge area is small, and the brightness is darker from the discharge image. With the increase of the voltage peak value, the discharge filaments continue to grow, the discharge area gradually increases, and the discharge becomes more intense and the brightness is greater. Therefore, a larger range of plasma discharge can be obtained by increasing the peak value of the pulsed voltage.

    Figure  6.  Discharge images of different voltage peaks (exposure time 0.04 s).

    Figure 7 shows the change process of the flow field induced by nanosecond pulsed actuation with different pulsed voltage peaks. It can be seen that the greater the peak value of the pulsed voltage, the greater the actuation intensity and the greater the disturbance to the still air. In addition, it can be concluded that by observing the change in the length of the tail as the peak value of the pulsed voltage increases, the tail of the induced shock wave structure becomes longer. Combined with the discharge image, it can be obtained that the length of the tail of the shock wave structure is related to the length of the discharge filament, which is consistent with the previous conclusions.

    Figure  7.  Variation process of the flow field induced by nanosecond pulsed actuation with different pulsed voltage peaks: (a) 8 kV, (b) 10 kV, (c) 12 kV, (d) 14 kV.

    Figure 8 shows the distribution of the surface temperature of the actuator with different pulsed voltage peaks at the time of 120 s. It can be seen that as the peak value of the pulsed voltage increases, the surface temperature of the dielectric layer will increase significantly, and the high-temperature area will also increase significantly.

    Figure  8.  Surface temperature distribution of the actuator after continuous discharge of 120 s (t=120 s) with different pulsed voltage peaks.

    Figure 9 shows the changes of the surface temperature along the X-axis at Y=4 mm under different pulsed voltage peak conditions (t=120 s). When the pulsed voltage peak value increases from 8 to 10 kV, the surface temperature increases by about 5 ℃. When the peak value of the pulsed voltage increases from 10 to 12 kV, the temperature increases by nearly 30 ℃.

    Figure  9.  The surface temperature changes under different pulsed voltage peak values along the X-axis at Y=4 mm direction (t=120 s).

    The results in figures 10 and 11 also show that the surface temperature significantly increases with the increase of the pulsed voltage peak value. It can be seen from the graph of surface temperature changing with time in figure 11 that the higher the peak value of the pulsed voltage, the faster the surface temperature rises. Besides, it should be pointed out that in figure 11, when the pulsed voltage peak value is 14 kV, the sudden drop in temperature at the time of 72 s is caused by the breakdown of the actuator. The insulating medium (Kapton) near the upper electrode reaches the ignition point, causing the insulating material to ignite and breakdown. A plasma arc was generated at the location where it was pierced, and a strong current was formed, causing the circuit to short-circuit.

    Figure  10.  Changes of surface temperature along the Y-axis at X=30 mm at different pulsed voltage peaks (t=120 s).
    Figure  11.  Variation of surface temperature with time at point A (X=30 mm, Y=4 mm) at different pulsed voltage peaks.

    Increasing the pulsed voltage peak increases the actuation intensity of the single pulsed energy, so the input energy is also very high. The intensity of the electric field increases as the voltage increases, so that the gas far away from the upper electrode can also be broken down. Thus, the discharge filament becomes longer with the increase of voltage. The higher the energy is, the faster the surrounding flow field flows, the faster the temperature rises and the wider the actuation range is.

    The pulsed voltage peak value is 12 kV, the rising edge time is 150 ns, the pulsed width is 100 ns, the falling edge time is 150 ns, and the covering electrode width is 20 mm. Further study was carried out by changing the pulsed actuation frequency.

    Figure 12 shows the variation of the single pulsed energy and the peak value of positive and negative current with the increase of pulsed actuation frequency. It can be seen that the change of the pulsed actuation frequency has almost no effect on the peak value of the positive and negative current and the single pulsed energy, indicating that the change of the pulsed actuation frequency only changes the number of discharges per unit time, but has no effect on the single discharge process. This conclusion is consistent with the conclusion in the literature [25], but is not consistent with the conclusion in the literature [17]. The difference in experimental results is due to the different internal structures and design principles of the high-voltage pulsed power supply.

    Figure  12.  Schematic diagram of positive and negative peak current and single pulsed energy change with frequency.

    Figure 13 shows the discharge images of different pulsed actuation frequencies. By comparison, as the pulsed frequency increases, the filament discharge brightness gradually increases, but the filament length and discharge area hardly change. The reason is that the actuation frequency does not affect the single discharge process. With the increase of frequency, the discharge times per unit time increase, which is reflected in the discharge images of multiple pulsed integrals, so the brightness increases.

    Figure  13.  Discharge images of different pulsed frequencies (exposure time 0.04 s).

    Figure 14 shows the change process of the flow field induced by nanosecond pulsed actuation with different pulsed actuation frequencies. It can be seen from the figure that the single shock wave structure almost does not change with the increase of pulsed actuation frequency, which is consistent with the previous conclusion that changing the pulsed actuation frequency has almost no effect on a single discharge. Besides, as the pulsed actuation frequency increases, the more discharge times per unit time, the faster the energy accumulation, and the faster the induced flow field tends to a steady state.

    Figure  14.  Variation process of the flow field induced by nanosecond pulsed actuation with different pulsed actuation frequencies: (a) 500 Hz, (b) 1000 Hz, (c) 2000 Hz, (d) 4000 Hz.

    Figure 15 shows the surface temperature distribution cloud diagram under different pulsed actuation frequencies after the discharge time is 120 s. Figures 16 and 17 show the temperature distribution along the X-axis and Y-axis, respectively. It can be seen that increasing the pulsed actuation frequency will keep the heated area unchanged, but the surface temperature of the dielectric layer will increase accordingly. Because the pulsed actuation frequency is increased, the number of discharges per unit time increases. However, the single pulsed energy remains unchanged, so the energy loaded per unit time increases and the surface temperature of the dielectric layer increases. According to the results given in figure 18, as the pulsed actuation frequency increases, the temperature rises faster.

    Figure  15.  Surface temperature distribution of the actuator after continuous discharge of 120 s (t=120 s) with different pulsed actuation frequencies.
    Figure  16.  The surface temperature changes under different pulsed actuation frequencies along the X-axis at Y=4 mm direction (t=120 s).
    Figure  17.  Changes of surface temperature along the Y-axis at X=30 mm at different pulsed actuation frequencies (t=120 s).
    Figure  18.  Variation of surface temperature with time at point A (X=30 mm, Y=4 mm) at different pulsed actuation frequencies.

    The pulsed voltage peak remains unchanged to change the actuation frequency, but the single pulsed energy of the discharge does not change. The width of the discharge filaments is unchanged, but the brightness is brighter. This is because the increase of frequency makes the discharge filament that can be recorded increase, and the brightness is more obvious. Increasing the frequency increases the input power and the energy injected into the flow field, strengthening its effect on the surrounding flow field and increasing the thermal effect accordingly.

    The peak value of the pulsed voltage is 12 kV, the pulsed excitation frequency is 2 kHz, and the width of the covered electrode is changed.

    Figure 19 shows the variation of the single pulsed energy with the change of the rising edge time, falling edge time, and pulsed width with different coverage electrode widths. It can be seen that the width of the covered electrode has a greater influence on the single pulsed energy, and the wider the width of the covered electrode, the greater the single pulsed energy. Under different coverage electrode widths, the changing trend of single pulsed energy with a rising edge, falling edge, and pulsed width is not obvious. However, the smaller the electrode width, the smaller the influence of the electrical parameters on the single pulsed energy change.

    Figure  19.  Variation of single pulsed energy with rising edge time, falling edge time, and pulsed width with different covered electrode widths.

    Figure 20 shows the discharge images of different electrode widths when the pulsed voltage peak is 12 kV, the pulsed frequency is 2 kHz, the rising edge time is 150 ns, the pulsed width is 500 ns, and the falling edge time is 150 ns. It can be seen that the electrode width also has a greater influence on the discharge area and discharge pattern. When the electrode width is 5 mm, the discharge area is smaller and the brightness is relatively dark. As the electrode width increases, the discharge filaments gradually grow, the discharge area gradually increases, and the discharge becomes more intense and brighter. It is shown that the width of the covered electrode is a key parameter that restricts the size of the discharge area, and the length of the discharge filament will not exceed the width of the lower electrode. In order to obtain a larger plasma discharge area, the width of the covered electrode can be appropriately increased.

    Figure  20.  Discharge images with different covered electrode widths (exposure time 0.04 s).

    Figure 21 shows the change process of the flow field induced by nanosecond pulsed actuation under different covered electrode widths. The results show that the greater the electrode width, the greater the discharge intensity, the greater the power consumption, and the stronger the disturbance of the plasma actuation to the flow field.

    Figure  21.  Variation process of the flow field induced by nanosecond pulsed actuation with different covered electrode widths: (a) 5 mm, (b) 10 mm, (c) 20 mm.

    The pulsed voltage peak value is 12 kV, the pulsed excitation frequency is 2 kHz, the rising edge time is 150 ns, the pulsed width is 100 ns, and the falling edge time is 150 ns. The width of the covered electrode is changed.

    Figure 22 shows the surface temperature distribution of different covered electrode widths when the discharge time is 120 s. It can be seen that when the actuation parameters remain unchanged, increasing the electrode width can increase the surface temperature of the dielectric layer. The results in figures 2325 also confirm this conclusion. The width of the covered electrode limits the extension of the discharge filament so that the length of the discharge filament does not exceed the width of the covered electrode. Therefore, under the actuation parameters in this experiment, increasing the width of the covered electrode will increase the injection energy, and the energy converted into heating the wall surface will also increase, resulting in a higher surface temperature of the dielectric layer.

    Figure  22.  Surface temperature distribution of the actuator after continuous discharge of 120 s (t=120 s) with different covered electrode widths.
    Figure  23.  The surface temperature changes under different covered electrode widths along the X-axis at Y=4 mm direction (t=120 s).
    Figure  24.  Changes of surface temperature along the Y-axis at X=30 mm at different covered electrode widths (t=120 s).
    Figure  25.  Variation of surface temperature with time at point A (X=30 mm, Y=4 mm) at different covered electrode widths.

    When the voltage and frequency are constant, as the covered electrode width is wider, the discharge filament is longer, and the single pulsed energy is higher. The rising and falling edges have little effect on the single pulsed energy, and the single pulsed energy is the highest when the pulsed width is 500 ns. The longer the covered electrode width, the higher the single pulsed energy, the greater the range and intensity of the flow field and temperature field after discharge.

    NS-DBD plasma actuation is an active flow control method commonly used to control flow separation. Many characteristics and control mechanisms of NS-DBD plasma actuation, including discharge characteristics and induced flow field characteristics, have been deeply studied. For the high-frequency NS-DBD, it is found that its thermal effect is more obvious, and it has a good effect in the field of plasma anti-icing. This paper tests the plasma discharge characteristics of NS-DBD under high frequency conditions, which provides a reference for anti-icing research.

    According to the influence of pulsed voltage peak, pulsed actuation frequency, and covered electrode width on NS-DBD discharge characteristics, induced flow field characteristics, and infrared radiation thermal characteristics, the rules of surface DBD on nanosecond pulsed are analyzed. The conclusion is as follows: there exists NS-DBD in the process of pulsed voltage rising and falling, and the air is heated rapidly and the shock wave and jet with lower velocity are induced. The direction of the induced jet is greatly affected by various parameters, and the nanosecond pulsed actuation is not only simple rapid heating but also has the effect of volume force. The covered electrode width will affect the potential distribution during the discharge process, and then affect the extension process of the plasma discharge filament, and the discharge area will be restricted by the electrode width. Increasing the peak value of the pulsed voltage can significantly increase the actuation intensity, and the plasma discharge area is significantly increased. Increasing the pulsed actuation frequency can increase the number of discharges per unit time. Both will cause more energy input, and the temperature rising effect will be more obvious. The surface temperature rising of the dielectric layer is closely related to the amount of input energy. The more the input energy, the more obvious the surface temperature rising effect of the dielectric layer. The surface temperature distribution is directly affected by different discharge patterns, and the temperature rising is more obvious in the area with strong discharge and more concentrated filaments.

    This work was supported in part by National Natural Science Foundation of China (No. 51907007), Natural Science Foundation of Beijing (No. 3212034), State Key Laboratory of Electrical Insulation and Power Equipment (No. EIPE20204), and State Key Laboratory of Advanced Electromagnetic Engineering and Technology (No. AEET 2019KF006).

    Data availability statement

    The data that support the findings of this study are available from the corresponding author uponreasonable request.

  • [1]
    Chace W G 1964 Phys. Today 17 19 doi: 10.1063/1.3051737
    [2]
    Pereira N R 2020 Matter Radiat. Extremes 5 026402 doi: 10.1063/1.5133378
    [3]
    Han R Y et al 2020 J. Phys. D: Appl. Phys. 53 225202 doi: 10.1088/1361-6463/ab7798
    [4]
    Krasik Y E et al 2016 IEEE Trans. Plasma Sci. 44 412 doi: 10.1109/TPS.2015.2513757
    [5]
    Sanford T W et al 1996 Phys. Rev. Lett. 77 5063 doi: 10.1103/PhysRevLett.77.5063
    [6]
    Haines M G 2011 Plasma Phys. Control. Fusion 53 093001 doi: 10.1088/0741-3335/53/9/093001
    [7]
    Sasaki T et al 2006 Laser Part. Beams 24 371 doi: 10.1017/S0263034606060538
    [8]
    Sheftman D and Krasik Y E 2010 Phys. Plasmas 17 112702 doi: 10.1063/1.3497010
    [9]
    Kotov Y A 2003 J. Nanopart. Res. 5 539 doi: 10.1023/B:NANO.0000006069.45073.0b
    [10]
    Deeney et al 1998 Phys. Rev. Lett. 81 4883 doi: 10.1103/PhysRevLett.81.4883
    [11]
    Ryutov D D, Derzon M S and Matzen M K 2000 Rev. Mod. Phys. 72 167 doi: 10.1103/RevModPhys.72.167
    [12]
    Kantsyrev V L et al 2007 High Energy Dens. Phys. 3 136 doi: 10.1016/j.hedp.2007.02.009
    [13]
    Safronova A S et al 2011 High Energy Dens. Phys. 7 252 doi: 10.1016/j.hedp.2011.05.008
    [14]
    Li M et al 2015 Planar wire array Z-pinches on qiangguang-I facility IEEE Int. Conf. on Plasma Sciences (ICOPS) (Antalya: IEEE) p 1
    [15]
    Wu J et al 2018 Plasma Phys. Control. Fusion 60 075014 doi: 10.1088/1361-6587/aac4fe
    [16]
    Efimov S et al 2008 Phys. Plasmas 15 112703 doi: 10.1063/1.3023156
    [17]
    Antonov O et al 2013 Appl. Phys. Lett. 102 124104 doi: 10.1063/1.4798827
    [18]
    Yanuka D, Theocharous S and Bland S N 2019 Phys. Plasmas 26 122704 doi: 10.1063/1.5128720
    [19]
    Rososhek A et al 2020 Appl. Phys. Lett. 116 243702 doi: 10.1063/5.0011226
    [20]
    Qian D et al 2020 IEEE Trans. Plasma Sci. 48 3373 doi: 10.1109/TPS.2019.2963424
    [21]
    Efimov S et al 2009 J. Appl. Phys. 106 073308 doi: 10.1063/1.3243233
    [22]
    Li C et al 2020 Acta Phys. Sin. 69 075203 in Chinese doi: 10.7498/aps.69.20191797
    [23]
    Oreshkin V I and Baksht R B 2020 IEEE Trans. Plasma Sci. 48 1214 doi: 10.1109/TPS.2020.2985100
    [24]
    Rousskikh A G et al 2008 Phys. Plasmas 15 102706 doi: 10.1063/1.3000390
    [25]
    Sarkisov G S et al 2020 J. Appl. Phys. 128 183302 doi: 10.1063/5.0017528
    [26]
    Sarkisov G S et al 2004 J. Appl. Phys. 96 1674 doi: 10.1063/1.1767976
    [27]
    Grinenko A et al 2006 Phys. Plasmas 13 042701 doi: 10.1063/1.2188085
    [28]
    Yin G F et al 2020 J. Phys. D: Appl. Phys. 53 195502 doi: 10.1088/1361-6463/ab747d
    [29]
    Shelkovenko T A et al 2018 IEEE Trans. Plasma Sci. 46 3741 doi: 10.1109/TPS.2018.2852063
    [30]
    Teramoto Y et al 2001 IEEE Trans. Plasma Sci. 29 632 doi: 10.1109/27.940958
    [31]
    Rososhek A et al 2019 Appl. Phys. Lett. 115 074101 doi: 10.1063/1.5115134
    [32]
    Hu M and Kusse B R 2004 Phys. Plasmas 11 1145 doi: 10.1063/1.1644582
    [33]
    Tkachenko S I and Kuskova N I 1999 J. Phys. : Condens. Matter 11 2223 doi: 10.1088/0953-8984/11/10/009
    [34]
    Romanova V M et al 2018 Phys. Plasmas 25 112704 doi: 10.1063/1.5052549
    [35]
    Kunze H J 2009 Introduction to Plasma Spectroscopy (Berlin: Springer)
  • Related Articles

    [1]Victor TARASENKO, Dmitry BELOPLOTOV, Mikhail LOMAEV, Dmitry SOROKIN. E-beam generation in discharges initiated by voltage pulses with a rise time of 200 ns at an air pressure of 12.5–100 kPa[J]. Plasma Science and Technology, 2019, 21(4): 44007-044007.
    [2]Wenjia WANG (王文家), Deng ZHOU (周登), Yue MING (明玥). The residual zonal flow in tokamak plasmas with a poloidal electric field[J]. Plasma Science and Technology, 2019, 21(1): 15101-015101. DOI: 10.1088/2058-6272/aadd8e
    [3]Shuichi SATO, Hiromu KAWANA, Tatsushi FUJIMINE, Mikio OHUCHI. Frequency dependence of electron temperature in hollow cathode-type discharge as measured by several different floating probe methods[J]. Plasma Science and Technology, 2018, 20(8): 85405-085405. DOI: 10.1088/2058-6272/aabfcd
    [4]Zheng ZHANG (张政), Xueke CHE (车学科), Wangsheng NIE (聂万胜), Jinlong LI (李金龙), Tikai ZHENG (郑体凯), Liang LI (李亮), Qinya CHEN (陈庆亚), Zhi ZHENG (郑直). Study of vortex in flow fields induced by surface dielectric barrier discharge actuator at low pressure based on Q criterion[J]. Plasma Science and Technology, 2018, 20(1): 14006-014006. DOI: 10.1088/2058-6272/aa8e95
    [5]Yang LIU (刘杨), Yue TONG (佟悦), Ying WANG (王莹), Dan ZHANG (张丹), Suyu LI (李苏宇), Yuanfei JIANG (姜远飞), Anmin CHEN (陈安民), Mingxing JIN (金明星). Influence of sample temperature on the expansion dynamics of laser-induced germanium plasma[J]. Plasma Science and Technology, 2017, 19(12): 125501. DOI: 10.1088/2058-6272/aa8acc
    [6]Yakun LIU (刘亚坤), Zhengcai FU (傅正财), Quanzhen LIU (刘全桢), Baoquan LIU (刘宝全), Anirban GUHA. Experimental and analytical investigation on metal damage suffered from simulated lightning currents[J]. Plasma Science and Technology, 2017, 19(12): 125301. DOI: 10.1088/2058-6272/aa8aca
    [7]Jianyang YU (俞建阳), Huaping LIU (刘华坪), Ruoyu WANG (王若玉), Fu CHEN (陈浮). Numerical study of the flow structures in flat plate and the wall-mounted hump induced by the unsteady DBD plasma[J]. Plasma Science and Technology, 2017, 19(1): 15502-015502. DOI: 10.1088/1009-0630/19/1/015502
    [8]Satoshi NODOMI, Shuichi SATO, Mikio OHUCHI. Electron Temperature Measurement by Floating Probe Method Using AC Voltage[J]. Plasma Science and Technology, 2016, 18(11): 1089-1094. DOI: 10.1088/1009-0630/18/11/06
    [9]WAN Gang (弯港), JIN Yong (金涌), LI Haiyuan (李海元), LI Baoming (栗保明). Study on Free Surface and Channel Flow Induced by Low-Temperature Plasma via Lattice Boltzmann Method[J]. Plasma Science and Technology, 2016, 18(3): 331-336. DOI: 10.1088/1009-0630/18/3/19
    [10]CHEN Ling (陈玲), WU Dejin (吴德金). Dispersion Equation of Low-Frequency Waves Driven by Temperature Anisotropy[J]. Plasma Science and Technology, 2012, 14(10): 880-885. DOI: 10.1088/1009-0630/14/10/05
  • Cited by

    Periodical cited type(1)

    1. Primc, G., Zaplotnik, R., Vesel, A. et al. Mechanisms Involved in the Modification of Textiles by Non-Equilibrium Plasma Treatment. Molecules, 2022, 27(24): 9064. DOI:10.3390/molecules27249064

    Other cited types(0)

Catalog

    Figures(11)  /  Tables(2)

    Article views (82) PDF downloads (101) Cited by(1)

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return