Effect of pressure on the performance of plasma synthetic jet actuator

被引:25
作者
Wang Lin [1 ]
Xia ZhiXun [1 ]
Luo ZhenBing [2 ]
Zhang Yu [2 ]
机构
[1] Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China
[2] Natl Univ Def Technol, Coll Aerosp Sci Technol, Changsha 410073, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
synthetic jet; plasma actuator; high speed shadowgraph images; ambient pressure level; FLOW-CONTROL; CROSS-FLOW;
D O I
10.1007/s11433-014-5611-1
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
The effects of the ambient air pressure level on the performance of plasma synthetic jet actuator have been investigated through electrical and optical diagnostics. Pressures from 1 atm down to 0.1 atm were tested with a 10 Hz excitation. The discharge measurement demonstrates that there is a voltage range to make the actuator work reliably. Higher pressure level needs a higher breakdown voltage, and a higher discharge current and energy deposition are produced. But when the actuator works with the maximum breakdown voltage, the fraction of the initial capacitor energy delivered to the arc is almost invariable. This preliminary study also confirms the effectiveness of the plasma synthetic jet at low pressure. Indeed, the maximum velocities of the precursor shock and the plasma jet induced by the actuator with maximum breakdown voltage are independent of the ambient pressure level; reach about 530 and 460 m/s respectively. The mass flux of the plasma jet increases with ambient pressure increasing, but the strength of the precursor shock presents a local maximum at 0.6 atm.
引用
收藏
页码:2309 / 2315
页数:7
相关论文
共 50 条
  • [41] Study on propagation mechanisms of the actuations generated by plasma synthetic jet actuator in a supersonic flow
    Zhang, Weilin
    Shi, Zhiwei
    Li, Zheng
    Geng, Xi
    Zhang, Chuanhong
    Sun, Quanbing
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 126
  • [42] Comparison of Separation Control Mechanisms for Synthetic Jet and Plasma Actuators
    Abe, Yoshiaki
    Nonomura, Taku
    Sato, Makoto
    Aono, Hikaru
    Fujii, Kozo
    ACTUATORS, 2023, 12 (08)
  • [43] Fabrication of a multi-stage plasma synthetic jet actuator using printed electronics
    Sato, Shintaro
    Enokido, Tomoki
    Ohnishi, Naofumi
    AIP ADVANCES, 2021, 11 (04)
  • [44] Jet control by a coaxial type dbd plasma actuator
    Miyagi, Norimasa
    Ohnishi, Masumi
    Asakura, Jun
    Sayo, Kentaro
    Kimura, Motoaki
    Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 2013, 79 (806): : 2041 - 2052
  • [45] Experimental and numerical response of a high-Reynolds-number M=0.6 jet to a Plasma Synthetic Jet actuator
    Chedevergne, F.
    Leon, O.
    Bodoc, V.
    Caruana, D.
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2015, 56 : 1 - 15
  • [46] Experiment on Jet Flow Control by SDBD Plasma Actuator
    Li, Jinlong
    Li, Xiudian
    Zhang, Zheng
    Che, Xueke
    Nie, Wansheng
    Zheng, Zhi
    PROCEEDINGS OF THE ADVANCES IN MATERIALS, MACHINERY, ELECTRICAL ENGINEERING (AMMEE 2017), 2017, 114 : 578 - 582
  • [47] Experimental characteristics of a two-electrode plasma synthetic jet actuator array in serial
    Zhou, Yan
    Xia, Zhixun
    Luo, Zhenbing
    Wang, Lin
    Deng, Xiong
    CHINESE JOURNAL OF AERONAUTICS, 2018, 31 (12) : 2234 - 2247
  • [48] Circular jet with annular backflow using a dielectric barrier discharge plasma actuator (Effect of backflow on circular jet diffusion)
    Miyagi, Norimasa
    Kimura, Motoaki
    JOURNAL OF FLUID SCIENCE AND TECHNOLOGY, 2023, 18 (01):
  • [49] Helmholtz Resonance Frequency of the Synthetic Jet Actuator
    Gil, Pawel
    Wilk, Joanna
    Korzeniowski, Michal
    APPLIED SCIENCES-BASEL, 2021, 11 (12):
  • [50] Multiphysics Modeling of a Synthetic Jet Actuator in Operation
    Butler, Matthew G. M.
    Ekmekci, Alis
    Sullivan, Pierre E.
    ACTUATORS, 2024, 13 (02)