Effect of electrode geometry on the flow structure induced by plasma actuators

被引:14
作者
Sun, Zhikun [1 ]
Shi, Zhiwei [1 ]
Li, Zheng [2 ]
Geng, Xi [1 ]
Yin, Zhenquan [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Key Lab Unsteady Aerodynam & Flow Control, Minist Ind & Informat Technol, Nanjing 210016, Peoples R China
[2] China Acad Launch Vehicle Technol, Sci & Technol Space Phys Lab, Beijing 100076, Peoples R China
关键词
Electric discharges - Electrodes - Flow structure - Heat transfer - Infrared imaging - Point contacts;
D O I
10.1063/5.0111877
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Pulsed surface arc discharge (PSAD) is one of the essential techniques in flow control. In this paper, the effects of electrode configuration on heat transfer characteristics of PSAD and disturbance characteristics of PSAD on the flow field were investigated by thermal imaging technology and high-speed photography technology. By defining the curvature of curve (COC) of the electrode, we investigated the physical mechanism of the electrode configuration, affecting the PSAD disturbed flow field. The results show that the COC has the optimal solution COCopt. When COC <= COCopt, the smaller the COC, the more concentrated the PSAD disturbances to the flow field. When COC > COCopt, the electrode configuration will have an end point effect, resulting in a deviation between the theoretical COC and the real COC. The larger the COC, the stronger the end point effect, and the more concentrated the PSAD disturbances to the flow field. The COC affects the disturbance degree of PSAD to the flow field by distorting the electric field intensity distribution. The change in the electric field intensity causes the fluctuation frequency of the flow field to be inconsistent with the discharge frequency of the PSAD. The stronger the distortion degree of the electric field intensity, the stronger the high-frequency characteristics of the fluctuating frequency of the flow field, and the stronger the high-frequency characteristics of the flow mode of the flow field. In addition, we obtained the value range of COCopt within 0.5-0.7 through theoretical derivation and established a mathematical model of electrode structure's effect on the flow field's flow structure. Published under an exclusive license by AIP Publishing.
引用
收藏
页数:13
相关论文
共 32 条
  • [1] Computational Study of Wing-Tip Effect for Flow-Control Authority of Dielectric-Barrier-Discharge Plasma Actuator
    Abe, Takumi
    Asada, Kengo
    Sekimoto, Satoshi
    Fukudome, Koji
    Tatsukawa, Tomoaki
    Mamori, Hiroya
    Fujii, Kozo
    Yamamoto, Makoto
    [J]. AIAA JOURNAL, 2021, 59 (01) : 104 - 117
  • [2] Temperature measurement of air convection using a Schlieren system
    Alvarez-Herrera, C.
    Moreno-Hernandez, D.
    Barrientos-Garcia, B.
    Guerrero-Viramontes, J. A.
    [J]. OPTICS AND LASER TECHNOLOGY, 2009, 41 (03) : 233 - 240
  • [3] Study on instability of circular liquid jets at subcritical to supercritical conditions using dynamic mode decomposition
    Ayyappan, Dhanesh
    Kumar, Ajith S.
    Vaidyanathan, Aravind
    Nandakumar, K.
    [J]. PHYSICS OF FLUIDS, 2020, 32 (01)
  • [4] Plasma Control of a Turbulent Shock Boundary-Layer Interaction
    Bisek, Nicholas J.
    Rizzetta, Donald P.
    Poggie, Jonathan
    [J]. AIAA JOURNAL, 2013, 51 (08) : 1789 - 1804
  • [5] Actuators for Active Flow Control
    Cattafesta, Louis N., III
    Sheplak, Mark
    [J]. ANNUAL REVIEW OF FLUID MECHANICS, VOL 43, 2011, 43 : 247 - 272
  • [6] Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications
    Corke, Thomas C.
    Post, Martiqua L.
    Orlov, Dmitriy M.
    [J]. EXPERIMENTS IN FLUIDS, 2009, 46 (01) : 1 - 26
  • [7] On respiratory droplets and face masks
    Dbouk, Talib
    Drikakis, Dimitris
    [J]. PHYSICS OF FLUIDS, 2020, 32 (06)
  • [8] Three-dimensional wake dynamics behind a tapered cylinder with large taper ratio
    De, Arnab Kumar
    Sarkar, Sandip
    [J]. PHYSICS OF FLUIDS, 2020, 32 (06)
  • [9] Experimental study on frequency characteristics of the actuations produced by plasma synthetic jet actuator and its geometric effects
    Geng, Xi
    Zhang, Weilin
    Shi, Zhiwei
    Li, Zheng
    Sun, Qijie
    Sun, Zhikun
    [J]. PHYSICS OF FLUIDS, 2021, 33 (06)
  • [10] Active flow control of a wing section in stall flutter by dielectric barrier discharge plasma actuators
    Hajipour, M.
    Ebrahimi, A.
    Amandolese, X.
    [J]. PHYSICS OF FLUIDS, 2022, 34 (07)