A Plasma Synthetic Jet (PSJ) actuator is the promised equipment to produce a high-speed synthetic jet, which can be potentially applied to control the supersonic flow. Several researchers paid much attention to its application on Active Flow Control (AFC) in supersonic conditions, but the understanding of the flow field inner the cavity is extremely inadequate. This study aims to use experimental measurement and numerical simulation to reveal the variation of flow field during the issuing PSJ. The PSJ actuator driven by the capacitor group has been designed, and Large Eddy Simulation(LES) was conducted and verified by experimental data with high-resolution particle image velocimetry (PW) and hot wire anemometer (HWA). The kinetic energy of the PSJ dominantly results from its thermal energy during the stage of plasma deposition, which makes the pressure and temperature of tiny volume near the electrode, increase sharply in microseconds. The electric discharge of the PSJ actuator is simulated by employing the energy input into the source term of the energy equation. The efficiency of the actuator was 20% is demonstrated in this study, which is consistent with the previous research. It is found that the high-pressure zone generated by plasma deposition shifts in a reciprocating way between the bottom and top of the cavity. The pressure inner the cavity and velocity of the PSJ attenuate while oscillating with the real-time. The geometry of the actuator paly a significant role in the performance of the PSJ. Keeping the cavity height constant, the frequency of the pressure is almost the same because the attenuating frequency is related to the cavity height. Increasing cavity height decreases attenuating frequency. The attenuation rate increases with the increase of orifice diameter and decreases of orifice height because of the leaking of gas from the cavity. The mathematic model is built and verified to describe the variation of pressure inner the cavity and the velocity of the PSJ.
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Wei XIE
Zhenbing LUO
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Zhenbing LUO
Yan ZHOU
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Yan ZHOU
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Wenqiang PENG
Qiang LIU
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Qiang LIU
Dengpan WANG
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Beijing Special Engineering Design and ResearchCollege of Aerospace Engineering, National University of Defense Technology
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Wei XIE
Zhenbing LUO
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Zhenbing LUO
Yan ZHOU
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Yan ZHOU
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Wenqiang PENG
Qiang LIU
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College of Aerospace Engineering, National University of Defense TechnologyCollege of Aerospace Engineering, National University of Defense Technology
Qiang LIU
Dengpan WANG
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Beijing Special Engineering Design and Research InstituteCollege of Aerospace Engineering, National University of Defense Technology
机构:
Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China
Song, Guozheng
Zong, Haohua
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Xi An Jiao Tong Univ, Sch Mech Engn, Xian 710049, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China
Zong, Haohua
Liang, Hua
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China
Liang, Hua
Su, Zhi
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China
Su, Zhi
Xie, Like
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China
Xie, Like
Zheng, Xing
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China
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Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering UniversityScience and Technology on Plasma Dynamics Laboratory, Air Force Engineering University
宋国正
宗豪华
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School of Mechanical Engineering, Xi'an JiaotongScience and Technology on Plasma Dynamics Laboratory, Air Force Engineering University
宗豪华
梁华
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Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering UniversityScience and Technology on Plasma Dynamics Laboratory, Air Force Engineering University
梁华
苏志
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Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering UniversityScience and Technology on Plasma Dynamics Laboratory, Air Force Engineering University
苏志
谢理科
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Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering UniversityScience and Technology on Plasma Dynamics Laboratory, Air Force Engineering University
谢理科
郑猩
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Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering UniversityScience and Technology on Plasma Dynamics Laboratory, Air Force Engineering University