Experimental investigation on plasma jet deflection with magnetic fluid control based on PIV measurement

Kai ZHAO (赵凯); Baigang SUN (孙佰刚); Yongji LU (卢永吉); Feng LI (李锋); Yongbo LIU (刘永波); Xiangbin LIU (刘祥彬); Kefu WANG (王可夫)

doi:10.1088/2058-6272/aae09b

Plasma Science and Technology > 2019 > 21(2): 25503-025503. > DOI: 10.1088/2058-6272/aae09b

Kai ZHAO (赵凯), Baigang SUN (孙佰刚), Yongji LU (卢永吉), Feng LI (李锋), Yongbo LIU (刘永波), Xiangbin LIU (刘祥彬), Kefu WANG (王可夫). Experimental investigation on plasma jet deflection with magnetic fluid control based on PIV measurement[J]. Plasma Science and Technology, 2019, 21(2): 25503-025503. DOI: 10.1088/2058-6272/aae09b

Citation:

PDF (945 KB)

Experimental investigation on plasma jet deflection with magnetic fluid control based on PIV measurement

¹ School of Energy and Power Engineering, Beihang University, Beijing 100191, People’s Republic of China
² School of Aviation Operations and Services, Aviation University of Air Force, Changchun 130022, People’s Republic of China
³ Air Force Command College, Beijing 100191, People’s Republic of China
⁴ Air Force Harbin Flight Academy, Harbin 150000, People’s Republic of China

Funds: This work was supported by National Natural Science Foundation of China (No. 90716025).

More Information

Received Date: June 28, 2018

Graphical Abstract

Abstract

Abstract

This paper is devoted to experimentally investigating the influence of magnetic field intensity and gas temperature on the plasma jet deflection controlled by magneto hydrodynamics. The catalytic ionization seed CS₂CO₃ is injected into combustion gas by artificial forced ionization to obtain plasma fluid on a high-temperature magnetic fluid experimental platform. The plasma jet was deflected under the effect of an external magnetic field, forming a thrust-vector effect. Magnesium oxide was selected as a tracer particle, and a two-dimensional image of the jet flow field was collected using the particle image velocimetry (PIV) measurement method. Through image processing and velocity vector analysis of the flow field, the value of the jet deflection angle was obtained quantitatively to evaluate the thrust-vector effect. The variation of the jet deflection angle with the magnetic field intensity and gas temperature was studied under different experimental conditions. Experimental results show that the jet deflection angle increased gradually with a rise in gas temperature and then increased substantially when the gas temperature exceeded 2300 K. The jet deflection angle also increased with an increase in magnetic induction intensity. Experiments demonstrate it is feasible to use PIV test technology to study the thrust vector under magnetic control conditions.
- PIV,
- plasma,
- jet deflection,
- MHD,
- image processing

FullText(HTML)

References (20)

References

[1]	Macheret S O, Shneider M N and Miles R B 2004 AIAA J. 42 1378
[2]	Yamaguchi H, Suzuki Y and Shuchi S 2003 J. Thermophys. Heat Transfer 17 89
[3]	Sun B G et al 2010 Plasma Sci. Technol. 12 723
[4]	Li Z M, Hawk C W and Jones J E 2001 Experimental study of a crossed-field MHD accelerator coupling with microwave plasma 37th Joint Propulsion Conf. and Exhibit (Salt Lake City, USA) AIAA 2001 (https://doi.org/10.2514/6. 2001-3495)
[5]	Li Z M, Jones J E and Hawk C W 2000 Experimental study of microwave plasma MHD accelerators 36th AIAA/ ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit (Las Vegas, USA) AIAA 2000 (https://doi.org/10.2514/6. 2000-3882)
[6]	Ohkuma H et al 2008 Performance prediction of scramjet driven dcw mhd generator with three-dimensional analysis 39th Plasmadynamics and Lasers Conf. (Seattle, USA) AIAA 2008 (https://doi.org/10.2514/6.2008-4333)
[7]	Lineberry J T et al 2006 Scramjet driven MHD power demonstration—HVEPS program 37th AIAA Plasmadynamics and Lasers Conf. (San Francisco, USA) AIAA 2006 (https://doi.org/10.2514/6.2006-3080)
[8]	Ganji A R, Khadem M and Khandani S M H 1993 J. Propul. Power 9 153
[9]	Bityurin V A et al 2000 Thermodynamic analysis of the AJAX propulsion concept 38th Aerospace Sciences Meeting and Exhibit Reno (USA) AIAA 2000 (https://doi.org/10.2514/ 6.2000-445)
[10]	Kaminaga S, Tomioka S and Yamasaki H 2005 Feasibility study on MHD energy bypass scramjet engine AIAA/CIRA 13th Int. Space Planes and Hypersonics Systems and Technologies Conf. (Capua, Italy) AIAA 2005 (https://doi. org/10.2514/6.2005-3226)
[11]	Leonov S et al 2002 The features of electro-discharge plasma control of high-speed gas flows 33rd Plasmadynamics and Lasers Conf. (Maui, Hawaii) AIAA 2002 (https://doi.org/ 10.2514/6.2002-2180)
[12]	Roth J et al 2003 Flow re-attachment and acceleration by paraelectric and peristaltic electrohydrodynamic (EHD) effects 41st Aerospace Sciences Meeting and Exhibit Reno (USA) AIAA 2003 (https://doi.org/10.2514/6.2003-531)
[13]	Post M L and Corke T C 2004 Separation control using plasma actuators—stationary & oscillating airfoils 42nd AIAA Aerospace Sciences Meeting and Exhibit (Reno, USA) AIAA 2004 (https://doi.org/10.2514/6.2004-841)
[14]	Roth J R and Dai X 2006 Optimization of the aerodynamic plasma actuator as an electrohydrodynamic (EHD) electrical device 44th AIAA Aerospace Sciences Meeting and Exhibit (Reno, USA) AIAA 2006 (https://doi.org/10.2514/6.2006-1203)
[15]	Corke T C et al 2002 Application of weakly-ionized plasmas as wing flow-control devices 40th AIAA Aerospace Sciences Meeting & Exhibit Reno (USA) AIAA 2002 (https://doi. org/10.2514/6.2002-350)
[16]	Roy S and Gaitonde D V 2005 Multidimensional collisional dielectric barrier discharge for flow separation control at atmospheric pressures 35th AIAA Fluid Dynamics Conf. and Exhibit (Toronto, Canada) AIAA 2005 (https://doi.org/10. 2514/6.2005-4631)
[17]	Murray R C et al 2004 Observation of MHD effects with non-equlibrium ionization in Cold supersonic air flows 42nd AIAA Aerospace Sciences Meeting and Exhibit Reno (USA) AIAA 2004 (https://doi.org/10.2514/6. 2004-1025)
[18]	Adamovich I V et al 2003 Magnetogasdynamic power extraction and flow conditioning for a gas turbine 34th AIAA Plasmadynamics and Laser Conf. (Orlando, USA) AIAA 2003 https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa. gov/20040000981.pdf
[19]	Macheret S O, Shneider M N and Miles R B 1999 MHD power extraction from cold hypersonic air flow with external ionizers 9th Int. Space Planes and Hypersonic Systems and Technologies Conf. (Norfolk, VA, USA) AIAA 1999 (https://doi.org/10.2514/6.1999-4800)
[20]	Zhao K et al 2018 Plasma Sci. Technol. 20 065511

[1]	Jianhua LYU, Chunjie NIU, Yunqiu CUI, Chao CHEN, Weiyuan NI, Hongyu FAN. Automatic recognition of defects in plasma-facing material using image processing technology[J]. Plasma Science and Technology, 2023, 25(12): 125603. DOI: 10.1088/2058-6272/ace9af
[2]	Kai ZHAO (赵凯), Feng LI (李锋), Baigang SUN (孙佰刚), Hongyu YANG (杨宏宇), Tao ZHOU (周韬), Ruizhi SUN (孙睿智). Numerical and experimental investigation of plasma plume deflection with MHD flow control[J]. Plasma Science and Technology, 2018, 20(6): 65511-065511. DOI: 10.1088/2058-6272/aab2a4
[3]	Zhijun WANG (王智君), Xiang GAO (高翔), Tingfeng MING (明廷凤), Yumin WANG (王嵎民), Fan ZHOU (周凡), Feifei LONG (龙飞飞), Qing ZHUANG (庄清), EAST Team. Two-dimensional vacuum ultraviolet images in different MHD events on the EAST tokamak[J]. Plasma Science and Technology, 2018, 20(2): 25103-025103. DOI: 10.1088/2058-6272/aa9477
[4]	ihao TIE (铁维昊), Cui MENG (孟萃), Yuting ZHANG (张雨婷), Zirang YAN (闫自让), Qiaogen ZHANG (张乔根). Analysis on discharge process of a plasma-jet trigered gas spark switch[J]. Plasma Science and Technology, 2018, 20(1): 14009-014009. DOI: 10.1088/2058-6272/aa8cbe
[5]	ZHANG Xiujie (张秀杰), PAN Chuanjie (潘传杰), XU Zengyu (许增裕). MHD Stability Analysis and Flow Controls of Liquid Metal Free Surface Film Flows as Fusion Reactor PFCs[J]. Plasma Science and Technology, 2016, 18(12): 1204-1214. DOI: 10.1088/1009-0630/18/12/11
[6]	GAO Ling (高岭), ZHANG Bailing (张百灵), LI Yiwen (李益文), FAN Hao (樊昊), DUAN Chengduo (段成铎), WANG Yutian (王宇天). Experimental Study of MHD-Assisted Mixing and Combustion Under Low Pressure Conditions[J]. Plasma Science and Technology, 2016, 18(8): 855-859. DOI: 10.1088/1009-0630/18/8/11
[7]	ZHANG Xiaodan(张小丹), HU Chundong(胡纯栋), SHENG Peng(盛鹏), ZHAO Yuanzhe(赵远哲), WU Deyun(吴德云), CUI Qinglong(崔庆龙). The Implementation of Computer Data Processing Software for EAST NBI[J]. Plasma Science and Technology, 2014, 16(10): 984-987. DOI: 10.1088/1009-0630/16/10/15
[8]	XU Ming (徐明), WEN Yizhi (闻一之), XIE Jinlin (谢锦林), YU Changxuan (俞昌旋), et al.. Internal Magnetic Configuration Measured by ECE Imaging on EAST Tokamak[J]. Plasma Science and Technology, 2013, 15(12): 1194-1196. DOI: 10.1088/1009-0630/15/12/05
[9]	M. ANWARI, H. H. QAZI, SUKARSAN, N. HARADA. Numerical Analysis of MHD Accelerator with Non-Equilibrium Air Plasma[J]. Plasma Science and Technology, 2012, 14(12): 1110-1115. DOI: 10.1088/1009-0630/14/12/14
[10]	LI Li(李莉), LIU Yue (刘悦), XU Xinyang(许欣洋), XIA Xinnian(夏新念). The Effect of Equilibrium Current Profiles on MHD Instabilities in Tokamaks[J]. Plasma Science and Technology, 2012, 14(1): 14-19. DOI: 10.1088/1009-0630/14/1/04

Cited By

Cited by

Periodical cited type(5)

1.	Kadhem, S.J.. Enhancing plasma jet parameters control by external magnetic field strength variation. Optical and Quantum Electronics, 2024, 56(7): 1118. DOI:10.1007/s11082-024-07069-0
2.	Hu, J.-C., Chen, Y.-C., Guo, Y.-M. et al. Numerical study of molten salt flow and heat transfer in a pipe applied non-uniform magnetic field. Physics of Fluids, 2024, 36(3): 035115. DOI:10.1063/5.0189476
3.	Zhao, Q., Mao, B., Bai, X. et al. Advances in Electrical Conductivity Calculation Method of Thermal Ionization Plasma. 2021. DOI:10.1109/ICMIMT52186.2021.9476174
4.	ZHAO, K., MING, M., LI, F. et al. Experimental study on plasma jet deflection and energy extraction with MHD control. Chinese Journal of Aeronautics, 2020, 33(6): 1602-1610. DOI:10.1016/j.cja.2020.01.003
5.	Zhao, K., Lu, Y., Li, F. et al. Experimental investigation on the effect of ionization seed mass fraction on gas plasma jet deflection. Acta Astronautica, 2020. DOI:10.1016/j.actaastro.2020.03.003

Other cited types(0)

Get Citation

PDF

XML

Article views (110) PDF downloads (327) Cited by(5)

Turn off MathJax

Article Contents

Abstract

References

Experimental investigation on plasma jet deflection with magnetic fluid control based on PIV measurement