Volume 47 Issue 1
Feb.  2017
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LI Yiwen, ZHANG Bailing, LI Yinghong, XIAO Lianghua, WANG Yutian, HE Guoqiang. Applications and prospects of magnetohydrodynamics in aeronautical engineering[J]. Advances in Mechanics, 2017, 47(1): 452-502. doi: 10.6052/1000-0992-16-036
Citation: LI Yiwen, ZHANG Bailing, LI Yinghong, XIAO Lianghua, WANG Yutian, HE Guoqiang. Applications and prospects of magnetohydrodynamics in aeronautical engineering[J]. Advances in Mechanics, 2017, 47(1): 452-502. doi: 10.6052/1000-0992-16-036

Applications and prospects of magnetohydrodynamics in aeronautical engineering

doi: 10.6052/1000-0992-16-036
  • Received Date: 2016-11-02
    Available Online: 2017-01-24
  • Publish Date: 2017-02-24
  • This article reviews the applications of magnetohydrodynamics in aeronauti-cal engineering, including magnetohydrodynamic (MHD) combined ramjet, MHD combined turbine engine, post combustion chamber MHD power generation, surface MHD power gen- eration, MHD acceleration wind tunnel, MHD thrust-vectoring, large-size MHD flow control, boundary layer separation flow control, boundary layer transition control, and air vehicle head heat flow control. In addition, this article discusses the key scientific and techni-cal problems in MHD applications, and analyzes the conductive fluid generation, MHD experimental equipment and experimental technology, multi-field coupling mechanism and numerical simulation methods. At last, this article reviews and envision the applications of MHD in aeronautical engineering.

     

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  • [1]
    鲍文, 唐井峰, 于达仁. 2007. MHD_Arc_Ramjet 联合循环与AJAX 间的性能比较. 宇航学报, 28: 157-161 https://www.researchgate.net/publication/289056951_Comparative_analysis_about_performance_between_MHD-Arc-Ramjet_combined_cycle_and_AJAX
    [2]
    Bao WTang J F, Yu D R. 2007. Comparative analysis about performance between MHD-Arc-Ramjet combined cycle and AJAX. Journal of Astronautics, 28: 157-161. https://www.researchgate.net/publication/289056951_Comparative_analysis_about_performance_between_MHD-Arc-Ramjet_combined_cycle_and_AJAX
    [3]
    樊昊, 张百灵, 李益文, 阳鹏宇, 高岭, 张义宁. 2015.超声速非平衡电离磁流体动力技术实验系统. 航空动力学报, 8:2025-2032 http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201508030.htm
    [4]
    Fan H, Zhang B L, Li Y W, Gao L, Zhang Y N. 2015.Supersonic non-equilibrium ionization magnetohydrodynamic technical experimental system. Journal of Aerospace Power, 8: 2025-2032. http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201508030.htm
    [5]
    樊昊. 2015. 超声速非平衡电离磁流体流动控制原理研究.[硕士论文]. 西安: 空军工程大学
    [6]
    Fan H. 2015. Principle study of supersonic MHD flow control wit nonequilibrium ionization. [Master Thesis]. Xi'an: Air Force Engineering University.
    [7]
    范月华, 蒋崇文, 高振勋, 李椿萱. 2016.磁流体湍流及数值模拟研究综述. 力学与实践, 38: 14-21 http://www.cnki.com.cn/Article/CJFDTOTAL-LXYS201601004.htm
    [8]
    Fan Y H, Jiang C W, Gao Z X, Li C X. 2016. Review of the magneto hydrodynamic turbulence and its numerical simulation. Mechanics in Engineering, 38: 14-21. http://www.cnki.com.cn/Article/CJFDTOTAL-LXYS201601004.htm
    [9]
    高岭, 李益文, 张百灵, 阳鹏宇, 樊昊, 段成铎, 向波罗. 2015.高温磁流体动力技术实验系统设计与调试. 推进技术, 35: 774-779 http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201505018.htm
    [10]
    Gao L, Li Y W, Zhang B L, Yang P Y, Fan H, Duan C D, Xiang B L.2012. High temperature MHD technology system design and commissioning experiments. Journal of Propulsion Technology, 35: 774-779. https://www.researchgate.net/publication/283228727_High_temperature_MHD_technology_system_design_and_commissioning_experiments
    [11]
    姜宗林, 李进平, 赵伟, 刘云峰, 俞鸿儒. 2012.长试验时间爆轰驱动激波风洞技术研究.力学学报, 44: 824-831 http://www.cnki.com.cn/Article/CJFDTOTAL-LXXB201205004.htm
    [12]
    Jiang Z L, Li J P, Zhao W, Liu Y F, Yu H R. 2012. Investigating into techniques for extending the test-duration of detonation-driven shock tunnels. Chinese Journal of Theoretical and Applied Mechanics, 44: 824-831. http://en.cnki.com.cn/Article_en/CJFDTOTAL-LXXB201205004.htm
    [13]
    解少飞, 杨武兵, 沈清. 2015.高超声速边界层转捩机理及其应用的若干进展回顾. 航空学报, 36:714-723 http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201503002.htm
    [14]
    Xie S F, Yang W B, Shen Q. 2015. Review of progresses in hypersonic boundary layer transition mechanism and its applications. Acta Aeronautica Et Astronautica Sinica, 36: 714-723. https://www.researchgate.net/publication/282303647_Review_of_progresses_in_hypersonic_boundary_layer_transition_mechanism_and_its_applications
    [15]
    居滋象, 吕友昌, 荆伯弘. 1998. 开环磁流体发电. 北京:北京工业大学出版社
    [16]
    Ju Z X, Lv Y C, Jing B H. 1998. Open Cycle MHD Power. Beijing: Beijing Industrial University Press.
    [17]
    李桦, 田正雨. 2010.高超声速流动磁流体力学控制的数值模拟研究. 长沙: 国防科技大学出版社
    [18]
    Li H, Tian Z Y. 2010. Numerical Investigation for Hypersonic Flow Control by Magnetohydrodynamics Methods. Changsha: National University of Defense Technology Press.
    [19]
    李建, 赵凌志, 刘保林, 彭燕, 沙次文, 许玉玉, 李然. 2010.一种阀式磁流体波浪能直接发电系统的研究. 机床与液压, 38:38-49 http://www.cnki.com.cn/Article/CJFDTOTAL-JCYY201016017.htm
    [20]
    Li J, Zhao L Z, Liu B L, Peng Y, Sha C Y, Xu Y Y, Li R.2010. Research on valve-type liquid metal magnetohydrodynamic ocean wave energy conversion system. Machine Tool & Hydraulics, 38: 38-49. https://www.researchgate.net/publication/269378894_Research_on_New_Type_Magnetohydrodynamic_Ocean_Wave_Energy_Conversion_System
    [21]
    李益文, 李应红, 张百灵, 陈峰, 朱涛. 2012.超声速气流磁流体加速初步实验研究. 力学学报, 44: 238-244 http://www.cnki.com.cn/Article/CJFDTOTAL-LXXB201202008.htm
    [22]
    Li Y W, Li Y H, Zhang B L, Chen F, Zhu T. 2012. Preliminary experimental investigation on supersonic flow magnetohydrodynamic MHD) acceleration. Chinese Journal of Theoretical and Applied Mechanics, 44: 238-244. https://www.researchgate.net/publication/290016069_Preliminary_experimental_investigation_on_supersonic_flow_MagnetohydrodynamicMHD_acceleration
    [23]
    李益文, 李应红, 张百灵, 金迪, 陈峰, 朱涛. 2011.基于激波风洞的超声速磁流体动力技术实验系统. 航空学报, 32:1015-1024 http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201106008.htm
    [24]
    Li Y W, Li Y H, Zhang B L, Jin D, Chen F, Zhu T. 2011.Supersonic magnetohydrodynamic technical experimental system based on shock tunnel. Acta Aeronautica et Astronautica Sinica, 32: 1015-1024. https://www.researchgate.net/publication/286988361_Supersonic_magnetohydrodynamic_technical_experimental_system_based_on_shock_tunnel
    [25]
    李益文, 张百灵, 李应红, 樊昊, 高岭, 段成铎, 王宇天. 2015.磁流体技术在冲压发动机中的应用研究//第五届全国冲压发动机会议, 厦门
    [26]
    Li Y W, Zhang B L, Li Y H, Fan H, Gao L, Duan C D, Wang Y T. 2015. Application investigation of MHD technology on cramjet engine// The fifth national cranjet engine conference)
    [27]
    李益文, 张百灵, 肖良华, 王宇天. 2016.进气道磁流体流动控制及其研究进展南京会议//第九届全国流体力学学术会议南京
    [28]
    Li Y W, Zhang B L, Xiao L H, Wang Y T. 2016. Inlet MHD flow control and its research progress//CSTAM 2016, Nanjing.
    [29]
    李益文. 2011. 高超声速飞行磁流体动力技术原理研究.[博士论文]. 西安: 空军工程大学
    [30]
    Li Y W. 2011. Theory investigation of MHD technology for hypersonic flight. [PhD Thesis]. Xi'an: Air Force Engineering University.
    [31]
    卢新培, 严萍, 任春生, 邵涛. 2011.大气压脉冲放电等离子体的研究现状与展望. 中国科学: 物理学 力学天文学, 41: 801-815 http://www.cnki.com.cn/Article/CJFDTOTAL-JGXK201107002.htm
    [32]
    Lu X P, Yan P, Ren C S, Shao T. 2011.Review on atmospheric pressure pulsed DC discharge. Scientia Sinica Physica, Mechanica & Astronomica, 41: 801-815. https://www.researchgate.net/publication/252889620_Review_on_atmospheric_pressure_pulsed_DC_discharge
    [33]
    罗纪生. 2015. 高超声速边界层的转捩及预测. 航空学报, 36: 357-372 http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201501027.htm
    [34]
    Luo J S. 2015. Transition and prediction for hypersonic boundary layers. Acta Aeronautica et Astronautica Sinica, 36: 357-372. https://www.researchgate.net/publication/282982891_Transition_and_prediction_for_hypersonic_boundary_layers
    [35]
    吕浩宇, 李椿萱, 曹德一. 2008.乘波构型飞行器磁流体进气道一体化概念设计. 北京航空航天大学学报, 34: 1130-1134 http://www.cnki.com.cn/Article/CJFDTOTAL-BJHK200810003.htm
    [36]
    LüH Y. Li C X, Cao D Y. 2008. Conceptual study on integrated design of airframe/mhd bypass scramjet for a waverider-based hypersonic vehicle. Journal of Beijing University of Aeronautics and Astronautics, 34: 1130-1134. http://en.cnki.com.cn/Article_en/CJFDTOTAL-LXXB200803003.htm
    [37]
    南和礼 著. 2007. 超导磁体设计基础. 北京: 国防工业出版社
    [38]
    Nan H L. 2007. Basis of Superconducting Magnet Design. Beijing: National defence Industry press.
    [39]
    苏纬仪, 陈立红, 张新宇. 2010.MHD控制激波诱导湍流边界层分离的机理分析. 推进技术, 31: 18-23 http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201001004.htm
    [40]
    Su W Y, Chen L H, Zhang X Y. 2010. Investigation of magnetohydrodynamic control on turbulent boundary layer separation induced by shock wave. Journal of Propulsion Technology, 31: 18-23. https://www.researchgate.net/publication/290656268_Investigation_of_magnetohydrodynamic_control_on_turbulent_boundary_layer_separation_induced_by_shock_wave
    [41]
    苏纬仪, 张新宇, 张垄元. 2011.洛仑兹力控制高超声速进气道边界层分离的数值模拟. 推进技术, 32: 36-41 http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201101009.htm
    [42]
    Su W Y, Zhang X Y, Zhang L Y. 2011. Numerical investigation of Lorentz force control on hypersonic inlet boundary layer separation. Journal of Propulsion Technology, 32: 36-41. https://www.researchgate.net/publication/290560239_Numerical_investigation_of_Lorentz_force_control_on_hypersonic_inlet_boundary_layer_separation
    [43]
    苏长兵. 2010. 高超声速磁流体流动控制技术原理研究.[博士论文]. 西安: 空军工程大学
    [44]
    Su C B. 2010. Technical principle research of hypersonic MHD flow control. [PhD Thesis]. Xi'an: Air Force Engineering University.
    [45]
    田正雨, 张康平, 潘沙, 李桦. 2008.磁流体动力学斜激波控制数值模拟分析. 力学季刊, 29: 72-77 http://www.cnki.com.cn/Article/CJFDTOTAL-SHLX200801012.htm
    [46]
    Tian Z Y, Zhang K P, Pan S, Li H. 2008. Numerical investigation and analysis for MHD oblique shock control. Chinese Quarterly of Mechanics, 29: 72-77. doi: 10.2514/6.2011-3427
    [47]
    田正雨. 2008. 高超声速流动的磁流体力学控制数值模拟研究.[博士论文]. 长沙: 国防科学技术大学
    [48]
    Tian Z Y. 2008. Numerical investigation for hypersonic flow control by magnetohydrodynamics methods. [PhD Thesis]. Changsha: National University of Defense Technology.
    [49]
    王健, 李应红, 程邦勤, 苏长兵, 宋慧敏, 吴云. 2009.等离子体气动激励控制激波的机理研究. 物理学报, 58: 5513-5519 http://www.cnki.com.cn/Article/CJFDTOTAL-WLXB200908058.htm
    [50]
    Wang J, Li Y H, Cheng B Q, Su C B, Song H M, Wu Y. 2009. The mechanism investigation on shock wave controlled by plasma aerodynamic actuation. Acta Physica Sinica, 58:5513-5519. http://en.cnki.com.cn/Article_en/CJFDTotal-WLXB200908058.htm
    [51]
    吴根, 姜宗林, 罗凡. 2014.空天飞行器先进风洞实验技术及我国发展建议. 中国基础科学, 12-16 http://www.cnki.com.cn/Article/CJFDTOTAL-ZGJB201401002.htm
    [52]
    Wu G, Jiang Z L, Luo F. 2014. Advanced wind tunnel testing techniques of aerospace vehicle and suggestions for its future development in China. China Basic Science, 12-16.
    [53]
    吴其芬, 李桦. 2007. 磁流体力学. 长沙: 国防科技大学出版社
    [54]
    Wu Q F, Li H. 2007. Magneto-fluid mechanics. Changsha: National University of Defense Technology Press.
    [55]
    阳鹏宇. 2014. 超声速非平衡等离子体产生及磁流体功率提取研究.[硕士论文]. 西安: 空军工程大学
    [56]
    Yang P Y. 2014. supersonic nonequilibrium plasma produce and MHD power generation. [Master Thesis]. Xi'an: Air Force Engineering University.
    [57]
    于达仁, 唐井峰, 鲍文. 2007.用于高超声速推进的MHD-Arc-Ramjet联合循环. 航空学报, 28:769-775 http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB200704002.htm
    [58]
    Yu D R, Tang J F, Bao W. 2007. MHD-arc-ramjet combined cycle for hypersonic propulsion. Acta Aeronautica et Astronautica Sinica, 28: 769-775. https://www.researchgate.net/publication/282675534_MHD-arc-ramjet_combined_cycle_for_hypersonic_propulsion
    [59]
    章程, 邵涛, 严萍. 2014. 大气压下纳秒脉冲弥散放电. 科学通报, 59: 1919-1926 http://www.cnki.com.cn/Article/CJFDTOTAL-KXTB201420003.htm
    [60]
    Zhang C, Shao T, Yan P. 2014.Nanosecond-pulse diffuse discharges at atmospheric pressure. Chinese Science Bulletin, 59: 1919-1926. doi: 10.1360/N972014-00003
    [61]
    郑小梅, 吕浩宇, 徐大军, 蔡国飙. 2010.MHD加速器模式磁控进气道的优化设计. 航空学报, 31: 223-230 http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201002004.htm
    [62]
    Zheng X M, Lü H Y, Xu D J, Cai G B. 2010. Optimization of accelerator mode mhd controlled inlet. Acta Aeronautica et Astronautica Sinica, 31: 223-230. http://www.wenkuxiazai.com/doc/c12e6bfa941ea76e58fa04dc.html
    [63]
    Aleksandrov, N L, Kirpichnikov A A, Kindusheva S V, Kosarev I N, Starikovskii A Yu. 2007. Non-equilibrium plasma life time measurements and flow control. AIAA Paper 2007-997.
    [64]
    Alferov V I. 2000. Current status and potentialities of wind tunnels with MHD acceleration. High Temperature, 38: 300-313. doi: 10.1007/BF02755960
    [65]
    Anderson R W, Brown G L, Miles R B. 2000. Performance models and predications for the RDHWT/MARIAH Hypersonic wind tunnel. AIAA Paper 2000-2274.
    [66]
    Bityurin V A, Bocharov A N, Baranov D S, Bychkov S SKrasilnikov A V, Knotko V A, Lineberry J T. 2006. Study of MHD flow control and on-board electrical power generation. AIAA Paper 2006-1008.
    [67]
    Bityurin V A, Bocharov A N, Krasilnikov A V, Mikhailov A V.2003. Experimental study of MHD electrical power generation. AIAA Paper 2003-0377.
    [68]
    Bityurin V A, Lineberry J T, Litchford R J, Cole J W. 2000. Thermodynamic analysis of the ajax propulsion concept (invited.AIAA Paper 2000-0445.
    [69]
    Bityurin V A, Zeigarnik V A, Kuranov A L. 1996. On a perspective of MHD technology in aerospace applications. AIAA Paper 96-2355.
    [70]
    Bityurin V A. 2000. A feasibility study and experimental evaluation on MHD acceleration for application to advanced propulsion and hypervelocity ground testing. AIAA Paper 2000-2301.
    [71]
    Blankson I M, Schneider S. 2003. Hypersonic engine using MHD energy bypass with a conventional turbojet. AIAA Paper 2003-6922.
    [72]
    Bobashev S V, Erofeev A V, Lapushkina T A, Zhukov B GPoniaev S A, Vasil'eva R V, Van Wie D M. 2006. Air plasma produced by gas discharge in supersonic MHD channel. AIAA Paper 2006-1373.
    [73]
    Bobashev S V, Golovachov Y P, Van Wie D M. 2002.Deceleration of supersonic plasma flow by an applied magnetic field. AIAA Paper 2002-2247.
    [74]
    Bobashev S V, Mende N P, Sakharov V A, Van Wie D M. 2003. MHD control of the separation phenomenon in a supersonic xenon plasma flow. AIAA Paper 2003-168.
    [75]
    Bogdanoff D W, Mehta U B. 2003. Experimental demonstration of magnetohydrodynamic (MHD) acceleration. AIAA Paper 2003-4285.
    [76]
    Bush W B. 1958. Magnetohydrodynamic-hypersonic flow pass a blunt body. Journal of Aero/Space Science, 25: 685-690, 728. doi: 10.2514/8.7845
    [77]
    Chapman J N, Ruoff R S, Dikin D A, Litchford R J, Schmidt H J. 2003. Flightweight magnets for space application using carbon nanotubes. AIAA Paper 2003-0330.
    [78]
    Chase R L, Boyd D R, Czysz D P, et al. 1998. An AJAX technology advanced SSTO design concept. AIAA Paper 98-5527.
    [79]
    Chase R L, Mehta U B, Bogdanoff D W, Park C, Lawrence S LAftosmis M J, Macheret S, Shneider M. 1999. Comments on MHD energy bypass engine powered spaceliner. AIAA Paper 99-4975.
    [80]
    Demetriades S T, Ziemer R W. 1962. Energy transfer to plasmas by continuous Lorentz forces//Proceedings of the Fourth Biennial Gas Dynamics Symposium. Cambel A B, Anderson T P, Slawsky M. M. (eds.), Northwestern University Press, Evanston, Illinois, 185-205.
    [81]
    Deng Z T, Qian X Q, Litchford R, Foote J. 2011. Date analysis of electromagnetic shockwave control experiment for high mach number ionized flow application. AIAA Paper 2011-3465.
    [82]
    Falempin F, Firsov A A, Yarantsev D A, Goldfeld M ATimofeev K, Leonov S B. 2015. Plasma control of shock wave configuration in off design mode of M=2 inlet. Exp Fluids, 56: 54, DOI10.1007/s00348-015-1928-4. doi: 10.2514/6.2013-3115
    [83]
    Fujino T, Sugita H, Mizuno M, Funaki I, Ishikawa M. 2006.Influences of electrical conductivity of wall on magnetohydrodynamic control of aerodynamic heating. Journal of Spacecraft and Rockets, 43: 63-70. doi: 10.2514/1.13770
    [84]
    Gordeev V P, Krasilnikov A V, Lagutin V I, Otmennikov V N. 1996. Experimental study of the possibility of reducing supersonic drag by employing plasma technology. Fluid Dynamics, 31: 313-317. doi: 10.1007/BF02029693
    [85]
    Gotoh D, Takahashi T, Fujino T, Ishikawa M, Lineberry J T. 2007. Computational analysis of HVEPS scramjet MHD power generation. AIAA Paper 2007-4015.
    [86]
    Gurijanov E P, Harsha P T. 1996. AJAX: new directions in hypersonic technology. AIAA Paper 96-4609.
    [87]
    Harada N. 2001. MHD acceleration studies at Nagaoka University of Technology. AIAA Paper 2001-2744. Jp aerospace. 2014. Year 2010 review in picture [OL].http://www.jpaerospace.com.
    [88]
    Kalra C S, Shneider M N, Miles R B. 2009. Numerical study of boundary layer separation control using magnetogasdynamic plasma actuators. Physics of Fluids (1994-present), 21: 443-451. https://www.researchgate.net/profile/MN_Shneider/publication/252229407_Numerical_study_of_boundary_layer_separation_control_using_magnetogasdynamic_plasma_actuators/links/564fe96808ae1ef9296ed656.pdf?origin=publication_list
    [89]
    Kalra C S, Zaidi S H, Alderman B J, Miles R B. 2007. Non-thermal control of shock-wave induced boundary layer separation using magneto-hydrodynamics. AIAA Paper 2007-4138.
    [90]
    Kalra C, Zaidi S H, Alderman B J, Miles R B, Murty Y V. 2007. Magnetically driven surface discharges for shock-wave induced boundary-layer separation control. AIAA Paper 2007-222.
    [91]
    Kaminaga S, Okuno Y, Yamasaki H. 2003. Quasi-one dimensional analysis on MHD energy bypass scramjet engine performance. AIAA Paper 2003-4286.
    [92]
    Kimmel R L. 2003. Aspects of hypersonic boundary-layer transition control. AIAA Paper 2003-772.
    [93]
    Kovalev L K, Larionoff A E, Poltavets V N, Kovalev K L. 1992. Theoretical and experimental studies of faraday multipole MHD generators//The 11th International Conference On MHD Electrical power Generation, China.
    [94]
    Murakamia T, Okuno Y. 2008. Experiments and numerical simulations on high-density magnetohydrodynamic electrical power generation. Journal of Applied Physics, 104: 063307. doi: 10.1063/1.2978190
    [95]
    Kuranov A L, Sheikin E G. 2002. MHD control on hypersonic aircraft under "Ajax" concept. Possibilities of MHD Generator. AIAA Paper 2002-0490.
    [96]
    Kuranov A L, Sheikin E G. 2003a. MHD control by external and internal flows in scramjet under "AJAX" concept. AIAA Paper 2003-0173.
    [97]
    Kuranov A L, Sheikin E G. 2003b. Magnetohydrodynamic Control on hypersonic Aircraft under "AJAX" concept. Journal of Spacecraft and Rockets, V40:174-182. https://www.researchgate.net/publication/245438057_Magnetohydrodynamic_Control_on_Hypersonic_Aircraft_Under_Ajax_Concept
    [98]
    Lee C H, Lu H Y. 2007. Quasi-One-Dimensional Parametric Study for MHD generator in MHD bypass scramjet system. AIAA Paper 2007-644.
    [99]
    Leonov S B, Firsov A A, Yarantsev D A, Falempin F, Miller A. 2012. Flow control in a supersonic inlet model by electrical discharge. Progress in Flight Physics, 3: 557-568.
    [100]
    Leonov S B, Yarantsev D A, Dmitry A, Gromov V G, Kuriachy A P. 2005. Mechanisms of flow control by near-surface electrical discharge. AIAA Paper 2005-0780.
    [101]
    Leonov S B, Yarantsev D A. 2008. Near-surface electrical discharge in supersonic airflow: properties and flow control.Journal of Propulsion and Power, 24: 1168-1181. doi: 10.2514/1.24585
    [102]
    Lineberry J T, Begg L L, Castro J H, Litchford R J. 2006. Scramjet driven MHD power demonstration-HVEPS program. AIAA Paper 2006-3080.
    [103]
    Lineberry J T, Begg L L, Castro J H, Litchford R J, Donohue J M. 2006. Scramjet driven MHD power demonstration-HVEPS project overview. AIAA Paper 2006-8010.
    [104]
    Lineberry J T, Begg L L, Castro J H, Litchford R J, Donohue J M. 2007. HVEPS scramjet-driven MHD power demonstration test results. AIAA Paper 2007-3880.
    [105]
    Lipinski R L, Nelson G L, Pena G E, Reed K W. 1999. Electron beam-induced conductivity experiments in a static cell for application to MHD accelerators. AIAA Paper 1999-3719.
    [106]
    Litchford R J, Cole J W, Bityurin V A, Lineberry J T. 2001. Thermodynamic analysis of magnetohydrodynamic-bypass hypersonic airbreathing engines. Journal of Propulsion and Power, 17: 477-480. doi: 10.2514/2.5769
    [107]
    Litchford R J, Cole J W, Lineberry J T, Chapman J NSchmidt H J, Lineberry C W. 2002. Magnetohydrodynamic augmented propulsion experiment: i. performance analysis and design. AIAA Paper 2002-2184.
    [108]
    Macheret S O, Shneider M N, Miles R B. 2001. Energy-efficient generation of non-equilibrium plasmas and their applications to hypersonic MHD systems. AIAA Paper 2001-2880.
    [109]
    Macheret S O, Shneider M N, Miles R B. 2002. MHD power extraction from cold hypersonic air flow with external ionizers. Journal of Propulsion and Power, 18: 424-431. doi: 10.2514/2.5951
    [110]
    Macheret S O, Shneider M N, Miles R B. 2003. Scramjet inlet control by off-body energy addition: a virtual cowl. AIAA Paper 2003-0032.
    [111]
    Macheret S O, Shneider M N, Miles R B. 2004. Magnetohydrodynamic and electrohydrodynamic control of hypersonic flows of weakly ionized plasmas. AIAA Journal, 42: 1378-1387. doi: 10.2514/1.3971
    [112]
    Macheret S O, Shneider M N, Murray R C, Zaidi S H, Vasilyak L M, Miles R B. 2004. RDHWTMARIAH II MHD modeling and experiments review. AIAA Paper 2004-2485.
    [113]
    Mikhail N S, Sergey O M. 2005. Hypersonic aerodynamic control and thrust vectoring by nonequilibrium cold-air MHD devices. AIAA Paper 2005-979.
    [114]
    Miles R B, Macheret S O, Shneider M N, Steeves C, Murray R C, Smith T, Zaidi S H. 2005. Plasma-enhanced hypersonic performance enabled by MHD power extraction. AIAA Paper 2005-0561.
    [115]
    Miles R, Brown G, Lempert W, Narelson D, Yetter R, Guest JWilliams G, Bogonoff S. 1994. Radiatively driven hypersonic wind tunnel. AIAA Paper 1994-2472.
    [116]
    Moeller T, Robert R, Lineberry J T, Begg L L, Litchford R J. 2008. HVEPS combustion driven MHD power demonstration tests. AIAA Paper 2008-4097.
    [117]
    Murakami T, Okuno Y. 2008. High-performance nonequilibrium-plasma magnetohydrodynamic electrical power generator using slightly divergent channel configuration: II.experimental. Journal of Physics D : Applied Physics, 41: 125212. doi: 10.1088/0022-3727/41/12/125212
    [118]
    Murray R C, Zaidi S H, Carraro M R, Vasilyak L M; Macheret S O, Shneider M N, Miles R B. 2006. Magnetohydrodynamic power generation using externally ionized, cold, supersonic air as working fluid. AIAA Journal, 44: 119-127. doi: 10.2514/1.11611
    [119]
    Neuringer J L, Mcillroy W. 1958. Incompressible two-dimensional stagnation-point flow of an electrically conducting viscous fluid in the presence of a magnetic field. Journal of Aeronautical Sciences, 25: 194-198. https://www.researchgate.net/profile/Janamejay_Singh/publication/253649026_Numerical_Solution_of_Two-Dimensional_MHD_Forward_Stagnation-Point_Flow_in_the_Presence_of_Hall_Current/links/0c96051f9f41435818000000.pdf?origin=publication_detail
    [120]
    Nishihara M, Bruzzese J, Adamovich I V. 2007. Experimental and computational studies of low-temperature M=4 Flow deceleration by lorentz force. AIAA Paper 2007-4595.
    [121]
    Nishihara M, Jiang N B, Rich J W, Lempert W R, Adamovich I V. 2005. Low-temperature supersonic boundary layer control using repetitively pulsed MHD forcing. AIAA Paper 2005-5178.
    [122]
    Nishihara M, Rich J W, Lempert W R, Adamovich I V. 2006a. Low-temperature M=3 flow deceleration by Lorentz force. Physics of Fluids, 18: 1-11.
    [123]
    Nishihara M, Rich J W, Lempert W R, Adamovich I V. 2006b. MHD flow control and power generation in low-temperature supersonic flows. AIAA Paper 2006-3076.
    [124]
    Nishihara M, Rich J W, Lempert W R, Adamovich I V. 2006c. Low-temperature M=3 flow deceleration by Lorentz force. AIAA Paper 2006-1004.
    [125]
    Pai D, Lacoste D, Laux C. 2010. Transitions between coronaglow and spark regimes of nanosecond repetitively pulsed discharges in air at atmospheric pressure. J Appl Phys, 107: 093303. doi: 10.1063/1.3309758
    [126]
    Ramon L C, Unmeel B M, David W B, Scott L L, Michael J AMacheret S, Shneider M. 1999. Comments on MHD energy bypass engine powered spaceliner. AIAA Paper 99-4975.
    [127]
    Resler E L, Sears W R. 1958. The prospects for magneto-aerodynamics. Journal of the Aeronautical Sciences, 25: 235-245. https://www.researchgate.net/publication/285421077_The_Prospects_for_Magneto-Aerodynamics
    [128]
    Rhodes R, Moeller T, Dennis K. 2012. Electrical conductivity measurements via a low-voltage conductivity channel. IEEE trans. on plasma sci, 40: 972-979. doi: 10.1109/TPS.2012.2185813
    [129]
    Ring L E, Brown G L, Girgis I G, Schneider L X, Lofftus D A. 2002. RDHWT/MARIAH II Program: Facility Performance and System Integration Issues. AIAA Paper 2002-3126.
    [130]
    Ring L E. 1964. General considerations of MHD acceleration for aerodynamic testing. Arc heaters and MHD accelerators for aerodynamic purposes, AGARDograph 84: Supplemental VolumeProceedings of AGARD Specialists Meeting, North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development. Sept, 1964.
    [131]
    Romig M F. 1964. The influence of electric and magnetic fields on heat transfer to electrically conducting fluid. Advances in Heat Transfer, 1: 267-354. doi: 10.1016/S0065-2717(08)70100-X
    [132]
    Sheikin E G, Kuranov A L. 2004. Scramjet with MHD bypass under "AJAX" concept. AIAA Paper 2004-1192.
    [133]
    Shneider M N, Macheret S O, Miles R B. 2003. Comparative analysis of MHD and plasma methods of scramjet inlet control. AIAA Paper 2003-170.
    [134]
    Shneider M N, Macheret S O. 2006. Modeling of plasma virtual shape control of ram/scramjet inlet and isolator. Journal of Propulsion and Power, 22: 447-454. doi: 10.2514/1.16959
    [135]
    Simmons G A, Nelson G L, Ossello C A. 1998. Electon attachment in seeded air for hypervelocity MHD accelerator propulsion wind tunnel applications. AIAA Paper 1998-3133.
    [136]
    Su C B, Li Y H, Cheng B Q, Wang J, Cao J, Li Y W. 2010. Experimental investigation of MHD flow control for the oblique shock wave around the ramp in low-temperature supersonic flow. Chinese Journal of Aeronautics, 22: 22-32. https://www.researchgate.net/publication/222340403_MHD_Flow_Control_of_Oblique_Shock_Waves_Around_Ramps_in_Low-temperature_Supersonic_Flows
    [137]
    Sun Q, Cheng B Q, Li Y H, Kong W S, Li J, Zhu Y F, Jin D. 2013. Computational and experimental analysis of Mach 2 air flow over a blunt body with plasma aerodynamic actuation. Science in China - Series E : Technological Sciences, 56: 795-802. doi: 10.1007/s11431-013-5177-6
    [138]
    Takeshita S, Buttapeng C, Harada N. 2008. The effects of swirl vane for disk MHD accelerator. AIAA Paper 2008-1100.
    [139]
    Tang J F, Bao W, Yu D R. 2006. The influence of energy-bypass on the performance of AJAX. AIAA Paper 2006-1376.
    [140]
    Tomoyuki M, Yoshihiro O. 2008. Experiments and numerical simulations on high-density magnetohydrodynamic electrical power generation.Journal of Applied Physics, 104, 063307. doi: 10.1063/1.2978190
    [141]
    Udagawa K, Gorbatov S, Pliavaka F, Nishihara M, Adamovich I V. 2008. Experimental Study of a fast ionization wave discharge at high pulse repetition rates. AIAA Paper 2008-1104.
    [142]
    Vanwie D M, Nedungadi A. 2004. Plasma Aerodynamic Flow Control for Hypersonic Inlets. AIAA Paper 2004-4129.
    [143]
    Wang J, Li Y H, Xing F. 2009a. Investigation on oblique shock wave control by arc discharge plasma in supersonic airflow. Journal of Applied Physics, 106: 073307. doi: 10.1063/1.3236658
    [144]
    Wang J, Li Y H, Cheng B Q, Su C B, Song H M, Wu Y. 2009b. Experimental investigation on shock wave control by plasma aerodynamic actuation. AIAA Paper 2009-3618.
    [145]
    Wang J, Li Y H, Cheng B Q, Su C B, Song H M, Wu Y. 2009c. Effects of plasma aerodynamic actuation on oblique shock wave in a cold supersonic flow. Journal of Physics D : Applied Physics, 42: 165503. doi: 10.1088/0022-3727/42/16/165503
    [146]
    Wang J, Li Y H, Cheng B Q, Su C B, Song H M, Wu Y. 2009d. Mechanism investigation on shock wave control by plasma aerodynamic actuation. AIAA Paper 2009-4286.
    [147]
    Wilson C R, Laster M L, Jordan J L, Limbaugh C. 2004. Plans and status of the RDHWT/MARIAH II facility research program. AIAA Paper 2004-2479.
    [148]
    Wood G P, Carter A F. 1960. Considerations in the design of a steady DC plasma accelerator. Proceedings of the Third Biennial Gas Dynamics Symposium, Cambel A. B. Fenn J. B. (eds.)Northwestern University Press, Evanston, Illinois, 1960: 201-212.
    [149]
    Wood G P, Carter A F, Sabol A P. 1964. Research on Linear Crossed-Field Steady-Flow D.C. Plasma accelerators at langley research center, nasa. arc heaters and MHD accelerators for aerodynamic purposes, AGARDograph 84: Part I, Proceedings of AGARD Specialists Meeting, North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, Sept, 1-45.
    [150]
    Yang P Y, Zhang B L, Li Y W, Wang Y T, Duan C D. 2016. Investigation of MHD power generation with supersonic non-equilibrium RF discharge. Chinese Journal of Aeronautics, 29: 863-873.
    [151]
    Zaidi S H, Smith T, Macheret S, Miles R B. 2006. Snowplow surface discharge in magnetic field for high speed boundary layer control. AIAA Paper 2006-1006.
    [152]
    Zhukov V P, Kindisheva S V, Kirpichnikov A A, Kosarev I NStarikovskaia S M, Starikovskii A Yu, Kelley, J D. 2006. Plasma production for MHD power generation by nanosecond discharge. AIAA Paper 2006-1370.
    [153]
    Ziemer R W, Bush W B. 1958. Magnetic field effects on bow shock stand-off distance. Phys. Rev. Lett, 1: 58-59. doi: 10.1103/PhysRevLett.1.58
    [154]
    Ziemer W. 1959. Experimental investigation in magneto-aerodynamics. American Rocket Society Journal, 29: 642-647.
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