| [1]李开. 高温真实气体条件下的磁控热防护机理研究[D]. 长沙: 国防科学技术大学, 2017.LI K. Magnetohydrodynamic Heat Shield System Including High Temperature Real Gas Effect [D]. Changsha: National University of Defense and Technology, 2017(in Chinese).[2]MacCormack R W. Evaluation of the low magnetic reynolds approximation for aerodynamic flow calculations[R]. AIAA 2005-4780. Reston: AIAA, 2005.[3]陈雄, 郑亚, 周长省等. 冲压增程弹丸进气道复杂湍流流场数值仿真[J]. 兵工学报, 2005, 26(3): 303~307.CHEN Xiong, ZHENG Ya, ZHOU Chang-sheng, et al. Numerical Simulation on the Inlet Complex Turbulent Flow ofRamjet Assisted Range Projectiles[J]. Acta Armamentarii, 2005, 26(3): 303~307.[4]苏纬仪,张新宇,张堃元. 洛仑兹力控制高速进气道边界层分离的数值模拟[J]. 推进技术, 2011, 32(1): 36~41.SU W Y, ZHANG X Y, ZHANG K Y. Numerical investigation of Lorentz force control on hypersonic inlet boundary layer separation[J]. Journal of Propulsion Technology , 2011, 32(1): 36~41.[5]JIANG H, LIU J, LUO S C, et al. Hypersonic flow control of shock wave/turbulent boundary layer interactions using magnetohydrodynamic plasma actuators[J]. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 2020 21(9):745-760.[6]陈智. 低磁雷诺数磁流体湍流建模及数值模拟研究[D]. 北京: 北京航空航天大学, 2011:21~23.CHEN Z. Theoretical Modeling and Numerical Study of Low Magnetic Reynolds Number Magnetohydrodynamic Turbulence[D]. Beijing: School of Aeronautic Science and Engineering Beihang University, 2011: 21~23.[7]丁明松,刘庆宗,江涛,等.磁控热防护系统在天地往返运载器上的应用仿真[J].航空学报, 2020, 42(2): 124501. DING M S, LIU Q Z, JIANG T, et al. Simulation of magnetohydrodynamic heat shield system on reusable launch vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2020, 42(2): 124501.(in Chinese). doi: 10.7527/S1000-6893.2020.24501[8]丁明松, 江涛, 董维中,等. 三维等离子体MHD气动热环境数值模拟[J]. 航空学报, 2017, 38(8):121030DING M S, JIANG T, DONG W Z, et al. Numerical simulation of 3D plasma MHD aero-thermal environment[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(8):121030. (in Chinese).[9]Bobashev S V, Mende N P, Sakharov V A. MHD Control of the Separation Phenomenon in a Supersonic Xenon Plasma Flow. I : AIAA-2003-168[R]. Reston: AIAA, 2003.[10]Bobashev S V, Erofeev A V, Lapushkina T A, et al. Experiments on MHD control of attached shocks in diffuser : AIAA-2003-169[R]. Reston: AIAA, 2003.[11]Zaidi S H, Smith T, Macheret.S Snowplow Surface Discharge in Magnetic Field for High Speed Boundary Layer Control: AIAA 2006-1006[R]. Reston: AIAA, 2006.[12]Saito S, Udagawa K, Kawaguchi K. Boundary Layer Separation Control by MHD Interaction :AIAA 2008-1091[R]. Reston: AIAA, 2008.[13]苏纬仪, 陈立红, 张新宇. MHD控制超声速边界层的理论研究和数值分析[J], 力学学报, 2010,42(4):782-788.SU W Y, CHEN L H, ZHANG X Y. Physics and numerical simulations of mhd acceletrated supersonic boundary layer[J]. Chinese Journal of Theoretical and Applied Mechanics, 2010,42(4):782-788.[14]王宇天,张百灵,李益文等. 表面磁流体气动激励控制楔面激波规律数值研究[J], 推进技术, 2017, 38(11): 2456~2462.WANG Y T,ZHANG B L,LI Y I, et al. Numerical Research for Regularity of Wedge ShockWave with Surface MHDAerodynamic Actuation[J]. Journal of Propulsion Technology, 2017, 38(11): 2456~2462.[15]李益文, 王宇天, 庞垒, 等. 进气道等离子体/磁流体流动控制研究进展[J], 力学学报, 2019, 51(2):311-321.LI Y W,WANG Y T, PANG L, et al. Presearch progress of plasma/mhd flowcontrol in inlet[J]. Chinese Journal of Theoretical and Applied Mechanics, 2019, 51(2): 311-321.[16]WANG D, WANG J F, LI L F. Electromagnetic field/hypersonic flow field coupled algorithm and its application in the magnetic controlled inlet design[J], Aerosp. Sci. Technol. 2022, 126: 107598. [17] 罗仕超, 吴里银, 常雨. 高速湍流流动磁流体动力学控制机理[J]. 物理学报, 2022, 71(21) :214702.LUO S C, WU L Y, CHANG Y. Mechanism analysis of magnetohydrodynamic control in hypersonic turbulent flow[J]. Acta Phys. Sin. , 2022, 71(21) :214702[18]WU Z Y,Ding M S,Dong W Z. Effect of MHD Control on Turbulent Boundary Layer Separation Flow in Scramjet Inlet[J], Journal of Physics Conference Series,2022,2381:012015.[19]滕子昂, 周志峰, 张智超, 许珂, 高振勋. 高超声速磁流体流动控制数值模拟研究[J], 气动研究与试验,2024,2(1):86-99.TENG Z, ZHOU Z F, ZHANG Z C, XU K, GAO Z X Numerical Investigation of Magnetohydrodynamics Flow Control[J], Aerodynamic Research & Experiment, 2024, 02(01): 86-99.(in Chinese)[20]罗仕超,柳军,胡守超,等. 高超声速进气道自起动特性磁流体动力学控制机理[J]. 中国科学:物理学 力学 天文学,2024,54(03):234711.LUO S C, LIU J, HU S C, et al. Effect of magnetohydrodynamic control on the self-starting ability of hypersonic inlets[J]. SCIENTIA SINICA Physica, Mechanica& Astronomica, 2024, 54(03): 234711.[21]Macheret S O. Physics of magnetically accelerated non-equilibrium surface discharges in high speed flow[R]. AIAA 2005-1005.[22]王宇天,张百灵,李益文等. 等离子体激励控制激波与边界层干扰流动分离数值研究[J]. 航空动力学报, 2018, 33(2):364-371.WANG Y T, ZHANG B L, LI Y W. Numerical investigation for control of shock wave and boundary layer interactions flow separation with plasma actuation[J]. Journal of Aerospace Power, 2018, 33(2):364-371(in Chinese).[23]丁明松, 傅杨奥骁, 高铁锁, 等. 高超声速磁流体力学控制霍尔效应影响研究[J]. 物理学报, 2020, 69(21):214703.DING M S, FU Y A X, GAO T S, et al. Study of impact of Hall effect on hypersonic magnetohydrodynamic control [J]. Acta Physica Sinica, 2020, 69(21):214703. (in Chinese).[24]丁明松, 刘庆宗, 江涛, 等. 高温气体效应对高速磁流体力学控制影响的分析[J]. 航空学报, 2020,41(2): 123278.DING M S, LIU Q Z, JIANG T, et al. Impact of high temperature gas effect on hypersonic magneto-hydrodynamic control[J]. Acta Physica Sinica, 2020,41(2): 123278(in Chinese).[25]丁明松,江涛,刘庆宗,等.电导率模拟对高速MHD控制影响分析[J].航空学报, 2019, 40(11): 123009. DING M S, JIANG T, LIU Q Z,et al. Impact of simulation of electrical conductivity on hypersonic Flow MHD control[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(11):123009(in Chinese).[26]丁明松, 江涛, 刘庆宗, 等. 基于电流积分计算磁矢量势修正的低磁雷诺数方法[J]. 物理学报, 2020, 69(13):164702.DING M S, JIANG T, LIU Q Z, et al. An improved low magnetic Reynolds magnetohydrodynamic method based on computing induced magnetic vector potential by integrating induced current[J]. Acta Physica Sinica,2020, 69(13): 164702 (in Chinese).[27]DIETIKER J F. Numerical Simulation of Magneto-hydrodynamic flows [D]. Whichita State: Whichita State University, 2001:25~30.[28]Datta V G, Poggie J. An implicit technique for 3-D turbulent MGD with the generalized Ohm's Law [R]. AIAA 2001-2736. Reston: AIAA, 2001.[29]赵慧勇. 超燃冲压整体发动机并行数值研究[D]. 绵阳: 中国空气动力研究与发展中心, 2005: 50~56.ZHAO,H Y. Parallel Numerical Study of Whole Scramjet engine[D]. China Aerodynamics Research and Development Center, 2005: 50~56.[30]蒋浩,柳军,王君媛,黄伟,杜洋. 全隐LU-SGS算法在高超声速热化学非平衡流刚性问题中的应用[J], 国防科技大学学报, 2022,44(2):1~8.JANG H,LIU J,WANG J Y,HUANG W,DU Y. Fully implicit LU-SGS algorithms applied to stiff problems in hypersonic thermochemical non-equilibrium flows[J]. JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY, , 2022,44(2):1~8.[31]Kalra C, Zaidi S H, Alderman B J, et al. Magnetically driven surface discharges for shock-wave induced boundary-layer separation control [R]. AIAA 2007-222. Reston: AIAA, 2007.[32]R B Miles, S O Macheret, M N Shneider, et al. Plasma-Enhanced hypersonic performance enabled by MHD power extraction. [R]. AIAA 2005-561. Reston: AIAA, 2005.[33]Updike G A, Shang J S, Gaitonde D V. Hypersonic separated flow control using Magneto-aerodynamic interaction [R]. AIAA 2005-164. Reston: AIAA, 2005.[34]李开, 柳军, 刘伟强. 高超声速飞行器磁控热防护霍尔电场数值方法研究[J]. 物理学报, 2017, 66(8): 084702.LI K, LIU J, LIU W Q. Numerical solution procedure for Hall electric field of the hypersonic magnetohydrodynamic heat shield system[J]. Acta Physica Sinica, 2017, 66(8):084702. (in Chinese).[35]吕浩宇, 李椿萱. 三维非理想低磁雷诺数磁流体流动的数值模拟[J]. 中国科学E辑:技术科学, 2009, 39(11): 1836~1842.LV H Y, LI C X. Simulation of three-dimensional nonideal MHD flow at low magnetic Reynolds number. Sci China Ser E-Tech Sci, 2009, 52(12): 3690~3697, doi: 10.1007/s11431-009-0263-5. (in Chinese).[36]Bisek N J, and Boyd I D. Numerical study of magnetoaerodynamic flow around a hemisphere[C]. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando,Florida, 4-7 January 2010, AIAA 2010-227.[37]张百灵, 朱涛, 李益文等. 超声速气流磁流体加速技术的应用与发展[J], 力学与实践, 2013, 35(2):13-21.ZHANG B L, ZHU T, LI Y W. Application and development of supersonic airflow acceleration technology based on magnetohydrodynamics[J], Mechanics in Engineering, 2013, 35(2):13-21. (in Chinese).[38]左光, 齐玢, 欧东斌. 磁流体动力加速风洞技术发展分析[J], 航天返回与遥感,2018,39(6):1-11.ZOU G, QI B, OU D B. Research on Development of Magneto-hydro-dynamics Acceleration Wind Tunnel Technology[J] , Spacecraft Recovery & Remote Sensing , 2018,39(6):1-11 (in Chinese).[39]BOBASHEV S V. MHD control of the separation phenomenon in asupersonic Xenon plasma flow[R], 2003,AIAA 2003-168.BOBASHEV S V. Air plasma pruduced by gas discharge in supersonic MHD channel[R], 2006,AIAA 2006-1373 |