Acta Aeronautica et Astronautica Sinica ›› 2026, Vol. 47 ›› Issue (6): 132481.doi: 10.7527/S1000-6893.2025.32481
• Fluid Mechanics and Flight Mechanics •
Mingsong DING1,2, Yong XU1,2(
), Tao JIANG1,2, Qingzong LIU2, Peng LI1,2
Received:2025-06-27
Revised:2025-08-05
Accepted:2025-08-26
Online:2025-09-19
Published:2025-09-05
Contact:
Yong XU
E-mail:stephen000@sina.com
Supported by:CLC Number:
Mingsong DING, Yong XU, Tao JIANG, Qingzong LIU, Peng LI. Magnetohydrodynamics control of turbulent boundary layer separation with low electric field[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(6): 132481.
| [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: 国防科技大学, 2017: 14-23. |
| LI K. Magnetohydrodynamic heat shield system including high temperature real gas effect[D]. Changsha: National University of Defense Technology, 2017:14-23 (in Chinese). | |
| [2] | MACCORMACK R W. Evaluation of the low magnetic reynolds approximation for aerodynamic flow calculations[C]∥36th AIAA Plasmadynamics and Lasers Conference. 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 X, ZHENG Y, ZHOU C S, et al. Numerical simulation on the inlet complex turbulent flow of Ramjet assisted range projectiles[J]. Acta Armamentarii, 2005, 26(3): 303-307 (in Chinese). | |
| [4] | 苏纬仪, 张新宇, 张堃元. 洛仑兹力控制高超声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 (in Chinese). | |
| [5] | JIANG H, LIU J, LUO S B, et al. Hypersonic flow control of shock wave/turbulent boundary layer interactions using magnetohydrodynamic plasma actuators[J]. Journal of Zhejiang University: Science A, 2020, 21: 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: Beihang University, 2011: 21-23 (in Chinese). | |
| [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, 2021, 42(7): 124501. |
| DING M S, LIU Q Z, JIANG T, et al. Simulation of magnetohydrodynamic heat shield system on reusable launch vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(7): 124501 (in Chinese). | |
| [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): 121030. |
| DING 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, MENDE N, SAKHAROV V, et al. MHD control of the separation phenomenon in a supersonic xenon plasma flow[C]∥41st Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2003. |
| [10] | BOBASHEV S, EROFEEV A, LAPUSHKINA T, et al. Experiments on MHD control of attached shocks in diffuser[C]∥41st Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2003. |
| [11] | ZAIDI S, SMITH T, MACHERET S, et al. Snowplow surface discharge in magnetic field for high speed boundary layer control[C]∥44th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2006. |
| [12] | SAITO S, UDAGAWA K, KAWAGUCHI K, et al. Boundary layer separation control by MHD interaction[C]∥46th AIAA Aerospace Sciences Meeting and Exhibit. 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 (in Chinese). | |
| [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 W, et al. Numerical research for regularity of wedge shock wave with surface MHD aerodynamic actuation[J]. Journal of Propulsion Technology, 2017, 38(11): 2456-2462 (in Chinese). | |
| [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. Research progress of plasma/mhd flow control in inlet[J]. Chinese Journal of Theoretical and Applied Mechanics, 2019, 51(2): 311-321 (in Chinese). | |
| [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]. Aerospace Science and Technology, 2022, 126: 107598. |
| [17] | 罗仕超, 吴里银, 常雨. 高超声速湍流流动磁流体动力学控制机理[J]. 物理学报, 2022, 71(21): 260-269. |
| LUO S C, WU L Y, CHANG Y. Mechanism analysis of magnetohydrodynamic control in hypersonic turbulent flow[J]. Acta Physica Sinica, 2022, 71(21): 260-269 (in Chinese). | |
| [18] | WU Z Y, DING M S, DONG W Z, et al. Effect of MHD control on turbulent boundary layer separation flow in scramjet inlet[J]. Journal of Physics: Conference Series, 2022, 2381(1): 012015. |
| [19] | 滕子昂, 周志峰, 张智超, 等. 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(1): 86-99. |
| TENG Z A, ZHOU Z F, ZHANG Z C, et al. Numerical investigation of magnetohydrodynamics flow control[J]. Aerodynamic Research & Experiment, 2024(1): 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(3): 138-149. |
| 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(3): 138-149 (in Chinese). | |
| [21] | MACHERET S. Physics of magnetically accelerated non-equilibrium surface discharges in high speed flow[C]∥44th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2005. |
| [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, et al. 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[J]. 物理学报, 2020, 69(21): 307-324. |
| DING M S, FU Y A X, GAO T S, et al. Influence of Hall effect on hypersonic magnetohydrodynamic control[J]. Acta Physica Sinica, 2020, 69(21): 307-324 (in Chinese). | |
| [24] | 丁明松, 刘庆宗, 江涛, 等. 高温气体效应对高超声速磁流体控制的影响[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 magnetohydrodynamic control[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(2): 123278 (in Chinese). | |
| [25] | 丁明松, 江涛, 刘庆宗, 等 . 电导率模拟对高超声速MHD控制影响[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 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): 218-230. |
| 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): 218-230 (in Chinese). | |
| [27] | DIETIKER J F. Numerical simulation of magneto-hydrodynamic flows[D]. Whichita: Whichita State University, 2001: 25-30. |
| [28] | GAITONDE D, POGGIE J. An implicit technique for 3-D turbulent MGD with the generalized Ohm’s law[C]∥ 32nd AIAA Plasmadynamics and Lasers Conference. 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]. Mianyang: China Aerodynamics Research and Development Center, 2005: 50-56 (in Chinese). | |
| [30] | 蒋浩, 柳军, 王君媛, 等. 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. |
| JIANG H, LIU J, WANG J Y, et al. 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 (in Chinese). | |
| [31] | KALRA C, ZAIDI S, ALDERMAN B, et al. Magnetically driven surface discharges for shock-wave induced boundary-layer separation control[C]∥45th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2007. |
| [32] | MILES R, MACHERET S, SHNEIDER M, et al. Plasma-enhanced, hypersonic performance enabled by MHD power extraction[C]∥43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2005. |
| [33] | UPDIKE G, SHANG J, GAITONDE D. Hypersonic separated flow control using magneto-aerodynamic interaction[C]∥43rd AIAA Aerospace Sciences Meeting and Exhibit. 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): 208-217. |
| 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): 208-217 (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[J]. Science in China (Series E (Technological Sciences)), 2009, 39(11): 1836-1842 (in Chinese). | |
| [36] | BISEK N J, BOYD I D, POGGIE J. Numerical study of magnetoaerodynamic flow around a hemisphere[C]∥ 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Reston: AIAA, 2010. |
| [37] | OTSU H, ABE T, KONIGORSKI D. Influence of the Hall effect on the electrodynamic heat shield system for reentry vehicles[C]∥ 36th AIAA Plasmadynamics and Lasers Conference. Reston: AIAA, 2005. |
| [38] | NAGATA Y, OTSU H, YAMADA K, et al. Influence of Hall effect on electrodynamic flow control for weakly ionized flow[C]∥ 43rd AIAA Plasmadynamics and Lasers Conference. Reston: AIAA, 2012. |
| [39] | 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, et al. Application and development of supersonic airflow acceleration technology based on magnetohydrodynamics[J]. Mechanics in Engineering, 2013, 35(2): 13-21 (in Chinese). | |
| [40] | 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. |
| ZUO 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). | |
| [41] | BOBASHEV S, EROFEEV A, LAPUSHKINA T, et al. Air plasma pruduced by gas discharge in supersonic MHD channel[C]∥ 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2006. |
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