[1]彭俊. 强激波干扰与极端热载荷机理研究[D]. 北京: 中国科学院大学, 2021.PENG J. Study on strong shock interaction and extreme thermal load mechanism[D]. Beijing: University of Chinese Academy of Sciences, 2021. (in Chinese)
[2]EDNEY B E. Effects of shock impingement on the heat transfer around blunt bodies[J]. AIAA Journal, 1968, 6(1): 15-21.
[3]CHU Y B, LU X Y. Characteristics of unsteady type IV shock/shock interaction[J]. Shock Waves, 2012, 22(3): 225-235.
[4]肖丰收, 李祝飞, 朱雨建, 等. 第IV类激波-激波干扰非定常性及其敏感因素分析[J]. 空气动力学学报, 2017, 35(1): 20-26.XIAO F S, LI Z F, ZHU Y J, et al. Unsteadiness and sensitive factors of type IV shock-shock interaction[J]. Acta Aerodynamica Sinica, 2017, 35(1): 20-26. (in Chinese)
[5]李佳伟, 王江峰, 杨天鹏, 等. “IV型”激波干扰中流-热-固耦合问题一体化计算分析[J]. 航空学报, 2019, 40(12): 123175.LI J W, WANG J F, YANG T P, et al. Integrated computation and analysis of fluid-thermal-structural coupling in type IV shock interaction[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(12): 123175. (in Chinese)
[6]饶洛瑜，张涛，施崇广，等. 侧滑角对 V 型钝化唇口激波干扰结构的影响[J]. 航空学报, 2025, 46(2): 130681.RAO L Y, ZHANG T, SHI C G, et al. Effect of sideslip angle on shock interaction structure of V-shaped blunt lip[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(2): 130681.(in Chinese)
[7]李祝飞, 王军, 张志雨, 等. V形钝化前缘激波干扰问题[J]. 气动研究与试验, 2024, 2(5): 1-13.LI Z F, WANG J, ZHANG Z Y, et al. Shock interaction on V-shaped blunt leading edge[J]. Aerodynamic Research & Experiment, 2024, 2(5): 1-13. (in Chinese)
[8]LOPATOFF M. Wind-flow study of pressure-drag reduction at transonic speed[R]. Washington, D. C.: NASA, 1951.
[9]WARREN C H E. An experimental investigation of coolant gas ejection at bluff body nose[J]. Journal of Fluid Mechanics, 1960, 8(3): 400-417.
[10]HAYASHI K, ASO S. Aerodynamic heating reduction by opposing jet in supersonic flow[J]. Journal of the Japan Society for Aeronautical and Space Sciences, 2004, 52(600): 38-44.
[11]PRABHU R K, THAREJA R R, WIETING A R. Computational studies of fluid spike for shock interaction heating protection[C]// 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. Reston: AIAA, 1991: 1-12.
[12]ALBERTSON C, VENKAT V. Shock interaction control for scramjet cowl leading edges[C]// AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Reston: AIAA, 2005: 1-12.
[13]范冰, 黄杰, 单先阳. 逆向喷流主动流动控制及减阻机理研究[J]. 机械设计与制造工程, 2020, 49(12): 68-72.FAN B, HUANG J, SHAN X Y. Research on active flow control and drag reduction mechanism of counterflow jet[J]. Machine Design and Manufacturing Engineering, 2020, 49(12): 68-72. (in Chinese)
[14]罗凯,王永海,汪球,等. 高焓风洞中等离子体激励流动控制试验[J]. 航空学报,2022,43(202): 92-99.Luo K, Wang Y H, Wang Q, et al. Experimental study on plasma-induced flow control in high-enthalpy wind tunnel [J]. Journal of Aeronautics, 2022,43(202):92-99.(in Chinese)
[15]周岩, 刘冰, 罗振兵, 等. 火花放电合成射流与超声速来流相互干扰特性数值模拟研究[J]. 空气动力学学报, 2016, 34(4): 511-516.ZHOU Y, LIU B, LUO Z B, et al. Numerical simulation of interaction characteristics between spark discharge synthetic jet and supersonic flow[J]. Acta Aerodynamica Sinica, 2016, 34(4): 511-516. (in Chinese)
[16]谢玮. 逆向/横向等离子体合成射流超/高超声速激波减阻研究[D]. 长沙: 国防科技大学, 2021.XIE W. Research on drag reduction of hypersonic/supersonic shock waves by counter-flow/lateral plasma synthetic jet[D]. Changsha: National University of Defense Technology, 2021. (in Chinese)
[17]周岩, 罗振兵, 王林, 等. 等离子体合成射流激励器及其流动控制技术研究进展[J]. 航空学报, 2022, 43(3): 98-140.ZHOU Y, LUO Z B, WANG L, et al. Research progress on plasma synthetic jet actuator and its flow control technology[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(3): 98-140. (in Chinese)
[18]罗振兵, 谢玮, 解旭祯, 等. 激波及其干扰主动流动控制研究进展[J]. 航空学报, 2023, 44(15): 529002.LUO Z B, XIE W, XIE X Z, et al. Research progress in active flow control of shock and shock interaction[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 529002. (in Chinese)
[19]XIE W, LUO Z B, ZHOU Y, et al. Experimental study on steady jet control of hypersonic double-wedge shock interaction[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 81-94.
[20]李沛峰,张彬乾,陈迎春,等. 减小翼型激波阻力的鼓包流动控制技术[J]. 航空学报,2011,(6): 971-977.LI P F, Zhang B Q, Chen Y C, et al. Control of bulging flow to reduce the wingtip shock resistance[J]. Journal of Aeronautics, 2011, (6):971-977.(in Chinese)
[21]关晓辉,宋笔锋,李占科. 两种超声速翼身激波阻力优化方法对比研究[J]. 航空学报,2013,34(11): 2510-2519.Guan X H, Song B F, Li Z K. Comparative study on two methods of supersonic wing-body shock wave drag optimization[J].Journal of Aeronautics,2013,34(11): 2510-2519. (in Chinese)
[22]李珺,王俊峰,赵雅甜,等. 面向非设计工况的激波针-喷流复合构型研究[J]. 航空学报,2022,43(9): 329-344.Li J, Wang J F, Zhao Y T, et al. Study on the Shock Pin-Jet Composite Configuration for Non-Design Conditions [J]. Journal of Aeronautics, 2022,43(9):329-344.(in Chinese)
[23]LI Y F, CHANG J T, WANG Z, et al. Inversion and reconstruction of supersonic cascade passage flow field based on transposed-residual network[J]. Physics of Fluids, 2019, 31(12): 126102.
[24]LI Y F, CHANG J T, KONG C, et al. Flow field reconstruction of supersonic cascade using symmetry neural network[J]. AIP Advances, 2020, 10(6): 065102.
[25]DING Z W, LUO Z B, LIU Q, et al. Fast prediction of high-speed missile flow field characteristics under transverse jet control based on deep learning[J]. Chinese Journal of Aeronautics, 2025, 38(8): 103447.
[26]WU W T, HONG Y J, WANG D K, et al. Rainbow schlieren study of oblique-bow shock interaction[J]. Journal of Propulsion Technology, 2015, 36(5): 671-677.
[27]赵涛. 振荡射流激励器性能优化及应用研究[D]. 南京: 南京航空航天大学, 2021.ZHAO T. Performance optimization and application of oscillating jet actuator[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2021.(in Chinese)
[28]SUN D, WANG Z R, QU F, et al. Deep learning prediction for supercritical airfoil at transonic speeds[J]. Physics of Fluids, 2021, 33(8): 086109.
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