[1]WEN X, LIU J, LI J, DING F, XIA Z X.Design and Numerical Simulation of a Clamshell-Shaped Inlet Cover for Air-Breathing Hypersonic Vehicles[J].Journal of Zhejiang University-Science a, 2019, 20(5):347-57
[2] Chamberlain R.Time-Accurate Calculation of the HEDI Shroud Separation Event[C]. AIAA/Annual Interceptor Technology Conference, Huntsville, AL, USA, May 19-21, 1992.
[3] LI Y, REIMANN B, EGGERS T.Coupled Simulation of CFD and Flight Mechanics with a Two-Species-Gas-Model for the Hot Staging of a Multistage Rocket [C]. AIAA/International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, USA, June 16-20, 2014.
[4]蒋增辉, 宋威, 陈农, 等.高超声速风洞子母弹大迎角抛壳投放试验[J].实验流体力学, 2016, 30(5):42-48
[5]赵飞, 刘丽玲, 石泳, 等.类X-43A飞行器高超声速分离仿真[J].航空学报, 2022, 43(5):229-238
[6]唐伟, 刘深深, 余雷, 等.用于级间分离研究的tbcc动力tsto气动布局概念设计[J].空气动力学报, 2019, 37(5):698-704
[7]王粤, 汪运鹏, 王春, 等.一种并联两级入轨飞行器纵向分离方案的数值研究[J].航空学报, 2023, 44(11):78-92
[8]郭凤美, 余梦伦.导弹分离设计技术研究[J].导弹与航天运载技术, 2014, 无(1):5-10
[9] BLOCKER W, RUEBUSH D.X-43A Stage Separation System - a Flight Data Evaluation[C]. AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Capua, Italy, May 16-20, 2005.
[10]朱学昌, 李浩远, 喻天翔, 等.低空高速飞行器整流罩分离技术研究现状和展望[J].固体火箭技术, 2014, 37(1):12-17
[11]王振国, 梁剑寒, 丁猛, 等.高超声速飞行器动力系统研究进展[J].力学进展, 2009, 39(6):78-92
[12]HOLLAND S D, WILLIAM C W, WALTER C E.Hyper-X Research Vehicle Experimental Aerodynamics Test Program Overview[J].Journal of Spacecraft and Rockets, 2001, 38(6):828-835
[13] BRASE L, HAUDRICH D.Flutter and divergence assessment of the HyFly missile[C]. 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Palm Springs, California, USA, May 4-7, 2009.
[14] DAUBY B, ADMACZAK D, MUSE J et al.HIFiRE 6 Overview and Status Update 2014[C]. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Glasgow, Scotland, May 4-7, 2009.
[15] MARSHALL L, GRIFFIN C, ROBERT S.A Chief Engineer’s View of the NASA X-43A Scramjet Flight Test[C]. AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Capua, Italy, July 6-9, 2015.
[16] FOELSCHE R, BECKEL S, BETTI A et al.Flight Results from a Program to Develop a Freeflight Atmospheric Scramjet Test Technique[C]. AIAA/CIRA 14th International Space Planes and Hypersonics Systems and Technologies Conference. Canberra, Australia, November 6-10, 2006.
[17] 董楠.吸气式高超声速飞行器多体分离流动特性及机理的数值研究[D]. 武汉: 华中科技大学, 2022.
[18]郭善广, 柳军, 金亮, 等.高超飞行器内流道激波振荡问题的数值研究及试验验证[J].实验流体力学, 2012, 26(1):7-11
[19]宋威, 艾邦成.多体分离动力学研究进展[J].航空学报, 2022, 44(11):253-273
[20]闻讯, 柳军, 夏智勋.吸气式高超声速飞行器助推分离过程数值仿真[J].国防科技大学学报, 2019, 41(1):34-40
[21]Buning P G, Wong T, Dilley A D.Computational Fluid Dynamics Prediction of Hyper-X Stage Separation Aerodynamics[J].Journal of Spacecraft and Rockets, 2001, 38(6):820-827
[22]庞川博, 向玉伟, 马兴普, 等.高超声速导弹进气道整流罩分离气动特性研究[J].弹箭与制导学报, 2020, 40(3):123-128
[23]朱国祥, 王磊, 苑朝凯, 等.进气道整流罩全尺度动态分离试验研究[J].实验流体力学, 2019, 33(4):45-51
[24]钟俊, 林敬周, 解福田, 等.高超声速大动压下整流罩分离测力风洞试验[J].实验流体力学, 2024, 38(2):98-106
[25]林敬周, 王雄, 钟俊, 等.高马赫数多体分离试验技术研究与应用[J].推进技术, 2020, 41(4):925-933
[26] Lien J, Bose D, Martin J.Automated Sensitivity Analysis of Hyper-X (X-43A) Separation Simulation [C]. AIAA Modeling and Simulation Technologies Conference and Exhibit. Providence, Rhode Island, August 16-19, 2004.
[27]刘广, 江玉刚, 任智毅, 等.整体式整流罩高速分离流固耦合仿真[J].战术导弹技术, 2018, 无(3):30-37
[28]白晓征, 刘君, 郭正, 等.冲压发动机进气道压力振荡过程的数值研究[J].推进技术, 2008, 无(5):562-565
[29]赵星宇, 王翼, 范晓樯, 等.高速进气道抛罩过程内流场演化特性研究[J].推进技术, 2021, 42(5):970-979
[30] 赵星宇.高超声速飞行器抛罩过程内外流非定常特性与进气道起动性能研究[D]. 长沙: 国防科技大学, 2022.
[31] Wang S, Li C, Chen W.Numerical Investigation on Unsteady Flows with an Air- Breathing Hypersonic Vehicle during Its Shroud Separation[C]. 21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, China, March 6-9, 2017.
[32]邓艳丹, 黄生洪, 杨基明, 等.一种-相似飞行器模型的气动特性初探[J].空气动力学报, 2013, 31(3):376-380
[33] 刘雪松.X-51A高超声速飞行器三维重建及气动/隐身特性分析[D]. 南京: 南京航空航天大学, 2017.
[34] Borg M P.Laminar instability and transition on the X-51A[D]. West Lafayette, Indiana: Purdue University, 2009.
[35]Jiao X L, Chang J T, Wang Z Q, et al.Numerical study on hypersonic nozzle inlet starting characteristics in a shock tunnel[J].Acta Astronautica, 2017, 130(无):167-179
[36]Xing F, Ruan C.Numerical investigation on shock train control and applications in a scramjet engine[J].Aerospace Science and Technology, 2017, 60(无):162-171
[37]Prasad T G, Kumar G D, Patel R, Mounika C, et al.Computational analysis of 2D transition inlets for supersonic capture[J].International Journal of Vehicle Structures & Systems, 2022, 14(1):68-74
[38] 王巍.有相对运动的多体分离过程非定常数值算法研究及实验验证[D]. 长沙: 国防科技大学, 2017.
[39]Saito T, Takayama K.Numerical Simulations of Nozzle Starting Process[J].Shock Waves, 1999, 9(2):73-79
[40]陶渊，范晓樯，刘俊林.超声速连续风洞喷管启动过程分析[J].推进技术, 2015, 36(1):24-29
[41]Lian X, Xu H, Duan L, et al.Flow structure and parameter evaluation of conical convergent–divergent nozzle supersonic jet flows[J].Physics of Fluids, 2023, 35(6):066109-1
[42]高周景明，蒋凌峰，朱佳宇, 等.电子初始位置对高能电子空间及时间辐射特性的影响[J].光散射学报, 2023, 35(1):71-77
CJA