[1] 胡冬冬,牛文,李文杰,等.美国高超声速地面试验设施建设现状及能力提升举措分析[J].飞航导弹,2015(3):3-9.
[2] 胡冬冬,牛文,陈英硕,等.美国高超声速技术试验设施建设历史教训及启示[J].飞航导弹,2015(2):9-12.
[3] 钟萍,陈丽艳,王颖.国外高超声速技术焦点领域及相关设备改造综述[J].飞航导弹,2011(10):17-22.
[4] LESLIE J,MARREN D.Hypersonic test capabilities overview[C]//U.S.Air Force T&E Days 2009.Reston,Virigina: AIAA,2009.
[5] 赵芳.低总温直连式空气加热器数值仿真与试验研究[D].长沙: 国防科学技术大学,2012.
[6] 罗飞腾.污染空气对煤油燃料超燃冲压发动机性能的影响研究[D].西安: 西北工业大学,2012.
[7] SERRE L.ONERA potential for scramjet ground testing up to Mach 12[C]//AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference.Capua,Italy.Reston,Virigina: AIAA,2005.
[8] THOMAS S,LEE J,STEPHENS J,et al.The mothball,sustainment,and proposed reactivation of the hypersonic tunnel facility(HTF)at NASA Glenn research center plum brook station[C]//27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.Reston,Virigina: AIAA,2010.
[9] GOYNE C,CRESCI D.Hy—V program overview and status[C]//15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.Reston,Virigina: AIAA,2008.
[10] TOMIOKA S,HIRAIWA T,KOBAYASHI K,et al.Vitiation effects on scramjet engine performance in Mach 6 flight conditions[J].Journal of Propulsion and Power,2007,23(4):789-796.
[11] SERRE L,FALEMPIN F.Development of S4 free jet test facility for the French LEA flight test program[C]//15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.Dayton,Ohio.Reston,Virigina: AIAA,2008.
[12] SAARI D,CHU P,JAUCH C.Clean air regenerative storage heater technology for propulsion test facilities[C]//16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.Bremen,Germany.Reston,Virigina: AIAA.
[13] FANK K L,MARREN D E.先进高超声速试验设备[M].黄训铭,译.北京: 航空工业出版社,2015.
[14] 冯军红.高焓高压空气加热器数值仿真与试验研究[D].长沙: 国防科学技术大学,2011.
[15] DROZDA T G,CABELL K F,ZILTZ A R,et al.Comparisons between NO PLIF imaging and CFD simulations of mixing flowfields for high—speed fuel injectors[C]//53rd AIAA/SAE/ASEE Joint Propulsion Conference.Atlanta,GA.Reston,Virginia: AIAA,2017.
[16] SMITH D M,YOUNKER T.Comparative ablation testing of carbon phenolic TPS materials in the AEDC—H1arcjet[C]//AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference.Capua,Italy.Reston,Virigina: AIAA,2005.
[17] VIGUIER P,GARRAUD J,SOUTADE J,et al.Scramjet tests in the ONERA F4 hotshot wind tunnel[C]//19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.Atlanta,GA.Reston,Virginia: AIAA,2014.
[18] 胡冬冬,叶蕾.从高速系统试验(HSST)项目看美国高超声速试验科学技术专项实施现状[J].飞航导弹,2016(4):22-27.
[19] 钟萍.国外高超声速飞行加速地面模拟能力研究进展[J].飞航导弹,2014(6):10-15.
[20] GARRARD D,SEELY J,ABEL L.An analysis of alternatives to provide a varying Mach number test capability at APTU[C]//14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference.Canberra,Australia.Reston,Virigina: AIAA,2006.
[21] MONTGOMERY P,GARRARD D.Test and evaluation of hypersonic aeropropulsion systems along flight trajectories in a time—varying flight environment[C]//41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Tucson,Arizona.Reston,Virigina: AIAA,2005.
[22] 黄斌.基于TDLAS的RBCC发动机出口燃烧流场诊断实验研究[D].西安: 西北工业大学,2015.
[23] 叶景峰.超燃冲压发动机燃烧流场羟基分子标记速度测量技术研究[D].西安: 西北工业大学,2019.
[24] KOHSE-HOINGHAVS K, JEFFRIES J B.应用燃烧诊断学[M].刘晶儒,叶景峰,陶波,等译.北京:国防工业出版社,2017.
[25] 王璐,韩洪涛,王友利.2017年国外高超声速技术发展回顾[J].国际太空,2018(3):41-45.
[26] 张灿,林旭斌,胡冬冬,等.2018年国外高超声速飞行器技术发展综述[J].飞航导弹,2019(2):1-5.
[27] 胡冬冬,刘晓明,张绍芳,等.2016年国外高超声速飞行器技术发展综述[J].战术导弹技术,2017(1):28-33.
[28] 李文杰,牛文,叶蕾.美国准备地面试验10倍于X—51A的超燃冲压发动机[J].飞航导弹,2015(3):10-13.
[29] 田宏亮.临近空间高超声速武器发展趋势[J].航空科学技术,2018,29(6):1-6.
[30] GARRARD D.Hypersonic test capabilities at the aerodynamic and propulsion test unit [R].AIAA 2015-1784.
[31] 龚红明.0.6米激波风洞马赫数8喷管设计及数值计算[D].重庆: 重庆大学,2015.
[32] 栗继伟.JFX爆轰驱动激波风洞关键问题研究[D].太原: 中北大学,2017.
[33] 吕治国,李国君,赵荣娟,等.卡尔斯潘公司高超声速脉冲设备建设历程分析[J].实验流体力学,2014,28(5):1-6.
[34] 杨阳.污染组分对超燃冲压发动机性能的影响研究[D].成都: 西南交通大学,2009.
[35] CURRAN E T,MURTHY S N B.Scramjet propulsion [C]//Progress in Astronautics and Aeronautics.Washington,DC: AIAA,2001.
[36] MCCLINTON C,ROUDAKOV A,SEMENOV V,et al.Comparative flow path analysis and design assessment of an axisymmetric hydrogen fueled scramjet flight test engine at a Mach number of 6.5[C]//Space Plane and Hypersonic Systems and Technology Conference.Norfolk,VA,USA.Reston,Virigina: AIAA,1996.
[37] VOLAND R,AUSLENDER A,SMART M,et al.CIAM/NASA Mach 6.5 scramjet flight and ground test[C]//9th International Space Planes and Hypersonic Systems and Technologies Conference.Norfolk,VA,USA.Reston,Virigina: AIAA,1999.
[38] 茆青.高超声速风洞带式电阻加热器强化换热数值研究[D].绵阳: 中国空气动力研究与发展中心,2016.
[39] ORTH R,KISLYKH V.American/Russian hypersonic combustion research experiments in the TSNIIMASH PGU—11 facility[C]//33rd Aerospace Sciences Meeting and Exhibit.Reno,NV,USA.Reston,Virigina: AIAA,1995.
[40] 赵小运.板片蓄热式加热器设计方法研究[D].长沙: 国防科学技术大学,2011.
[41] CHEVALIER A,FALEMPIN F.Review of new French facilities for PREPHA program[C]//International Aerospace Planes and Hypersonics Technologies.Chattanooga,TN,USA.Reston,Virigina: AIAA,1995.
[42] HOHN O M.Experimental investigation of sidewall compression and internal contraction in a scramjet inlet[J].Journal of Propulsion and Power,2017,33(2):501-513.
[43] FALEMPIN F,SERRE L.French contribution to hypersonic airbreathing propulsion technology development—status in 2006[C]//42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Sacramento,California.Reston,Virigina: AIAA,2006.
[44] OLIVIER H,HABERMANN M,BLEILEBENS M.Use of shock tunnels for hypersonic propulsion testing[C]//35th Joint Propulsion Conference and Exhibit.Los Angeles,CA,USA.Reston,Virigina: AIAA,1999.
[45] SCHRAMM J M,SUNAMI T,et al.Experimental investigation of supersonic combustion in the HIEST and HEG free piston driven shock tunnels[R].AIAA 2010-7122.
[46] 俞鸿儒.大幅度延长激波风洞试验时间[J].中国科学: 物理学 力学 天文学,2015,45(9):6-11.
[47] 王振锋.脉冲设备二维高超进气道压缩面激波—边界层干扰显示技术及应用研究[D].绵阳: 中国空气动力研究与发展中心,2015.
[48] 陈苏宇.高超声速压缩拐角气动热环境研究[D].绵阳: 中国空气动力研究与发展中心,2014.
[49] 乐嘉陵.吸气式高超声速技术研究进展[J].推进技术,2010,31(6):641-649.
[50] 谭宇,毛雄兵,焦伟,等.燃烧风洞不同模拟方式对超燃发动机性能影响试验研究[J].推进技术,2017,38(9):2062-2068.
[51] 邓维鑫.宽范围马赫数超燃冲压发动机燃烧组织技术研究[D].成都: 西南交通大学,2013.
[52] 钟战.超声速气流中气化煤油的喷注与燃烧特性研究[D].长沙: 国防科学技术大学,2015.
[53] 吕仲.固体火箭超燃冲压发动机工作特性研究[D].长沙: 国防科学技术大学,2012.
[54] 李庆.基于凹腔火焰稳定器的亚燃冲压发动机燃烧室点火过程研究[D].长沙: 国防科学技术大学,2010.
[55] 吴海燕.超燃冲压发动机燃烧室两相流混合燃烧过程仿真及实验研究[D].长沙: 国防科学技术大学,2009.
[56] 陈植.超燃冲压发动机隔离段流动机理及其控制的试验研究[D].长沙: 国防科学技术大学,2015.