[1] 《航空发动机设计手册》总编委会. 航空发动机设计手册. 第7册. 进排气装置[M]. 北京:航空工业出版社, 2001. Aeroengine Design Manual Editorial Board. Aeroengine Design Manual. Volume 7. Inlet and nozzle[M]. Beijing:Aviation Industry Press, 2001(in Chinese).
[2] 《飞机设计手册》总编委会. 飞机设计手册. 第13册. 动力装置系统设计[M]. 北京:航空工业出版社, 2006. Aircraft Design Manual Editorial Board. Aircraft Design Manual. Volume 13. Engine system design[M]. Beijing:Aviation Industry Press, 2006(in Chinese).
[3] 孙冰, 张建伟. 火箭发动机热防护技术[M]. 北京:北京航空航天大学出版社, 2016. SUN B, ZHANG J W. Thermal protection technology of rocket engine[M]. Beijing:Beihang University Press, 2016(in Chinese).
[4] 约翰·霍普金斯大学应用物理实验所. 冲压发动机技术(上册)[M]. 李存杰, 王树声,李济众,等. 译. 北京:国防工业出版社, 1987. The Johns Hopkins University Applied Physics Laboratory. Scramjet engine (Volume 1)[M]. LI C J, WANG S S, LI J Z, et al. translated. Beijing:National Defense Industry Press, 1987(in Chinese).
[5] 徐旭, 陈兵, 徐大军. 冲压发动机原理及技术[M]. 北京:北京航空航天大学出版社, 2014. XU X, CHEN B, XU D J. Principle and technology of scramjet[M]. Beijing:Beihang University Press, 2014(in Chinese).
[6] 季鹤鸣, 龚正真, 邵万仁, 等. 喷管与机后体一体化设计初探[J]. 航空发动机, 2008, 34(2):27-29, 35. JI H M, GONG Z Z, SHAO W R, et al. Preliminary investigated of integrated design for nozzle and aircraft afterbody[J]. Aeroengine, 2008, 34(2):27-29, 35(in Chinese).
[7] 王占学, 刘帅, 周莉. S/VTOL战斗机用推力矢量喷管技术的发展及关键技术分析[J]. 航空发动机, 2014, 40(4):1-6. WANG Z X, LIU S, ZHOU L. Development and critical technology analysis on thrust vector technology of short/vertical take-off and landing fighter[J]. Aeroengine, 2014, 40(4):1-6(in Chinese).
[8] 汪运鹏, 姜宗林. 高超声速喷管设计理论与方法[J]. 力学进展, 2021, 51(2):257-294. WANG Y P, JIANG Z L. A review of theories and methods for hypersonic nozzle design[J]. Advances in Mechanics, 2021, 51(2):257-294(in Chinese).
[9] 徐惊雷, 莫建伟, 于洋. 高速飞行器的发动机排气系统[M]. 北京:国防工业出版社, 2019. XU J L, MO J W, YU Y. Exhaust system of high speed vehicle engine[M]. Beijing:National Defense Industry Press, 2019(in Chinese).
[10] 李崇俊, 闫联生, 崔红. 航天飞行器热防护系统技术综述[J]. 高科技纤维与应用, 2014, 39(1):19-25, 35. LI C J, YAN L S, CUI H. A review on thermal protection system for aerospace vehicles[J]. Hi-Tech Fiber & Application, 2014, 39(1):19-25, 35(in Chinese).
[11] 叶正寅, 吕广亮. 火箭发动机喷管非定常侧向力和流固耦合研究进展[J]. 航空工程进展, 2015, 6(1):1-12. YE Z Y, LV G L. Advances in the study of unsteady side-loads and fluid/structure interaction of rocket nozzles[J]. Advances in Aeronautical Science and Engineering, 2015, 6(1):1-12(in Chinese).
[12] 胡海峰, 鲍福廷, 王艺杰, 等. 喷管分离流流动-热-结构顺序耦合数值模拟及试验研究[J]. 宇航学报, 2011, 32(7):1534-1541. HU H F, BAO F T, WANG Y J, et al. Nozzle flow separation fluid-thermal-structure load transfer coupled analysis and test research[J]. Journal of Astronautics, 2011, 32(7):1534-1541(in Chinese).
[13] 王书贤. 几何可调喷管的结构特点及发展[J]. 兵器装备工程学报, 2018, 39(1):6-13. WANG S X. Review on structural characteristics and development of geometric variable nozzle[J]. Journal of Ordnance Equipment Engineering, 2018, 39(1):6-13(in Chinese).
[14] 魏建生. 高效异型气膜冷却结构流动与换热特性研究[D]. 西安:西北工业大学, 2018. WEI J S. Study on the flow and heat transfer characteristics of high efficiency shaped film cooling structures[D]. Xi'an:Northwestern Polytechnical University, 2018(in Chinese).
[15] MAISONNEUVE Y. Ablation of solid-fuel booster nozzle materials[J]. Aerospace Science and Technology, 1997, 1(4):277-289.
[16] 宋学智, 李长德, 魏化震. 固体火箭发动机喷管用烧蚀隔热材料研究进展[J]. 弹箭技术, 1998(4):11-21. SONG X Z, LI C D, WEI H Z. Advance of researching of ablative and thermal insulating materials used in the solid rocket motor nozzle[J]. Projectile and rocket technology, 1998(4):11-21(in Chinese).
[17] 苏君明. 火箭喷管多晶石墨的研究[C]//第18届炭-石墨学术会议论文集, 2000:409-414. SU J M. Research on rocket nozzle polycrystalline graphite[C]//Proceedings of the 18th Carbon-Graphite Conference, 2000:409-414(in Chinese).
[18] 冉宏星, 崔红, 郝志彪, 等. 几种喉衬材料断裂韧性的比较[J]. 新型炭材料, 2002, 17(1):30-35. RAN H X, CUI H, HAO Z B, et al. The fracture toughness of several rocket nozzle throat materials[J]. New Carbon Materials, 2002, 17(1):30-35(in Chinese).
[19] 陈华辉, 邓海金, 李明, 等. 现代复合材料[M]. 北京:中国物资出版社, 1998. CHEN H H, DENG H J, LI M, et al. Modern composite material[M]. Beijing:China Materials Press, 1998(in Chinese).
[20] 王零森. 钨基复合材料自冷发汗机理研究[J]. 中南矿冶学院学报, 1983, 14(1):8-16. WANG L S. On the mechanism of self-cooling in tungsten-base composite materials[J]. Journal of Central South Institute of Mining and Metallurgy, 1983, 14(1):8-16(in Chinese).
[21] 陈正求, 李世英. 钨铜复合材料的发展[J]. 钨铝科技, 1984, 10(3):7-18. CHEN Z Q, LI S Y. Development of tungsten copper composite materials[J]. Tungsten Aluminum Technology, 1984, 10(3):7-18(in Chinese).
[22] 史可顺, 林济福. 生焦基石墨的特性和显微结构[J]. 宇航材料工艺, 1982, 12(5):6-10. SHI K S, LIN J F. Characteristics and micro-structure of raw Joulous graphite[J]. Aerospace Materials & Technology, 1982, 12(5):6-10(in Chinese).
[23] 何洪庆, 周旭. 石墨渗铜材料的烧蚀模型探索[J]. 固体火箭技术, 1991, 14(4):102-107. HE H Q, ZHOU X. Exploration of ablation model of graphite copper-permeable materials[J]. Journal of Solid Rocket Technology, 1991, 14(4):102-107(in Chinese).
[24] 孙百顺. 喉衬用钨渗铜制品质量的控制[J]. 固体火箭技术, 1994(1):75-78. SUN B S. Quality control of the copper sintered tungsten products for throat insert[J]. Journal of Solid Rocket Technology, 1994(1):75-78(in Chinese).
[25] 王书贤, 陈林泉, 苏君明, 等. 石墨渗铜喉衬材料的抗热震性能与烧蚀微观结构研究[J]. 科学技术与工程, 2004, 4(3):206-210. WANG S X, CHEN L Q, SU J M, et al. Thermal shock resistance of copper-impregnated graphite throat insert and the erosive microscopic structure[J]. Science Technology and Engineer, 2004, 4(3):206-210(in Chinese).
[26] 苏君明. 石墨渗铜喉衬材料抗热震性能评价[J]. 新型碳材料, 1998, 13(3):21-26. SU J M. Evaluation on the property of thermal shock resistance of copper impregnated graphite throat liner material[J]. New Carbon Materials, 1998, 13(3):21-26(in Chinese).
[27] 陈林泉, 王书贤, 张胜勇, 等. 石墨渗铜喉衬材料烧蚀机理分析[J]. 固体火箭技术, 2004, 27(1):57-59. CHEN L Q, WANG S X, ZHANG S Y, et al. Study on the erosion mechanism of copper-infiltrated graphite throat insert[J]. Journal of Solid Rocket Technology, 2004, 27(1):57-59(in Chinese).
[28] 苏君明, 陈林泉, 王书贤, 等. 石墨渗铜喉衬的烧蚀特性[J]. 固体火箭技术, 2004, 27(1):69-72. SU J M, CHEN L Q, WANG S X, et al. The erosive property of copper-infiltrated graphite throat insert[J]. Journal of Solid Rocket Technology, 2004, 27(1):69-72(in Chinese).
[29] 陈军, 王政时, 董师颜. 钨渗铜材料喷管在长时间续航下的沉积特性[J]. 兵工学报, 2001, 22(3):426-428. CHEN J, WANG Z S, DONG S Y. Sediment properties of copper-sintered-wolfram nozzle with long-range sustained flight in solid rocket missiles[J]. Acta Armamentarii, 2001, 22(3):426-428(in Chinese).
[30] 尹健, 张红波, 熊翔, 等. 针刺整体毡C/C复合材料整体喉衬烧蚀分析[J]. 中国有色金属学报, 2006, 16(9):1539-1544. YIN J, ZHANG H B, XIONG X, et al. Analysis on ablation performance of bulk-needled-felt reinforced carbon composites throat[J]. The Chinese Journal of Nonferrous Metals, 2006, 16(9):1539-1544(in Chinese).
[31] 苏君明. 高效高冲质比C/C喷管的应用与进展[J]. 新型碳材料, 1996, 11(4):18-23. SU J M. Application and progress of high efficiency and high-mass ratio C/C nozzle[J]. New Carbon Materials, 1996, 11(4):18-23(in Chinese).
[32] 黄坚定, 唐菊花. 国外大型团体发动机喷管性能分析[J]. 固体火箭技术, 1996, 19(2):9-16. HUANG J D, TANG J H. Analysis of performance of foreign large-scale solid rocket nozzles[J]. Journal of Solid Rocket Technology, 1996, 19(2):9-16(in Chinese).
[33] CHEN J X, XIONG X, HUANG Q Z, et al. Densification mechanism of chemical vapor infiltration technology for carbon/carbon composites[J]. Transactions of Nonferrous Metals Society of China, 2007, 17(3):519-522.
[34] CANFEILD A A. Braided carbon/carbon nozzle development[C]//21 st AIAA/SAE/ASME/ASEE Joint Propulsion Conference, 1985.
[35] BUSSIERE M, PREL M. Ariane V solid rocket booster nozzle development status[C]//30th Joint Propulsion Conference and Exhibit, 1994.
[36] 朱良杰, 廖东娟. C/C复合材料在美国导弹上的应用[J]. 宇航材料工艺, 1993, 23(4):12-14. ZHU L J, LIAO D J. Application of C/C composite materials in US missiles[J]. Aerospace Materials & Technology, 1993, 23(4):12-14(in Chinese).
[37] 苏君明. C/C喉衬材料的研究与发展[J]. 炭素科技, 2001(1):6-11. SU J M. Research and development of C/C throat lining materials[J]. Carbon Science and Technology, 2001(1):6-11(in Chinese).
[38] 宋桂明, 周玉, 王玉金, 等. 固体火箭发动机喉衬材料[J]. 固体火箭技术, 1998, 21(2):51-55, 61. SONG G M, ZHOU Y, WANG Y J, et al. Throat materials for solid rocket motors[J]. Journal of Solid Rocket Technology, 1998, 21(2):51-55, 61(in Chinese).
CJA