[1] 乐嘉陵,高铁锁,曾学军,等.再入物理[M].北京:国防工业出版社,2005. LE J L,GAO T S,ZENG X J,et al. Reentry physics[M]. Beijing: National Defense Industry Press,2005. (in Chinese) [2] 常雨,陈伟芳,孙明波,等.等离子体涡电磁散射特性及隐身性能[J]. 航空学报,2008,29(2):304-308. CHANG Y,CHEN W F,SUN M B,et al. Scattering and stealth of plasma vortex[J]. Acta Aeronautica et Astronautica Sinica,2008,29(2):304-308.(in Chinese) [3] 常雨,陈伟芳,罗宁,等.基于物理光学法的再入等离子体包覆体空间散射特性分析[J].微波学报,2008,24(2):1-6. CHANG Y,CHEN W F,LUO N,et al. Analysis of the spatial scattering characteristic for the reentry target cloaked by plasma based on the physical optics method[J].Journal of Microwaves,2008,24(2): 1-6.(in Chinese) [4] 谢楷,李小平,杨敏,等. L、S频段电磁波在等离子体中衰减实验研究[J].宇航学报,2013,34(8):1166-1171. XIE K,LI X P,YANG M,et al. Experimental study on attenuation characteristics of L and S band electromagnetic wave in plasma[J]. Journal of Astronautics,2013,34(8):1166-1171.(in Chinese) [5] 任宁,奚斌,李晓斐.黑障抑制技术的发展现状与研究难点[J].导弹与航天运载技术,2018(1): 122-126. REN N,XI B,LI X F. Development status and difficulties of the technology of blackout suppression[J]. Missiles and Space Vehicles,2018(1): 122-126.(in Chinese) [6] 曹文祥,高铁锁.烧蚀对电离边界层的影响[J].计算物理,1992(增刊1):536. CAO W X,GAO T S. The ablation of ionization effect on boundary layer[J].Chinese Journal of Computational Physics,1992(S1):536.(in Chinese) [7] 张志成,潘梅林,刘初平,等.高超声速气动热和热防护[M].北京:国防工业出版社,2003. ZHANG Z C,PAN M L,LIU C P,et al. Hypersonic aerodynamic heating and thermal protection[M].Beijing: National Defense Industry Press,2003.(in Chinese) [8] 刘小镇. C/C复合材料表面等离子渗锆、铬涂层及其高温氧化性能研究[D].太原:太原理工大学,2017. LIU X Z. Plasma Zr-alloyed and Cr-alloyed coatings formed on C/C composites and their high temperature oxidation property [D].Taiyuan:Taiyuan University of Technology,2017. (in Chinese) [9] 陈伟芳.碳基材料烧蚀下的热化学非平衡流场数值模拟研究[J].工程力学,2016,33(2):249-256. CHEN W F. Numerical simulation for thermochemical nonequilibrium flow under carbon based material ablation condutions[J]. Engineering Mechanics,2016,33(2):249-256. (in Chinese) [10] 张威,曾明,肖凌飞,等.碳-酚醛材料烧蚀热解对再入流场特性影响的数值计算[J].国防科技大学学报,2014,36(4):41-48. ZHANG W,ZENG M,XIAO L F,et al. Numerical study for the effects of ablation and pyrolysis on the hypersonic reentry flow[J].Journal of National University of Defense Technology,2014,36(4):41-48.(in Chinese) [11] TISSERA S, TITAREV V, DRIKAKIS D. Chemically reacting flows around a double-cone, including ablation effects[C]∥Proceedings of the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, FL,US: AIAA, 2010. [12] 张涛,陈德江.再入钝锥体烧蚀热防护内部热响应的数值仿真[J].航空动力学报,2013, 28(10):2248-2255. ZHANG T,CHEN D J. Numerical simulation of internal thermal response of ablative thermal protection for reentry spacecraft[J].Journal of Aerospace Power,2013,28(10): 2248-2255. (in Chinese) [13] 张志豪,孙得川.飞行器气动加热烧蚀工程计算[J].兵工学报,2015,36(10): 1949-1954. ZHANG Z H,SUN D C. Calculation of aerodynamic heating and ablation of multi-layer thermal protection material[J]. Acta Armamentarii,2015,36(10):1949-1954.(in Chinese) [14] 柴栋,方洋旺,童中翔,等.含碱金属杂质的高超声速烧蚀流场特性数值模拟[J].航空动力学报,2013,28(9):1962-1966. CHAI D,FANG Y W,TONG Z X,et al. Numerical simulation of characteristic of hypersonic ablation flow field containing alkali-metal impurities[J].Journal of Aerospace Power,2013, 28(9):1962-1966.(in Chinese) [15] BIANCHI D,NASUTI F,ONOFRI M. Aerothermodynamic analysis of reentry flows coupled with ablation[C]∥Proceedings of the 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco, CA, US:AIAA,2011. [16] 杨鹏飞,方洋旺,柴栋,等.高超声速钝锥体等离子体流场数值模拟[J].飞行力学,2013,31(4):313-316. YANG P F,FANG Y W,CHAI D,et al. Numerical simulation of hypersonic plasma flow fields around blunt cone model[J]. Flight Dynamics,2013,31(4):313-316. (in Chinese) [17] 童长青,成来飞,刘永胜,等. 2D C/SiC-ZrB2复合材料的烧蚀性能[J].航空材料学报,2012, 32(2):69-74. TONG C Q, CHENG L F, LIU Y S, et al. Ablation properties of 2D C/SIC-ZrB2 composite[J]. Journal of Aeronautical Materials,2012,32(2):69-74. (in Chinese) [18] 张松贺,杨远剑,王茂刚,等.电弧风洞热/透波联合试验技术研究及应用[J]. 空气动力学学报,2017,35(1):141-145. ZHANG S H,YANG Y J,WANG M G,et al. Studies and applications of thermal/wave-transmission test technique in arc-heated wind tunnel[J]. Acta Aerodynamica Sinica,2017,35(1):141-145.(in Chinese) [19] 宋永忠,樊桢,李兴超,等.碳/碳复合材料SiC/MoSi2/ZrO2涂层体系氧化烧蚀性能[J].复合材料学报,2016,33(10):2290-2296. SONG Y Z,FAN Z,LI X C,et al. Performance of carbon/carbon composite material SiC/MoSi2/ZrO2 oxidation ablation coating system[J]. Acta Materiae Compositae Sinica,2016, 33(10):2290-2296.(in Chinese) [20] LI Q G,DONG S M,WANG Z,et al. Ablation behavior and mechanism of 3D Cf/ZrC-SiC composites in a plasma wind tunnel environment[J]. Journal of Asian Ceramic Societies, 2015, 3(4): 377-382. [21] 潘德贤,蒋刚,王国林,等.静电探针在高频等离子体风洞中的应用[J].实验流体力学,2014,28(3): 72-77. PAN D X, JIANG G, WANG G L, et al. Application of Langmuir probe in high frequency plasma wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2014, 28(3): 72-77. (in Chinese) [22] SREENIVASULU M, PATRA S K, MOHAN R G. Powered automatic measuring system for Langmuir probe plasma analysis[J]. Review of Scientific Instruments, 2001, 72(11):4312-4314. [23] KOO B, HERSHKOWITZ N. Langmuir probe in low temperature, magnetized plasma: theory and experimental verification[J]. American Institute of Physics, 1999, 86(3): 1213-1220. [24] CHEN F F. Langmuir probe analysis for high density plasmas[J]. Physics of Plasma, 2001, 8(6): 3029-3041. [25] JESSE A L, ALEC D G. Internal Langmuir probe mapping of a hall thruster with xenon and krypton propellant[C]∥Proceedings of the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Sacramento, CA,US:AIAA, 2006:4470. [26] HUTCHINSON I H. Principles of plasma diagnostics [M]. 2nd ed. Cambridge, UK: Cambridge University Press, 2002. [27] 丁小恒. 高超声速飞行试验热流密度测量方法与装置研究[D].哈尔滨:哈尔滨工业大学,2015. DING X H. Heat flux measurement method and instrument for hypersonic flight test[D].Harbin:Harbin Institute of Technology,2015.(in Chinese)
第41卷 第2期2020 年2月兵工学报ACTA ARMAMENTARIIVol.41No.2Feb.2020
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