[1] |
王国雄, 马鹏飞. 弹头技术[M]. 北京: 宇航出版社, 1993.
|
[2] |
姜贵庆, 刘连元. 高速气流传热与烧蚀热防护[M]. 北京: 国防工业出版社, 2003.
|
[3] |
Chen Lianzhong Zhang Youhua. Types and Trend of Arc Heater Facility[J]. Aerospace Materials & Technology, 2011, (2): 34-42.
|
[4] |
杨鸿, 陈伟芳, 柳森. 电弧湍流平板烧蚀矩形喷管研制及应用[J]. 实验流体力学, 2006, 20(1): 27-30.YANG Hong, CHEN Weifang, LIU Sen. The development and application on rectangular nozzle of arc turbulent flat plate ablation test[J]. Journal of Experiments in Fluid Mechanics, 2006, 20(1): 27-30.
|
[5] |
齐斌, 娄文忠, 田宁, 等. 防热试验用高温超声速燃气流场热环境分析[J]. 宇航材料工艺, 2014, (5): 30-35.QI Bin, LOU Wenzhong, TIAN Ning, et al. Thermal-environment analysis of high temperature and supersonic flow field for thermal protection system test[J]. Aerospace Materials & Technology, 2014, (5): 30-35.
|
[6] |
张涛. 热解气体流动的二维烧蚀热防护数值仿真研究[J]. 宇航学报, 2014,35(1):119-124.ZHANG Tao. Numerical Simulation Research on Two-Dimensional Ablative Thermal Protection with Pyrolysis Gas Flow[J]. Journal of Astronautics, 2014,35(1):119-124.
|
[7] |
AMAR A J, BLACKWELL B F, EDWARDS J R. One-dimensional ablation using a full Newton’s method and finite control volume procedure [J]. Journal of Thermophysics and Heat Transfer, 2008, 22(1):77-82.
|
[8] |
LI W J, HUANG H M, WANG Q, et al. Protection of pyrolysis gases combustion against charring materials’ surface ablation [J]. International Journal of Heat and Mass Transfer, 2016, 102:10-17.
|
[9] |
AGRAWAL P, ELLERBY D, SWITZER M, et a1.Multidimensional Testing of Thermal Protection Materials in the Arcjet Test Facility [C]//10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. Reston, VA, USA:AIAA, 2010: AIAA 2010-4664.
|
[10] |
CHEN Y K, MILOS F S. Effects of nonequilibrium chemistry and Darcy-Forchheimer pyrolysis flow for charring ablator [J]. Journal of Spacecraft and Rockets, 2013, 50(2):256-269.
|
[11] |
姚峰, 董素君, 王浚. 高温燃气热环境加热特性的试验方法研究[J]. 宇航学报, 2010, 31(5):1446-1451.YAO Feng, DONG Sujun, WANG Jun. Numerical analysis of thermal characteristics of high temperature-gas thermal environment[J]. Journal of Astronautics, 2010, 31(5):1446-1451.
|
[12] |
李钟华, 张秀媚. 用独立组元法计算多元多相复杂化学平衡[J]. 哈尔滨工程大学学报, 1997, 18(4): 96~100.LI Zhonghua, ZHANG Xiumei. The calculation of complex equilibrium system by using the independent component method[J]. Journal of Harbin Engineering University, 1997, 18(4): 96-100.
|
[13] |
科.逻辑耶夫. 固体火箭发动机气体动力学与热物理过程[M]. 北京: 宇航出版社, 2007.
|
[14] |
THAKRE P, YANG V. A comprehensive model to predict and mitigate the erosion of carbon-carbon/graphite rocket nozzles[C]// 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2007.
|
[15] |
张斌, 刘宇, 王长辉, 等. 长时间工作固体火箭发动机燃烧室热防护层烧蚀计算[J]. 固体火箭技术, 2011, 34(2):189-192.ZHANG Bin, LIU Yu, WANG Changhui, et al. Computation of ablation of thermal-protection layer in long-time working solid rocket motors[J]. Journal of Solid Rocket Technology , 2011, 34(2):189-192.
|
[16] |
刘骁, 国义军, 刘伟, 等. 碳化材料三维烧蚀热响应有限元计算研究[J]. 宇航学报, 2016, 37(9):1150-1156.LIU Xiao, GUO Yijun, LIU Wei, et al. Numerical simulation research on three-dimensional ablative thermal response of charring ablators[J]. Journal of Astronautics, 2016, 37(9):1150-1156.
|
[17] |
LI W J, HUANG H M, TIAN Y, et al. Nonlinear analysis on thermal behavior of charring materials with surface ablation[J]. International Journal of Heat and Mass Transfer, 2015, 84:245-252.
|
[1] |
王国雄, 马鹏飞. 弹头技术[M]. 北京: 宇航出版社, 1993.
|
[2] |
姜贵庆, 刘连元. 高速气流传热与烧蚀热防护[M]. 北京: 国防工业出版社, 2003.
|
[3] |
Chen Lianzhong Zhang Youhua. Types and Trend of Arc Heater Facility[J]. Aerospace Materials & Technology, 2011, (2): 34-42.
|
[4] |
杨鸿, 陈伟芳, 柳森. 电弧湍流平板烧蚀矩形喷管研制及应用[J]. 实验流体力学, 2006, 20(1): 27-30.YANG Hong, CHEN Weifang, LIU Sen. The development and application on rectangular nozzle of arc turbulent flat plate ablation test[J]. Journal of Experiments in Fluid Mechanics, 2006, 20(1): 27-30.
|
[5] |
齐斌, 娄文忠, 田宁, 等. 防热试验用高温超声速燃气流场热环境分析[J]. 宇航材料工艺, 2014, (5): 30-35.QI Bin, LOU Wenzhong, TIAN Ning, et al. Thermal-environment analysis of high temperature and supersonic flow field for thermal protection system test[J]. Aerospace Materials & Technology, 2014, (5): 30-35.
|
[6] |
张涛. 热解气体流动的二维烧蚀热防护数值仿真研究[J]. 宇航学报, 2014,35(1):119-124.ZHANG Tao. Numerical Simulation Research on Two-Dimensional Ablative Thermal Protection with Pyrolysis Gas Flow[J]. Journal of Astronautics, 2014,35(1):119-124.
|
[7] |
AMAR A J, BLACKWELL B F, EDWARDS J R. One-dimensional ablation using a full Newton’s method and finite control volume procedure [J]. Journal of Thermophysics and Heat Transfer, 2008, 22(1):77-82.
|
[8] |
LI W J, HUANG H M, WANG Q, et al. Protection of pyrolysis gases combustion against charring materials’ surface ablation [J]. International Journal of Heat and Mass Transfer, 2016, 102:10-17.
|
[9] |
AGRAWAL P, ELLERBY D, SWITZER M, et a1.Multidimensional Testing of Thermal Protection Materials in the Arcjet Test Facility [C]//10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. Reston, VA, USA:AIAA, 2010: AIAA 2010-4664.
|
[10] |
CHEN Y K, MILOS F S. Effects of nonequilibrium chemistry and Darcy-Forchheimer pyrolysis flow for charring ablator [J]. Journal of Spacecraft and Rockets, 2013, 50(2):256-269.
|
[11] |
姚峰, 董素君, 王浚. 高温燃气热环境加热特性的试验方法研究[J]. 宇航学报, 2010, 31(5):1446-1451.YAO Feng, DONG Sujun, WANG Jun. Numerical analysis of thermal characteristics of high temperature-gas thermal environment[J]. Journal of Astronautics, 2010, 31(5):1446-1451.
|
[12] |
李钟华, 张秀媚. 用独立组元法计算多元多相复杂化学平衡[J]. 哈尔滨工程大学学报, 1997, 18(4): 96~100.LI Zhonghua, ZHANG Xiumei. The calculation of complex equilibrium system by using the independent component method[J]. Journal of Harbin Engineering University, 1997, 18(4): 96-100.
|
[13] |
科.逻辑耶夫. 固体火箭发动机气体动力学与热物理过程[M]. 北京: 宇航出版社, 2007.
|
[14] |
THAKRE P, YANG V. A comprehensive model to predict and mitigate the erosion of carbon-carbon/graphite rocket nozzles[C]// 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2007.
|
[15] |
张斌, 刘宇, 王长辉, 等. 长时间工作固体火箭发动机燃烧室热防护层烧蚀计算[J]. 固体火箭技术, 2011, 34(2):189-192.ZHANG Bin, LIU Yu, WANG Changhui, et al. Computation of ablation of thermal-protection layer in long-time working solid rocket motors[J]. Journal of Solid Rocket Technology , 2011, 34(2):189-192.
|
[16] |
刘骁, 国义军, 刘伟, 等. 碳化材料三维烧蚀热响应有限元计算研究[J]. 宇航学报, 2016, 37(9):1150-1156.LIU Xiao, GUO Yijun, LIU Wei, et al. Numerical simulation research on three-dimensional ablative thermal response of charring ablators[J]. Journal of Astronautics, 2016, 37(9):1150-1156.
|
[17] |
LI W J, HUANG H M, TIAN Y, et al. Nonlinear analysis on thermal behavior of charring materials with surface ablation[J]. International Journal of Heat and Mass Transfer, 2015, 84:245-252.
|