参考文献/References:
[1] 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,2003:67-78.
[2] 袁海根,曾金芳,杨杰,等.防热抗烧蚀复合材料研究进展[J].化学推进剂与高分子材料,2006,4(1):21-25.
Yuan Haigen,Zeng Jinfang,Yang Jie,et al.Research progress of high temperature thermo-protective and ablation resistant composite materials [J].Chemical Propellants&Polymeric Materials,2006,4(1):21-25.(in Chinese)
[3] 易法军,梁军,孟松鹤,等.防热复合材料的烧蚀机理与模型研究[J].固体火箭技术,2000,23(3):48-56.
Yi Fajun,Liang Jun,Meng Songhe,et al.Study on ablation mechanism and models of heat shield composites [J].Journal of Solid Rocket Technology,2000,23(3):48-56.(in Chinese)
[4] 易法军,孟松鹤,梁军,等.防热复合材料高温体积烧蚀模型[J].哈尔滨工业大学学报,2001,33(6):725-728.
Yi Fajun,Meng Songhe,Liang Jun,et al.A high-temperature volumetric ablation model for thermal protective composites [J].Journal of Harbin Institute of Technology,2001,33(6):725-728.(in Chinese)
[5] 韩杰才,赫晓东,杜善义.碳/碳复合材料研究的现状和进展[J].宇航材料工艺,1994,24(4):1-5.
Han Jiecai,Hao Xiaodong,Du Shanyi.Research and progress of C/C composites [J]. Aerospace Materials &Technology,1994,24(4):1-5.(in Chinese)
[6] 王臣,梁军,吴世平,等.高温烧蚀条件下C/C材料热力耦合场模拟[J].复合材料学报,2006,23(5):143-148.
Wang Chen,Liang Jun,Wu Shiping,et al.Numerical simulation of C/C composites coupled thermo-mechanical field under the condition of high temperature and ablation [J].Acta Materiae Compositae Sinica,2006,23(5):143-148.(in Chinese)
[7] 杨亚政,杨嘉陵,方岱宁.高超声速飞行器热防护材料与结构的研究进展[J].应用数学和力学,2008,29(1):47-55.
Yang Yazheng,Yang Jialing,Fang Daining.Research progress on the thermal protection materials and structures in hypersonic vehicles [J].Applied Mathematics and Mechanics,2008,29(1):47-55.(in Chinese)
[8] 常春,陈传忠,孙文成.SiC的高温抗氧化性分析[J].山东大学学报:工学版,2002,32(6):581-585.
Chang Chun,Chen Chuanzhong,Sun Wencheng.Oxidation resistance analysis of silicon carbide at high temperature [J].Journal of Shandong University:Engineering Science Edition,2002,32(6):581-585.(in Chinese)
[9] 余惠琴,陈长乐,邹武,等.C/C-SiC复合材料的制备与性能[J].宇航材料工艺,2001,31(2):28-32.
Yu Huiqin,Chen Changle,Zou Wu,et al.Fabrication and properties of C/C-SiC matrix composites [J].Aerospace Materials &Technology,2001,31(2):28-32.(in Chinese)
[10] 余惠琴,陈长乐,邹武.活性添加剂B、Cr对C/C-SiC复合材料性能的影响[J].宇航材料工艺,2002,32(4):36-40.
Yu Huiqin,Chen Changle,Zou Wu.The effects of boron or chromium additive on the properties of C/C-SiC composites [J].Aerospace Materials &Technology,2002,32(4):36-40.(in Chinese)
[11] 张智,郝志彪,闫联生.C/C-SiC复合材料制备方法及应用现状[J].炭素,2008(2):29-35.
Zhang Zhi,Hao Zhibiao,Yan Liansheng.Preparation methods and application of C/C-SiC composites[J].Carbon,2008(2):29-35.(in Chinese)
[12] 卞荫贵,钟家康.高温边界层传热[M].北京:科学教育出版社,1986.
[13] 姚从菊.再入飞行器烧蚀层内热质传输过程的数值模拟[D].哈尔滨:哈尔滨工业大学能源科学与工程学院,2007.