[1]汪海滨,李鑫.轴编C/C复合材料喉衬的多尺度烧蚀分析方法[J].固体火箭技术,2017,40(03):295-301.[doi:10.7673/j.issn.1006-2793.2017.03.005]
 [J].Journal of Solid Rocket Technology,2017,40(03):295-301.[doi:10.7673/j.issn.1006-2793.2017.03.005]
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轴编C/C复合材料喉衬的多尺度烧蚀分析方法

参考文献/References:

[1]Berton B,Bacos M P,Demange D,et al.High temperature behavior of the hot structure materials of Hermes Space Shuttle[C]//Naslain R,Lamalle J,Zulian J L,editors.Composite materials for high temperature application.France:AMAC.Paris,1990:315-325.2]Cavalier J C,Lacomber A,Rouges J M.Ceramic matrix composites new high performance materials.In:A.R.Bunsel,P.Lamicq,A.Massiah,editors.Developments in the science and technology of composite materials[C]//London:Eisevier,1989:99-110. [3]苏君明.C/C喉衬材料的研究与发展[J].炭素科技,2001,1(1):6-11.[4]陈林泉,李岩芳,侯晓.喷管收敛段与喉部型面对喷管流量的影响[J].固体火箭技术,2002,25(1):10-19.[5]Lee Young-jae,Joo Hyeok Jong.Investigation on ablation behavior of CFRC composites prepared at different pressure[J].Composites Part A,2004,35(11):1285-1290. [6]Zien T F.Thermal effects of particles on hypersonic ablation[R].Anaheim:AIAA,2001.[7]Williams S D,Curry D M,Chao D C.Ablation analysis of the shuttle orbiter oxidation protected reinforced carbon-carbo[R].Colorado Springs:AIAA,1994.[8]Bunker Robert C,Prince Andrew.Hybrid rocket motor nozzle material predictions and results[R].Nashville:AIAA,1992.[9]刘建军,苏君明,陈长乐.炭/炭复合材料烧蚀性能影响因素分析[J].炭素,2003(2):15-19.[10]Cho Bong-hwan,Byung Il-yoon.Micro-structural interpretation of the effect of various matrices on the ablation performances of carbon fiber-reinforced composites[J].Composites Science and Technology,2001,61(2):271-280. [11]冉宏星,崔红,郝志彪.炭基体结构状态对C/C复合材料抗烧蚀性能的影响[J].炭素,2002(4):20-25.[12]Naslain R,Guette A,Rebillat F,et al.Oxidation mechanisms and kinetics of SiCmatrix composites and their constituents[J].Journal of Materials Science,2004,39(24):7303-7316.[13]尹健,张红波,熊翔,等.不同预制体结构炭/炭复合材料烧蚀性能[J].复合材料学报,2007,24(1):40-44.[14]Han J C,He X D,Du S Y.Oxidation and ablation of 3D carbon-carbon composite at up to 3 000 ℃[J].Carbon,1995,33(4):473-478.[15]L Ji qiao,H Baiyun,S Gang,et al.Influence of porosity and total surface area on the oxidation resistance of C/C composites[J].Carbon,2002,40(13):2483-2488.[16]Gao P,Wang H,Jin Z.Study of oxidation properties and decomposition kinetics of threedimensional (3-D) braided carbon fiber[J].Thermochim. Acta,2004,414(1):59-63.[17]Lamouroux F,Camus G,Thébault J.Kinetics and mechanisms of oxidation of 2D woven C/SiC composites:I,Experimental Approach[J].Journal of the American Ceramic Society,1994,27(8):2049-2057.[18]Jacobon N S,Roth D J.Oxidation through coating cracks of SiCprotected carbon/carbon[R].NASA/TM-214834,2007.[19]Vignoles G L,Lachaud J,Aspa Y,et al.Ablation of carbonbased materials:multiscale roughness modelling[J].Composites Science and Technology,2009,69(9):1470-1477.[20]Cho D,Lee J Y,Yoon B L.Microscopic observations of the ablation behaviours of carbon fiber/phenolic composites[J].Journal of Material Science,1993,12(24):1894-1896.[21]Cho D,Yoon B L.Microstructural interpretation of the effect of various matrices on the ablation poperties of carbon-fiber-composites[J].Composites Science and Technology,2001,61(2):271-280.[22]Naslain R,Crtte A,Rebillat F,et al.Oxidation mechanisms and kinetics of SiC of SiC-matrix composites and their constituents[J].Journal of Materials Science,2004,39(24):7303-1316.[23]Katardjiev I V,Carter G,Nobes M J,et.al.Three dimensional simulation of surface evolution during growth and erosion[J].Journal of Vacuum Science and Technology A,1994,12(1):61-68.

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更新日期/Last Update: 2017-06-29
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