材料科学
复合材料
烧蚀
腐蚀
工程类
航空航天工程
作者
Lei Liu,Hejun Li,Wei Feng,Xiaohong Shi,Kezhi Li,Lingjun Guo
标识
DOI:10.1016/j.corsci.2013.04.038
摘要
Abstract Carbon/carbon composites modified by ZrB 2 –ZrC–SiC particles (C/C–Z–SiC), C/C–Z and C/C were ablated by oxyacetylene torch using two different heat fluxes to investigate the effect of doped ceramic particles. Results indicated that C/C–Z–SiC had the best ablation property in heat flux of 2.38 MW/m 2 whereas their ablation rates increased fastest when heat flux rising from 2.38 to 4.18 MW/m 2 . C/C composites had the poorest ablation property in the lower heat flux and their ablation rates increased slowest. Thermal mismatch of Z, SiC and C and evaporation of SiO 2 induced the various ablation behavior.
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