材料科学
烧蚀
复合材料
图层(电子)
腐蚀
工程类
航空航天工程
作者
Zhigang Zhao,Kezhi Li,Gang Kou,Wei Li
标识
DOI:10.1016/j.corsci.2022.110496
摘要
The cyclic and single ablation behavior of C/C-ZrC-SiC and C/C-ZrC composites prepared by reactive melt infiltration were studied. The ablation resistance properties of cyclic ablation of 30 s × 4 and single ablation of 120 s was similar to that of 60 s × 4 and 240 s. The oxidation of the matrix and the peeling content of oxides are aggravated with the increased cyclic ablation numbers. Under the cyclic ablation mode, C/C-ZrC-SiC composites showed lower mass loss than C/C-ZrC composites. At the single ablation of 240 s, C/C-ZrC-SiC composites showed desirable ablation resistance owing to the formation of an effective heat/oxygen protection layer on the ablated surface.
科研通智能强力驱动
Strongly Powered by AbleSci AI