材料科学
烧蚀
碳化物
氧化物
复合材料
碳化钽
耐火材料(行星科学)
钽
分析化学(期刊)
冶金
化学
有机化学
工程类
航空航天工程
作者
Yichen Wang,Duo Yu,Jie Yin,Buhao Zhang,Hangfeng Zhang,Xuejian Liu,Yulong An,Michael J. Reece,Qing Huang
摘要
Abstract The ablation behavior of (Hf–Ta–Zr–Nb–Ti)C high‐entropy carbide (HEC‐0) was investigated using a plasma flame in air for different times (60, 90, and 120 s) at about 2100°C. The effect of SiC content on the ablation resistance of HEC– x SiC composites ( x = 10 and 20 vol%) was also studied. The linear ablation rate of HEC‐0 decreases with increasing ablation time, showing the positive role of the oxide layer with a complex composition. The linear ablation rate of HEC–10 vol% SiC (0.3 µm s −1 ) is only a 10th of that of HEC‐0, showing a significant improvement in ablation resistance, probably due to the formation of a protective oxide layer containing melted SiO 2 and refractory Hf–Zr–Si–O oxides.
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