Abstract
Ablation of C/C-ZrC composites was studied at a heat flux of ∼25 MW/m2 in a nitrogen plasma torch. C/C-ZrC composites with 4.1 wt% ZrC illustrate a lower linear ablation rate than other composites, that is, 44.7 % lower than that of C/C composites. The formed ZrN/ZrO2 may decrease the ablation rate of the composites by blocking the chemical reaction of the plasma jet and carbon and absorbing significant heat from the plasma jet by their melting and evaporation. The ablation of C/C-ZrC composites is controlled by thermochemical ablation, mechanical breakage, and carbon sublimation, which plays a minor role.
Original language | English |
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Article number | 109409 |
Journal | Corrosion Science |
Volume | 185 |
DOIs | |
State | Published - Jun 2021 |
Keywords
- A. Ceramic matrix composites
- A. Zirconium
- C. High temperature corrosion
- C. Interfaces