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Published in 2020 at "Corrosion Science"
DOI: 10.1016/j.corsci.2020.108621
Abstract: Abstract Ablation behavior and thermal damage mechanisms of Cf/SiBCN composites were investigated in plasma ablation flame under a heat flux of 4.02 MW/m2, simulating a hypersonic service environment at ∼2200 °C. Oxide layer formed on the composites…
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Keywords:
thermal damage;
plasma ablation;
sibcn composites;
mechanisms sibcn ... See more keywords