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Thermochemical ablation modeling simulation of C/SiC composites
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Journal Article
Thermochemical ablation modeling simulation of C/SiC composites
2025
Overview
Currently, hypersonic vehicles are confronted with severe aerodynamic heating challenges, imposing strict demands on the thermal insulation and other characteristics of vehicle thermal protection materials. C/SiC composites have emerged as one of the favored materials for aircraft thermal protection, owing to their outstanding ablation resistance, oxidation resistance, and other properties. In this paper, a thermochemical ablation model was developed to elucidate the ablation mechanism of C/SiC composites. The dimensionless ablation rates of C/SiC under different pressures and material ratios were comparatively examined, and the total and linear ablation rates of C/SiC composites over 50 seconds were determined. The simulation results were contrasted with existing experimental data, and the error was within 10%.
Publisher
IOP Publishing
