Abstract
Degradation of high temperature ceramics caused by thermal ablation is a great challenge for maintaining structural integrity and stability under service conditions. In order to advance the understanding of the thermal ablation mechanisms of C/SiC composites, we adopt here the optical observation system to visualize the surface evolution of C/SiC in wind-tunnel test, and demonstrate experimentally the various flow characteristics of liquid SiO2 generated on the sample surface at different temperatures. Three different flow patterns (droplet flow, stream flow, and liquid film flow) corresponding to 1600 ℃, 1750 ℃, and 1950 ℃ were observed on the sample surface. Numerical simulation shows that the radius of the droplets plays a critical role in determining the flow patterns, as evidenced by the experiments. Droplets with large radius (≥0.5 mm) deform severely and cause “tailing”; droplets with small radius deform little under shear. We also observe that the large SiO2 droplet will continuously break into small droplets and eventually the droplets will oscillate with a certain radius. With the ablation rate increasing, a large number of droplets merge with each other to form a liquid film, and periodic K-H (Kelvin-Helmholtz) instability occurs at the gas-liquid interface.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.