The influence of high-temperature argon heat-treatment on the microstructure and room-
temperature in-plane tensile properties of 2D woven CVI and 2D unidirectional MI SiC/SiC …

Silicon carbide fiber-reinforced silicon carbide ceramic matrix composites (SiC f/SiC) are
considered as a promising material for aero-engine hot-end structural components. The …

As a promising high temperature structural material, ceramic matrix composites have
attracted much attention due to their excellent thermo-mechanical properties. The present …

Millisecond laser processing has advantages in terms of depth, efficiency, and cost. The
evolution mechanism of the laser ablation of SiC f/SiC fabricated through melt infiltration …

Abstract 3D woven SiC/SiC composites with Sylramic™-iBN SiC fibers have been fabricated
by first partially infiltrating 3D woven fiber preforms with SiC by chemical vapor infiltration …

The ablation resistance of C f/HfC PIP-SiC CVI composites was tested under an
oxyacetylene flame. After ablation, many SiO 2 nanowires were in-situ grown in the edge …

Abstract Chemical-vapor-infiltrated (CVI) SiC/SiC composites with Sylramic™-iBN SiC fibers
and CVI carbon, BN, and a combination of BN/C interface coating were heat treated in 0.1 …

For the advantages of high-temperature resistance, corrosion resistance and ultra-high
hardness, SiC f/SiC composite is becoming a preferred material for manufacturing aero …

A stress-free oxidation model considering the microstructural characteristics of SiC/SiC mini-
composites was proposed based on the electrical resistance change before and after …

In this paper, a unified physics-informed machine learning (PIML) model is proposed for the
accurate prediction of the creep rupture life of oxide/oxide ceramic matrix composites …