Under hypersonic flow conditions, the heat and mass transfer at the gas-solid interface of
thermal protection material becomes highly complicated due to the strong chemical and …

This paper presents the results of experimental tests for the characterization of Ultra-High-
Temperature Ceramic Matrix Composite (UHTCMC) materials for near-zero erosion rocket …

C/C composite material is one of the most widely used thermal protection materials for
hypersonic vehicles. As coupled with fluid dynamics, chemical reaction, heat transfer and …

An irreversible ablation process of a silica fiber reinforced polymer (SiFRP) composite under
various thermal conditions was investigated using a numerical and experimental study. Both …

Capacitance-based nondestructive flaw evaluation (NDE), electric permittivity,
piezoelectricity (capacitance-based stress/strain self-sensing) and piezoresistivity …

Abstract Carbon/carbon (C/C) composites impress with their excellent high-temperature
mechanical properties. In this paper, in order to simulate the complex service conditions of …

The microstructure of carbon fiber–reinforced carbon-matrix composites (carbon/carbon
composites) has important effects on its ablation performance. However, the traditional …

Carbon/carbon composites are usually used as a thermal protection material in the nose cap
and leading edge of hypersonic vehicles. In order to predict the thermal and ablation …

The classification of ablation images holds significant practical value in thermal protection
structures, as it enables the assessment of heat and corrosion resistance of composites. This …

The phenomenon of volumetric ablation of carbon fiber composites by a continuous high
power density laser was investigated theoretically and numerically. The main goal of this …