Reliability and failure mechanism of ceramic matrix composites in high-temperature combustion environment

Engineering

• Cyclic Fatigue 66%
• Failure Mechanism 100%
• Interfacial Bonding 33%
• Maximum Stress 33%
• Mechanical Fatigue Test 33%
• Room Temperature 100%
• Strength Degradation 33%
• Strength Enhancement 33%
• Stress Level 33%
• Test Condition 33%
• Ultimate Tensile Strength 33%

Material Science

• Carbon Fiber 50%
• Carbon Silicon Carbide Composites 25%
• Ceramic Matrix Composites 100%
• Composite Material 100%
• Residual Strength 25%
• Silicon Carbide 50%
• Thermomechanical Property 25%
• Ultimate Tensile Strength 25%