Interfaces of Ceramic-Matrix Composites

1 DEFINITION, FUNCTION AND DESIGN OF INTERFACE IN CERAMIC-MATRIX COMPOSITES
1.1. Introduction
1.2. The definition of interface in ceramic-matrix composites
1.3. The function of interface in ceramic-matrix composites
1.4. The design of interface in ceramic-matrix composites
1.5 Conclusion
2 INTERFACE CHARACTERIZATION OF CERAMIC-MATRIX COMPOSITES
2.1. Introduction
2.2. Effect of interface properties on tensile and fatigue behavior of ceramic-matrix composites
2.3. Effect of pre-exposure on tensile damage and fracture of ceramic-matrix composites
2.4. Effect of interface properties on lifetime of ceramic-matrix composites
2.5 Conclusion
3 INTERFACE ASSESSMENT OF CERAMIC-MATRIX COMPOSITES
3.1. Introduction
3.2. Relationships between interface slip and temperature rising in CMCs
3.3. Interface assessment of CMCs from hysteresis loops
3.4 Conclusion
4 INTERFACE DAMAGE LAW OF CERAMIC-MATRIX COMPOSITES
4.1. Introduction
4.2. Interface damage law at room temperature
4.3. Interface damage law at elevated temperature in intert atmosphere
4.4. Interface damage law at elevated temperature in air atmosphere
4.5. Interface damage law at elevated temperature in steam atmosphere
4.6. Results and discussion
4.7 Conclusion

Longbiao Li is a lecturer in the College of Civil Aviation at the Nanjing University of Aeronautics and Astronautics (NUAA), where he received his PhD. His research focuses on the fatigue, damage, fracture, reliability, and durability of aircraft and aero engine. In this research area, he is the first author of 128 SCI journal publications, 2 monograph, 3 book chapters, 10 Chinese Patents, and 1 US Patent, and more than 20 refereed conference proceedings. He has been involved in different projects related to structural damage, reliability, and airworthiness design for aircraft and aero engines, supported by the Natural Science Foundation of China, COMAC Company, and AECC Commercial Aircraft Engine Company.