1. Introduction
2. Design of composites facing stress-rupture behaviour
3. Stress-rupture behavior of CMCs under constant stress
4. Stress-rupture behavior of CMCs under stochastic stress
5. Strain response of CMCs under stress-rupture loading with
constant and stochastic loading stress
6. Lifetime of CMCs under stress-rupture loading with constant and
stochastic loading stress
Dr. Longbiao Li is a lecturer in the College of Civil Aviation at the Nanjing University of Aeronautics and Astronautics. Dr. Li’s research focuses on the vibration, fatigue, damage, fracture, reliability, safety and durability of aircraft and aero engine. In this research area, he is the first author of 171 SCI journal publications, 8 monograph, 3 edited book, 3 text book, 3 book chapters, 21 Chinese Patents, and 2 US Patents, 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.
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