Ceramic Matrix Composites: Lifetime and Strength Prediction Under Static and Stochastic Loading focuses on the strain response and lifetime prediction of fiber-reinforced ceramic-matrix composites under stress-rupture loading at intermediate temperatures. Typical damage mechanisms of matrix cracking, interface debonding and oxidation, and fiber's oxidation and fracture are considered in the micromechanical analysis. Effects of composite's constituent properties, peak stress, and testing temperature on the composite's strain response and lifetime are also analyzed in detail. Finally, a…mehr
Ceramic Matrix Composites: Lifetime and Strength Prediction Under Static and Stochastic Loading focuses on the strain response and lifetime prediction of fiber-reinforced ceramic-matrix composites under stress-rupture loading at intermediate temperatures. Typical damage mechanisms of matrix cracking, interface debonding and oxidation, and fiber's oxidation and fracture are considered in the micromechanical analysis. Effects of composite's constituent properties, peak stress, and testing temperature on the composite's strain response and lifetime are also analyzed in detail. Finally, a comparison of constant and different stochastic stress spectrum on composite's damage evolution and fracture is discussed. This book will be a practical guide for the material researcher and component designer needing to better understand the composite's damage and fracture behavior under stress-rupture loading at intermediate temperatures.Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
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.
Inhaltsangabe
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
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
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