Micromechanics of Ceramic-Matrix Composites at Elevated Temperatures
Del 6 i serien Advanced Ceramics and Composites
2 328 kr
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Produktinformation
- Utgivningsdatum:2025-04-04
- Mått:155 x 235 x 9 mm
- Vikt:236 g
- Format:Häftad
- Språk:Engelska
- Serie:Advanced Ceramics and Composites
- Antal sidor:131
- Förlag:Springer Verlag, Singapore
- ISBN:9789819712960
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Mer om författaren
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 202 SCI Journal Publications (58 JCR Q1), 11 Monograph, 4 Edited Books, 4 Textbooks, 3 Book Chapters, 33 Chinese Patents, 2 US Patents, 2 Chinese Software Copyright, and more than 30 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.
Innehållsförteckning
- Introduction.- Micromechanics Stress-Strain Behavior of Ceramic-Matrix Composites under Monotonic Tensile Loading at Room and Elevated Temperatures.- Micromechanics Proportional Limit Stress of Ceramic-Matrix Composites under Monotonic Tensile Loading at Elevated Temperatures.- Micromechanics Residual Strength of Ceramic-Matrix Composites under Cyclic Fatigue Loading at Elevated Temperatures.- Micromechanics Mechanical Hysteresis of Ceramic-Matrix Composites under Cyclic Fatigue at Elevated Temperature.- Micromechanics Interface Damage of Ceramic-Matrix Composites under Cyclic Fatigue at Elevated Temperature.- Micromechanics Lifetime of Ceramic-Matrix Composites under Cyclic Fatigue Loading at Elevated Temperatures.- Micromechanics Strain Response of Ceramic-Matrix Composites under Creep Loading at Elevated Temperature.- Micromechanics Strain Response of Ceramic-Matrix Composites under Creep-Fatigue Loading at Elevated Temperature.
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