本书基于测试实验与数值模拟相结合的方法，以涡轮叶片的冷却孔周围热障涂层系统为研究对象，总结了热-机械耦合作用诱发热障涂层系统失效行为，并阐明提高热障涂层系统性能的优化方法。本书内容将为下一代航天飞机发动机的研发提供宝贵的基础，并为发动机的检查周期和部件的更换周期提供理论依据。

Chapter 1 Introduction
1.1 TBC System
1.2 TGO
1.3 Review of Related Studies
Chapter 2 Experimental and Analytical Methods and Discussions of Results
2.1 Former Analysis for Characterization
2.2 Case of Thermal Cycling
2.3 Case of Thermo-mechanical Cycling
Chapter 3 Optimal Design for Upgrading Stability of TBC System
3.1 Optimization Strategies
3.2 Optimization for TBC System
3.3 Multi-objective Global Optimization
3.4 Effect of Vibration Frequency
Chapter 4 Conclusions
Appendix
References