Fatigue Limit and Predication of Foreign Object Damage of TC4 Titanium Alloy

被引：0
|
作者：
Zheng, Guang-Dong [1 ]
Zhao, Zhen-Hua [2 ]
Huang, Zong-Zheng [3 ]
Li, Jian [3 ]
Mi, Dong [3 ]
Guo, Xiao-Jun [3 ]
Lu, Kai-Nan [1 ]
Chen, Wei [1 ]
机构：
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
[2] State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
[3] AECC Hunan Aviation Powerplant Research Institute, Zhuzhou,412002, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2023年 / 44卷 / 11期
关键词：
Aircraft engines - Engines - Fatigue damage - Fatigue testing - Finite element method - High-cycle fatigue - Low-cycle fatigue - Residual stresses;
D O I：
10.13675/j.cnki.tjjs.2206005
中图分类号：
学科分类号：
摘要：
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