东华大学学报（英文版）2016，Vol.33Issue(2)：188-191,4.
Fatigue Life Estimation for an Aircraft Engine Fan Blade
Fatigue Life Estimation for an Aircraft Engine Fan Blade
YIN Heng-su 1YAN Jing 1CHEN Hao 1L(U) Zhi-qiang 1HUANG Hong-zhong1
作者信息
- 1. School of Mechatronics Engineering, University of Electronic Science and Technology of China, Chengdu 611731, China
- 折叠
摘要
关键词
fan blade/nominal stress method/fatigue notch factor/cumulative fatigue damage theoryKey words
fan blade/nominal stress method/fatigue notch factor/cumulative fatigue damage theory分类
矿业与冶金引用本文复制引用
YIN Heng-su,YAN Jing,CHEN Hao,L(U) Zhi-qiang,HUANG Hong-zhong..Fatigue Life Estimation for an Aircraft Engine Fan Blade[J].东华大学学报（英文版）,2016,33(2):188-191,4.
