CORC  > 北京航空航天大学
TMF constitutive and life modeling: From smooth specimen to turbine blade [TMF本构和寿命模型:从光棒到涡轮叶片]
Hu, X.; Shi, D.; Yang, X.; Yu, H.
刊名Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
2019
卷号40
关键词Constitutive models Creep Forecasting Isotherms Oxidation Stress concentration Superalloys Temperature Thermal fatigue Turbine components Creep constitutive models Directionally solidified superalloy Fatigue crack initiation Life predictions Material microstructures Stress concentration factors Thermo mechanical fatigues (TMF) Turbine blade Turbomachine blades
ISSN号10006893
DOI10.7527/S1000-6893.2018.22494
URL标识查看原文
收录类别EI
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/5919276
专题北京航空航天大学
推荐引用方式
GB/T 7714
Hu, X.,Shi, D.,Yang, X.,等. TMF constitutive and life modeling: From smooth specimen to turbine blade [TMF本构和寿命模型:从光棒到涡轮叶片][J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2019,40.
APA Hu, X.,Shi, D.,Yang, X.,&Yu, H..(2019).TMF constitutive and life modeling: From smooth specimen to turbine blade [TMF本构和寿命模型:从光棒到涡轮叶片].Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,40.
MLA Hu, X.,et al."TMF constitutive and life modeling: From smooth specimen to turbine blade [TMF本构和寿命模型:从光棒到涡轮叶片]".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 40(2019).
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace