您当前的位置:
首页 >
文章列表页 >
Research on fretting fatigue life of dovetail joints
更新时间:2026-07-07
    • Research on fretting fatigue life of dovetail joints

    • Vol. 29, Issue 1, Pages: 104-110(2014)
    • DOI:10.13224/j.cnki.jasp.2014.01.013    

      CLC:
    • Published:2014

    移动端阅览

  • doi: 10.13224/j.cnki.jasp.2014.01.013 DOI:

  •  
  •  
icon
试读结束,您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束,您可以通过登录账户,到个人中心,购买VIP会员阅读全文。
已是VIP会员?
去登录 >

0

Views

932

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Research on fretting fatigue life of anisotropic materials
High-temperature fretting fatigue life prediction model based on continuum damage mechanics
High temperature fatigue life model for single crystal nickel superalloy based on principal component analysis
Fatigue life prediction model based on critical plane of nickel-based single crystal superalloy
Fretting fatigue life prediction based on critical plane approach for dovetail joint

Related Author

吴博伟
张宏建
崔海涛
王楠
WANG Rong-qiao
JIANG Kang-he
HU Dian-yin
JING Fu-lei

Related Institution

南京航空航天大学 能源与动力学院 工信部航空发动机热环境与热结构重点实验室
School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing University of Aeronautics and Astronautics
Academy of Aeronautic Propulsion Technology, Aviation Industry Corporation of China
A Military Representative Office, Airforce Xi'an Bureau, The Chinese People's Liberation Army
0