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pro vyhledávání: '"Laicong Song"'
Publikováno v:
Metals, Vol 14, Iss 7, p 830 (2024)
Fretting wear in the contact area between the aero-engine blade tenon and turbine disk mortise has an important influence on the performance of the aero-engine. In this paper, the tenon joint structure of the DZ125/FGH99 superalloy material is taken
Externí odkaz:
https://doaj.org/article/dcd861cc8db544ed97d89287f26c9f45