Fretting Fatigue Experiment and Finite Element Analysis for Dovetail Specimen at High Temperature

The dovetail attachment between the turbine blade and disk for an aero-engine operates under varying centrifugal load and vibration at elevated temperatures. The fretting fatigue is prone to occur at the contact surface of the dovetail attachment. This paper investigated the fretting fatigue behavio...

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Autores principales: Zhen Qu, Kaicheng Liu, Baizhi Wang, Zhiying Chen
Formato: article
Lenguaje:EN
Publicado: MDPI AG 2021
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T
Acceso en línea:https://doaj.org/article/787be684c51b42b39bebeeabe770f52d
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