Dynamics of a Turbine Blade with an Under-Platform Damper Considering the Bladed Disc’s Rotation
Open Access
- 7 October 2019
- journal article
- research article
- Published by MDPI AG in Applied Sciences
- Vol. 9 (19), 4181
- https://doi.org/10.3390/app9194181
Abstract
High-cycle fatigue (HCF) failure of the turbine blades of aero-engines caused by high vibrational stresses is one of the main causes of aero-engine incidentsThis publication has 18 references indexed in Scilit:
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