Low cycle fatigue numerical estimation of a high pressure turbine disc for the AL-31F jet engine

This article deals with the description of an approximate numerical estimation approach of a low cycle fatigue of a high pressure turbine disc for the AL-31F turbofan jet engine. The numerical estimation is based on the finite element method carried out in the SolidWorks software. The low cycle fati...

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Bibliographic Details
Main Authors: Spodniak Miroslav, Klimko Marek, Hocko Marián, Žitek Pavel
Format: Article
Language:English
Published: EDP Sciences 2017-01-01
Series:EPJ Web of Conferences
Online Access:https://doi.org/10.1051/epjconf/201714302114