Abstract The paper presents a technique of calculating the life for gas turbine engine parts in a low cycle area based on the influence coefficients taking into account analytical and operational factors. A statistical method is used to determine the influence coefficients.
Calculation of low cycle fatigue life for gas-turbine engine critical parts
Russian Aeronautics ; 60 , 3 ; 421-427
2017-07-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Calculation of low cycle fatigue life for gas-turbine engine critical parts
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