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- W2362580348 abstract "Aiming at the forth blade-disc of a certain gas turbine,the multiaxial stresses effect is considered in the life prediction analyzing.Three variants of critical plane models are introduced,identifying the critical plane as the plane associated with the maximum damage and a computer-based procedure for multiaxial fatigue life assessment incorporating critical plane multiaxial damage models is presented.Also actual engineering instance was done with these models.The computational results show that multiaxial fatigue life prediction based on critical plane models has an upper precision.Especially,the amendatory Fatemi-Socie(FS) model for fatigue life prediction well consistent with the result of real blade-disc fatigue life,and the FEM which is applied in this paper is useful.Consequently,the results satisfy the applications of practical engineering." @default.
- W2362580348 created "2016-06-24" @default.
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- W2362580348 date "2010-01-01" @default.
- W2362580348 modified "2023-09-27" @default.
- W2362580348 title "Research of Fatigue Life Prediction of Multiaxial Low-cycle for A Gas Turbine Disc and Blade" @default.
- W2362580348 hasPublicationYear "2010" @default.
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