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- W2354110689 abstract "To analyze the fatigue behavior of joint-strengthened component in aircraft, a series of special finite element method (FEM) programs, in which 4-node isoparametric plane elements and two-dimensional rivet elements are used, are presented to analyze the detail stresses of the riveted component. After calculating the detail stresses of joint-strengthened component and determining its fatigue dangerous position, the stress severity factor method is used to calculate the fatigue life of the component and its fatigue safety life is gained." @default.
- W2354110689 created "2016-06-24" @default.
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- W2354110689 date "2001-01-01" @default.
- W2354110689 modified "2023-09-23" @default.
- W2354110689 title "The Analysis of Fatigue Behavior of Joint-strengthened Component in Aircraft" @default.
- W2354110689 hasPublicationYear "2001" @default.
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