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- W2363675560 abstract "Structural reliability analysis for aircrafts is necessary for their complex working environment and their terrible results if the structure lapses.In this paper,Spatial girder element and SP panel element are used to model the three dimension spatial aircrafts structure which is more fit for real structure than traditional model to calculate reliability index.Considered the material intensity,girder section area,panel thickness and loads as stochastic variables.stochastic finite element is adopted to analyze the influence of stochastic variables to the nodal displacement.Structural reliability principle is used to evaluate the structure system reliability analysis.Software is developed to implement this theory and is applied to two numerical samples." @default.
- W2363675560 created "2016-06-24" @default.
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- W2363675560 date "2003-01-01" @default.
- W2363675560 modified "2023-09-26" @default.
- W2363675560 title "Structural Reliability for spatial Girder-Panel Structure Based on SFEM" @default.
- W2363675560 hasPublicationYear "2003" @default.
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