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• W2046100342 abstract "Composite Sandwich Materials are being increasingly used in high-performance structural applications because of their high stiffness and low weight characteristics. Presently, the long-term performance of such structures, especially under fatigue loading, is not enough studied. The aim of this paper is to address such fatigue behaviour by using a fatigue model verified by experimentation. The fatigue model is based on the fatigue modulus concept (degradation of stiffness) which is proposed for core-dominated behaviour and for two directions cells (L and W). Two non-linear cumulative damage models (L and W) derived from the chosen stiffness degradation equation, are examined in context with the linear Miner’s damage summation and compared with available experimental results." @default.
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• W2046100342 date "2010-11-01" @default.
• W2046100342 modified "2023-10-17" @default.
• W2046100342 title "Modelling the fatigue behaviour of composites honeycomb materials (aluminium/aramide fibre core) using four-point bending tests" @default.
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• W2046100342 doi "https://doi.org/10.1016/j.ijfatigue.2010.01.005" @default.
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