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- W2079331397 abstract "Candidate materials for applications in advanced aerospace applications such as gas turbine engines have been identified among the metal matrix composites (MMC's). This special attention is attributed mainly to the superior stiffness to weight ratio as compared to other conventional materials. However, MMC's still lack general applicability due to the lack of appropriate material models capable of describing the material behavior with sufficient confidence. The current research describes the development of a micro-mechanical fatigue damage model for uni-directional MMC's. Micro-mechanical principles are applied in the sense that the behavior of the composite material, specifically the damage and its evolution, are predicted based on the material behavior of the individual constituents. A homogenization procedure in the form of the Mori–Tanaka method is employed. Based on thermo-dynamical principles individual damage criteria and damage evolution models are developed for the respective constituents. The damage due to fatigue is incorporated here through a kinematic-hardening type model for damage which may not be evident in monotonic loading cases. Model and material parameters are identified and their determination is discussed. A few parametric studies show the response of the model with respect to the damage evolution for variations in the described parameters. Results of these parametric studies confirm consistency of the proposed model. A comparison for the number of cycles to failure of a few high cycle fatigue simulations with experimental results reflect good correlation." @default.
- W2079331397 created "2016-06-24" @default.
- W2079331397 creator A5081075067 @default.
- W2079331397 creator A5089422028 @default.
- W2079331397 date "1998-10-01" @default.
- W2079331397 modified "2023-10-14" @default.
- W2079331397 title "High cycle fatigue damage evolution in uni-directional metal matrix composites using a micro-mechanical approach" @default.
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- W2079331397 doi "https://doi.org/10.1016/s0167-6636(98)00040-4" @default.
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