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- W1503170498 abstract "Presented are techniques based on 3-D finite-element analysis for the examination of continuous fiber reinforced metal matrix composites. Examples are shown for specific metal matrix composites such as boron/aluminum and silicon-carbide/aluminum. Specimen stress-strain behavior and stress at first fiber failure were predicted for boron/aluminum laminates containing circular holes and crack-like slits. The predictions compared very well for (+ or - 45) sub 2s laminates. Mesh configuration was shown to have an effect on the calculation of stresses local to the notch. The presence of thin interface layers of matrix material had a significant influence on the slit-tip stress state, causing sharper stress gradients near the notch. Interface layers reduced the slit-tip fibers stresses in a (+ or - 45) sub s silicon-carbide/aluminum laminate but increased them in a (0/90) sub s laminate." @default.
- W1503170498 created "2016-06-24" @default.
- W1503170498 creator A5082150439 @default.
- W1503170498 date "2008-12-04" @default.
- W1503170498 modified "2023-09-26" @default.
- W1503170498 title "Analysis of Notched Metal Matrix Composites Under Tensile Loading" @default.
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- W1503170498 doi "https://doi.org/10.1520/stp22852s" @default.
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