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Fiber/matrix debond with circular front is assumed to be originated from the fiber break.
Finite element analysis of the stress transfer mechanisms around a fiber break in the RVE was performed via ABAQUS/Standard.
The stress transfer profiles during mechanical loading emanating from the fiber break(s) can be obtained by means of the technique of laser Raman microscopy.
Multifiber composites were placed under constant load creep tests and the fiber strains were evaluated with time after one fiber break occurred.
In the study, ABAQUS USDFLD is used to simulate the fiber break and ABAQUS UMAT is employed to simulate the matrix cracking.
However, the fatigue fracture is very sensitive to a fiber break, and to microstructural features such as grain boundaries and dislocation structures.
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The fiber breaks with fiber splitting.
Tensile failure involves delamination, fiber pullout and fiber breaking.
The simulations include delamination, matrix cracks and fiber breaks.
For each harvest mode, the fiber breaking strength was greatest in the first ramie harvested.
Too much energy, they discovered, damages individual tubes so much that the fiber breaks down into an amorphous mass.
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