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Interfacial fracture behavior for GF/epoxy model composites was investigated under static loading using the bifiber shear (BFS) and the bifiber open (BFO) methods.
In fact, the maximum loss modulus in these model composites was found to be about 20 times greater than that given by the theoretical Hashin-Shtrikman upper bound.
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The feasibility of using Raman spectroscopy to map strain fields in model composites is demonstrated by means of two experiments.
Single-fibre model composites are prepared by embedding constrained high-modulus iPP fibres in thin films of a matrix material based on the same isotactic polypropylene grade.
Huang and Kinloch's model developed from composites was found not fit well into these nanocomposites.
A recently developed model for unidirectional composites was extended to hybrid composites to analyse this synergetic effect, called the hybrid effect.
One of the difficulties in modelling fabric composites is an inhomogeneous distribution of fibre yarns in them.
Numerical modelling of composites is becoming ever more important to commercial aircraft manufacturers for design-phase cost reductions and improved lead times.
At an early stage, the main purpose of modelling the ballistic response of composites was not their damage-evolution mechanisms.
Equivalent electrical conduction models of both composites were established using the two mixing rules.
Based on experimental data, the analytical models on polymer composites were developed for simultaneously calculating the thermal property with single or hybrid fillers [25, 26].
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