Sentence examples for laminates in terms from inspiring English sources

Damage in composite laminates in terms of ply failure may primarily occur as fiber fracture or matrix cracking.

Investigation of the as-moulded surface finish showed that the autoclave cured laminates had lower surface roughness than the Quickstep laminates in terms of arithmetic mean (Ra), maximum peak to valley height (Rt), skewness (Rsk) and kurtosis (Rku).

Finite element method (FEM) and IMPGA have been used to obtain optimum laminates in terms of minimizing the cost, weight or both cost and weight of Graphite/Epoxy (T300/5208)–Aramid/Epoxy (Kevlar 49) hybrid laminates.

The design problem formulation relies on a direct parameterization of the laminates in terms of the physical design variables, that is orientations and thicknesses, and not on alternative ones like the lamination parameters.

Using available experimental results obtained with the same test setup, but using RC slabs of higher strength concrete, it can be concluded that as minimum is the concrete strength as more effective is the NSM technique with prestressed CFRP laminates in terms of serviceability limit states.

Minimising disruption to the host laminate, in terms of fibre architecture, is key to the successful implementation of such a technology.

Finite element method (FEM) and genetic algorithm (GA) have been used to obtain optimum laminate in terms of minimizing the cost, weight or both cost and weight of graphite/epoxy (T300/5208)–aramid/epoxy (Kevlar 49) hybrid laminates while maximizing the strength.

However, early occurrence of pull-out and the likely presence of porosity were found to affect the performance of the laminates, especially in terms of the appearance of early damage under impact loading.

The impact behaviour of composite laminates under low velocity impact load is investigated by considering the influence of stacking sequence and laminate thickness in terms of contact loads, absorbed energy and delamination extent.

The comparison of the force time dependencies with the actual effects of the indenter laminate system (using high-speed cameras) contributed to the identification of the representative points and ranges that determine characteristic changes in the laminate structure in terms of damage and specific forms of its degradation.

Based on continuum damage mechanics, the progressive failure analysis using explicit finite element method is performed to predict the failure properties and burst strengths of aluminum carbon fiber/epoxy composite cylindrical laminate structures in terms of three composite pressure vessels with different geometry sizes.