Sentence examples for a given composite from inspiring English sources

Omni strain failure envelopes are proposed as the minimum inner failure envelope in strain space, which defines the failure of a given composite material for all ply orientations.

A direct method is also developed to determine the steady-state characteristics from just the initial conditions and configurations of a given composite system.

Property closures delineate the complete set of feasible effective property combinations in a given composite material, and are of tremendous interest in highly constrained design applications.

The effective coefficients are universal in nature and once determined, can be used to examine a number of boundary value problems associated with a given composite geometry.

For example, there are properties of composite (i.e. non-prime) numbers which can be shown to hold in relation to about half of the numbers less than a given composite number.

The temperature dependence of the anisomorphic CFL diagram for a given composite is characterized by the temperature dependence of the static strengths in tension and compression and of the reference S N relationship for a critical stress ratio.

This suggests that these factors partner with multiple TFs in such a way that any given composite site is present in relatively small numbers and thus cannot be detected by the algorithm used.

Or to take a more concrete example, the existence of any given composite object is grounded in the existence of its parts.

This suitable matter brings with it the features required by a given hylomorphic composite.

To calculate the QMEAN Z-score, the normalized raw scores of a given model (composite QMEAN score and individual mean force potential terms) are compared to scores obtained for a representative set of high-resolution X-ray structures of similar size (number of residues of query proteins ±10%).

Simultaneous activation of both synapses gave composite EPSCs, in which Δ increased with the distance between the synapses.