Properties for Design of Composite Structures. Neil McCartney

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cosine theta comma"/>(4.82)

      A comparison of (4.72) and (4.82) with (4.77) and (4.83) indicates that the identification α=τ/2 can be made. It then follows from (4.81) that

      upper A equals StartFraction mu Subscript m Baseline Over mu Subscript upper A Superscript f Baseline plus mu Subscript m Baseline EndFraction tau comma StartFraction beta Over a squared EndFraction zero width space equals one-half StartFraction mu Subscript m Baseline minus mu Subscript upper A Superscript f Baseline Over mu Subscript upper A Superscript f Baseline plus mu Subscript m Baseline EndFraction tau period(4.84)

      Substitution into (4.72) leads to the following expression for the displacement component uz:

      It should be noted that when fibre is introduced, the displacement components are perturbed as a second term appears in expression (4.85) for the matrix displacement that is inversely proportional to the radial distance r. This additional term will now be considered when applying Maxwell’s method of estimating the effective properties of a fibre-reinforced composite.

      4.4.3 Applying Maxwell’s Approach to Multiphase Fibre Composites

      Owing to the use of the far-field in Maxwell’s method for estimating the properties of fibre composites, it is possible to consider multiple fibre reinforcements. Suppose in a cluster of fibres that there are N different types such that for i = 1, …, N, there are ni fibres of radius ai. The properties of the fibres of type i are denoted by a superscript i. The cluster is assumed to be homogeneous regarding the distribution of fibres, and this leads to transverse isotropic effective properties.

      For the case of multiple phases, relation (4.85) is generalised to the following form:

      When this result is applied to a single fibre of radius b having effective properties corresponding to the multiphase cluster of fibres, it follows that

      The cluster of all types of fibre is now considered to be enclosed in a cylinder of radius b such that the volume fraction of fibres of type i within the cylinder of radius b is given by Vfi=niai2/b2. The volume fractions must satisfy the relation

      upper V Subscript m Baseline plus sigma-summation Underscript i equals 1 Overscript upper N Endscripts upper V Subscript f Superscript i Baseline equals 1 period(4.88)

      It then follows that (4.86) may be written in the form

      The coefficients of the 1/r terms in relations (4.87) and (4.89) must be identical so that

      sigma-summation Underscript i equals 1 Overscript upper N Endscripts upper V Subscript f Superscript i Baseline StartFraction mu Subscript upper A Superscript f left-parenthesis i right-parenthesis Baseline minus mu Subscript m Baseline Over mu Subscript upper A Superscript f left-parenthesis i right-parenthesis Baseline plus mu Subscript m Baseline EndFraction equals StartFraction mu Subscript upper A Superscript eff Baseline minus mu Subscript m Baseline Over mu Subscript upper A Superscript eff Baseline plus mu Subscript m Baseline EndFraction period(4.90)

      It then follows on using (4.1) that the effective axial shear modulus for the multiphase composite may be written as

      4.5 Transverse Shear of Multiphase Fibre Composites

      Consider a cluster of n cylindrical fibres of the same radius a embedded in an infinite matrix having different properties. The cluster is just enclosed by a cylinder of radius b and the fibre distribution is sufficiently homogeneous for it to lead to transverse isotropic properties for the composite formed by the cluster of fibres and the matrix lying within this cylinder. If the fibre volume fraction of the composite is denoted by Vf then

      

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