Properties for Design of Composite Structures. Neil McCartney

Properties for Design of Composite Structures - Neil McCartney


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href="#ulink_4c02f8b0-97e0-5b5b-be5c-1eae0ba48243">2.37) reduces in component form to

      where vj=∂uj/∂t is the velocity vector, uj is the displacement vector and σij is the stress tensor. In the absence of body couples, the principle of the conservation of angular momentum leads to the symmetry of the stress tensor so that σij=σji.

      The principle of the conservation of energy for infinitesimal deformations leads to the following local form of the internal energy balance equation that results from (2.44)

      where u is the specific internal energy, hi is the heat flux vector, r is the rate (per unit mass) at which heat from non-mechanical sources may be locally generated or lost that could arise, for example, from electrical heating and εij is the infinitesimal strain tensor defined in terms of the displacement vector ui by relation (2.107). Relations (2.109) and (2.110) are field equations that must always be satisfied for any type of homogeneous solid that deforms as a continuous medium and is subject to infinitesimal deformations.

      When developing a theory of thermoelastic materials behaviour, it is useful to introduce an equation of state of the following form (a generalisation of (2.67)1 to elastic materials subject to shear deformation)

      where υ^ is a prescribed function of the specific entropy η and the strain tensor εij. The corresponding differential form is written as

      and the thermodynamic temperature T (i.e. absolute temperature, which is always positive) is then defined by the relation

      upper T equals StartFraction partial-differential ModifyingAbove e With caret Over partial-differential eta EndFraction comma(2.113)

      whereas the stress tensor is defined by

      sigma Subscript i j Baseline equals rho 0 StartFraction partial-differential ModifyingAbove e With caret Over partial-differential epsilon Subscript i j Baseline EndFraction period(2.114)

      It follows from (2.110)–(2.114) that the local energy balance equation may be expressed in the form

      upper T StartFraction partial-differential left-parenthesis rho 0 eta right-parenthesis Over partial-differential t EndFraction equals minus StartFraction partial-differential h Subscript i Baseline Over partial-differential x Subscript i Baseline EndFraction plus rho 0 r period(2.115)

      This relation is now rearranged in the form of an entropy balance equation

      where Δ is the rate of internal entropy production per unit volume given by

      upper Delta equals h Subscript i Baseline StartFraction partial-differential Over partial-differential x Subscript i Baseline EndFraction left-parenthesis StartFraction 1 Over upper T EndFraction right-parenthesis comma(2.117)

      where the thermal conductivity κ≥0 can be temperature dependent. The relation (2.118) linearly relating the heat flux to the temperature gradient is the well-known Fourier heat conduction law that demands that heat will always flow from regions of high temperature to regions of lower temperature.

      2.12 Equilibrium Equations

      When a continuous medium is in mechanical equilibrium, the equations of motion (2.109) reduce to the form

      It is useful express the equilibrium equations (2.119) in terms of three coordinate systems that will be used later in this book. In terms of a set of Cartesian coordinates (x1,x2,x3) the equilibrium equations (2.119) may be expressed as the following three independent equilibrium equations (see, for example, [3])

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