Properties for Design of Composite Structures. Neil McCartney

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Properties for Design of Composite Structures - Neil McCartney


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state variables. It follows from the three differential relations in (2.54) that

      The total mass of the system denoted by M is given by

      upper M equals sigma-summation Underscript k equals 1 Overscript n Endscripts upper M Subscript k Baseline period(2.57)

      Any extensive state variable P depends directly on the total M of the system and is such that for any value of the dimensionless parameter λ

      upper P left-parenthesis lamda upper M right-parenthesis equals lamda upper P left-parenthesis upper M right-parenthesis period(2.58)

      On applying this principle to the functions introduced in (2.54)

      It follows that the functions U^,F^ or G^ are homogeneous of order unity in the extensive state variables. Provided that λ is independent of the state variables, on differentiating relations (2.59) with respect to λ, and then setting λ=1, it follows on using (2.56) that

      2.9.2 Local Thermodynamic Relations

      The extensive quantities are not used directly in simulations, as local expressions of these thermodynamic quantities defined per mole, per unit mass or per unit volume need to be defined. The approach to be taken here is to define thermodynamic variables per unit mass by introducing the state variables υ,ψ ,φ ,Ω and η using the relations

      implying that

      where υ,ψ​ and φ are the specific internal, specific Helmholtz and specific Gibbs energies, respectively, Ω is the volume per unit mass (i.e. 1/ρ where ρ is the mass density), whereas η and ωk,k=1,…,n are, respectively, the specific entropy and mass fractions for the n species. Substitution of (2.61) into (2.54) then leads to