where Dis the tangent matrix dependent on the state variables and history and ε 0corresponds to thermal and creep strains.
The main variables of the problem are thus uand p w. The effective stresses are determined at any stage by a sum of all previous increments and the value of p wdetermines the parameters S w(saturation) and χ w(effective area). On occasion, the approximation
(3.16) 
can be used.
An additional equation is supplied by the mass conservation coupled with fluid momentum balance. This is conveniently given by (2.33b)which can be written as
(3.17) 
with k= k( S w).
The contribution of the solid acceleration is neglected in this equation. Its inclusion in the equation will render the final equation system nonsymmetric (see Leung 1984) and the effect of this omission has been investigated in Chan (1988) who found it to be insignificant. However, it has been included in the force term of the computer code SWANDYNE‐II (Chan 1995) although it is neglected in the left‐hand side of the final algebraic equation when the symmetric solution procedure is used.
The above set defines the complete equation system for solution of the problem defined providing the necessary boundary conditions have been specified as in (2.18)and (2.19), i.e.
(3.18) 
and
Assuming isotropic permeability, the above equation becomes
where
is the influx, i.e. having an opposite sign to the outflow
.
The total boundary Γ is the union of its components, i.e.
3.2.2 Discretization of the Governing Equation in Space
The spatial discretization involving the variables uand p wis achieved by suitable shape (or basis) functions, writing
(3.19) 
Note that the nodal values of the pore pressures are indicated with a superscript.
We assume here that the expansion is such that the strong boundary conditions (3.18)are satisfied on Γ uand Γ pautomatically by a suitable prescription of the (nodal) parameters. As in most other finite element formulations, the natural boundary condition will be obtained by integrating the weighted equation by parts.
To obtain the first equation discretized in space, we premultiply (3.8)by ( N u) Tand integrate the first term by parts (see for details Zienkiewicz et al (2013) or other texts) giving:
(3.20) 
where the matrix Bis given as
(3.21) 
and the “load vector” f (1), equal in number of components to that of vector
contains all the effects of body forces, and prescribed boundary tractions, i.e.
(3.22) 
At this stage, it is convenient to introduce the effective stress see (3.12)now defined to allow for effects of incomplete saturation as
(3.23) 
The discrete, ordinary differential equation now becomes
(3.24) 
where
(3.25) 
is the MASS MATRIX of the system and
(3.26) 
is the coupling matrix‐linking equation (3.23)and those describing the fluid conservation, and
(3.22 \ bis) 
The computation of the effective stress proceeds incrementally as already indicated in the usual way and now (3.15)can be written in discrete form:
(3.27) 
where, of course, Dis evaluated from appropriate state and history parameters.
Finally, we discretize Equation (3.17)by pre‐multiplying by ( N p) Tand integrating by parts as necessary. This gives the ordinary differential equation
(3.28) 
where the various matrices are as defined below
(3.29) 
(3.30) 
(3.31) 
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