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F.E.M. for Prestressed Saint Venant-Kirchhoff Hyperelastic Membranes 125<br />
quired by the Newton-Raphson iterative scheme for the solution of the nonlinear<br />
equilibrium equations.<br />
The discussion to follow is divided into six parts. The second section reviews the<br />
classical nonlinear strong form equations. The consideration of the Saint Venant-<br />
Kirchhoff material as the adopted model will very conveniently provide a linear<br />
constitutive relationship of easy implementation. The third section entails a comprehensive<br />
explanation of the Finite Element semidiscretization of the previously<br />
obtained strong form. After the weak form is derived in a straightforward manner,<br />
the displacement field is interpolated by means of shape functions based on<br />
aLagrangian mesh geometry. The resulting formulation will be the so called Total<br />
Lagrangian Formulation (TLF). Afterwards, the exact linearization of the Total<br />
Lagrangian weak form of the momentum balance is carried out in detail. For the<br />
sake of further computing implementation reasons, the Direct Core Congruential<br />
Formulation (DCCF) is reviewed as the most appropriate formulation.<br />
Eventually, based on the aforementioned formulation, two numerical examples<br />
for both a cable network and for a prestressed membrane, are presented. These<br />
cases will show adequate performance as the required quadratically convergence of<br />
the Newton-Raphson method is obtained. Some conclusions are presented at the<br />
end.<br />
2 Strong Formulation: General Structural Principles<br />
Before establishing the formulation in terms of particular finite elements, that is, cable<br />
or membrane elements, we will develop in this section the general equations that<br />
govern the behaviour of prestressed membrane structures. For a complete understanding,<br />
it is necessary to consider three successive configurations of the material<br />
body: aninitialnominally stressed state ℜ0, aprimary state ℜt and asecondary<br />
state ℜt∗, for the time instants t and t∗ , respectively. It is important to point out<br />
that the term nominally stressed state is employed to describe a self-equilibrated<br />
configuration where the internal stresses are as small as required by the designer.<br />
Usually, ℜ0 represents the nominally stressed state found at a form finding state.<br />
ℜt symbolizes the actual in service prestressed state prior to the live loading, which<br />
may be different to ℜ0 and due to constructions prestresses. Finally, ℜt∗ stands for<br />
the live loading in service state.<br />
Between these latter two stages, a displacement field u = (u1,u2,u3) may be<br />
defined in R 3 . To differentiate the coordinates of a body particle along the deformation<br />
path, the following convention will be employed throughout the remainder<br />
of this paper:<br />
• XA, (A = 1, 2, 3) for the initial nominally stressed configuration ℜ0.<br />
• X pret<br />
X j , (j = 1, 2, 3) for the initial prestressed configuration ℜt or primary state.<br />
• xi, (i = 1, 2, 3) for the current spatial configuration ℜt∗ or secondary state.<br />
Henceforth, we will consider as incremental those quantities which proceed from<br />
the movement from the primary to the secondary state. The spatial coordinates for<br />
the time t ∗ of a particle can be related to its material coordinates in the initial nominally<br />
stressed configuration ℜ0 according to the classical mapping equation xi =<br />
xi(XA, t ∗ ). By recalling the chain rule, relations among deformation gradient tensors