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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

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