Finite element modelling of reinforced concrete framed structures including catenary action

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Abstract

In this paper, a 1D discrete element is formulated for analysis of reinforced concrete frames with catenary action. A force-based formulation is developed based on the total secant stiffness approach and an associated direct iterative solution scheme is derived. The effect of material nonlinearity as well as softening of concrete under compression is taken into account and a nonlocal averaging technique is employed to maintain the objectivity of displacement and force responses. Concerning geometrical nonlinearities, the fibre strains are assumed to be small; however, the effect of transverse displacement on the axial strain is large and it is taken into account as well as the effect of shear on the axial force. Using a Simpson integration scheme, together with a piecewise interpolation of curvature, the deformed shape of the element is consistently updated. The formulation is verified with numerical examples.

Introduction

Catenary action of frame elements when a structure is subjected to extreme loading scenarios, such as blast and fire, can assist the elements to withstand gravity loads and prevent progressive collapse. Accordingly, an accurate progressive collapse assessment procedure has to take account of the catenary effects. The catenary action of steel and composite elements has been studied extensively [1], [2], [3], [4], [5], whereas the effect of catenary action within reinforced concrete elements has not been studied that much, except for a few simplified cases [6], [7].

In a progressive collapse assessment of frames based on an alternate load path, one or two of the load-bearing elements within different scenarios are removed and the ensuing structural response is obtained [8], [9]. In this case, the beams bridging over the removed columns experience large vertical displacements and develop catenary action. In unrestrained reinforced concrete beams, after cracking the neutral axis moves within the section such that at the initial reference axis (i.e. neutral axis of the uncracked section) the strains are tensile. That is the average strain in the member is tensile. However, in a framed structure, due to in-plane axial restraints provided by columns, the member cannot extend freely and these restraints set up axial compressive forces in the beams that must be considered in the analytical model [7].

In 1D frame elements, softening of concrete under compression after peak is associated with a lack of objectivity of the post-peak results and localisation of failure that is observed at either the element or section level, depending on the formulation type [10]. In such cases, the objectivity of response can be maintained by using lumped nonlinearity models with a softening hinge [11], scaling of the constitutive law [10], using a plastic-hinge integration method [12], adopting a nonlocal averaging technique [13], [14], [15], or by using a gradient-dependent plasticity model within the distributed nonlinearity context [16]. In this study the nonlocal averaging method is adopted as it can maintain the objectivity of displacement and moment-curvature responses without additional provisions and the position of plastic hinges are not required to be determined a priori.

In the finite element context, the displacement and force-based formulations, more or less, have the same degree of approximations. For frame elements, however, force-based formulations leads to superior accuracy compared with displacement-based formulations due to exact fulfillment of equilibrium equations [17], [18], [19]. Consequently, in this paper the force interpolation concept within a framework of a total secant stiffness approach is adopted to formulate the element.

Adopting the concept of the “natural approach”, the geometrical nonlinearity is taken into account by decomposing element displacements into a rigid body rotation and deformations [20], [21], [22]. The effect of transverse displacement on the axial strain is taken into account; however, the strains are taken to be small. Further, the formulation takes account of varying axial force along the element caused by geometrical nonlinearity, because the definition of axial load adopted in the formulation includes the second order effects as well as the effect of shear (although small) on the axial force. A composite Simpson integration scheme, accompanied with a parabolic piecewise interpolation of curvature function is used to establish the displacements and rotation of the longitudinal sections required for the geometrical nonlinearity analysis. While the formulation is developed for 2D cases, the requirements for extension to 3D are given in [23].

Section snippets

Compatibility equations

Adopting perfect bond and the Navier–Bernoulli assumptions, section compatibility requirements yieldεx=εr-yκwhere εx denotes the total strain at the integration point in local xx direction (along the element axis, see Fig. 1a), εr denotes the section axial strain, κ denotes the total curvature of section and y is the distance of the integration point (fibre) from the mid-plane of the element and parallel with xz plane (see Fig. 1a).

Fig. 1a shows a two-node plane frame element AB with three

Displacement interpolation along the element axis

It is observed that incorporating the geometrical nonlinearity into the formulation necessitates the deformed shape of the element to be available. In the displacement-based formulation, the deformed shape of the element is obtained based on the nodal displacement values and adopted shape functions. In the force-based element, however, there is no displacement shape function to be used and a different technique is required. Carol and Murcia [24] have used combination of Simpson integration and

Implementation of the nonlocal integral formulation

The transverse deflection of reinforced concrete beams in a framed structure could be associated with compressive force as explained in Section 1. The stresses caused by this compressive axial force combined with compressive stresses caused by bending moment could lead to compressive softening of concrete fibres, which is associated with a lack of objectivity and with spurious mesh sensitivity.

In this study, the concept of a nonlocal integral model is adopted to maintain the objectivity of the

Rigid body motion and corresponding transformation

The flexibility formulation presented in the previous section was derived in the element reference system without rigid body motion. Thus, a transformation is required to relate the deformation and corresponding force vectors in the system without rigid body modes to the system with rigid body modes.

Satisfying the equilibrium equations, the following transformation between the force vectors of the systems with and without rigid body modes can be established (Fig. 6),Q=TTQ¯where Q=[Q1Q2Q3Q4Q5Q6]T

Direct iteration solution scheme

The solution procedure consists of a single loop that carries out the iteration at the structural level and, in which, element equilibrium as well as compatibility is satisfied. If the element is subjected to element load, an inner loop is required to restore the section (element) equilibrium. In the algorithm presented below, the right superscript i denotes the iteration number and right subscript k indicates the load step. If the results at the end of the kth load step are available, then

Linear elastic analysis of a pin supported indeterminate beam

This first example is used to demonstrate the performance of the developed formulation, for a linear-elastic beam and the results are compared with more demanding displacement-based formulations. A statically indeterminate simple beam with pin supports at both ends and subjected to point load at mid-span is analysed (Fig. 7). The elastic modulus is E = 25,000 MPa and as the material behaviour is linear-elastic, there is no need to use the nonlocal formulation. Thus, one half of the beam is

Conclusions

A novel flexibility-based formulation in the framework of the total secant stiffness matrix is derived for 1D frame elements and a direct iterative solution scheme, consistent with the formulation, is presented. In adopting a total secant solution strategy, the positive definiteness of the stiffness matrix is preserved and improves the stability of the solution. Furthermore, the inelastic deformation of the elements at each stage of the loading can be obtained directly without resorting to an

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