The push-out test is generally a key step in the study of the mechanical response of a steel–concrete composite structure. For this reason, in this section, a refined numerical methodology is proposed for the simulation of such a test. Based on refined “classic” 3D numerical modeling, developments in concrete behavior and connector shear modeling are presented.
2.1. Limits of the “Classical” Simulation of a Push-Out Test
The experimental study proposed in [
42] is considered. The ST25-A test is selected from the experimental campaign. It represents the behavior of headed shear studs welded on steel flanges and embedded in concrete blocks. All the characteristics of the components and the methodology of the test follow the recommendations from Eurocode 4 [
4] (
Figure 3).
The relative slip between the steel beam and the concrete blocks is measured as a function of the applied force. It allows us to define the force P per connector—slip
δ behavior law of the connection. The ultimate strength of the connection in shear
(
Figure 4a) has been specifically recorded. The experimental failure mode of the specimen is a shear failure of the stud near the welding point with the steel beam (
Figure 4b).
Because of the symmetry and considering homogenous material properties in the concrete blocks, only one-fourth of the structure is simulated. The concrete block, the steel beam, and the connectors are represented by 3D solid elements, while reinforcements are modeled with 1D beam elements. At the interface between the steel connectors and concrete, the nodes related to each material have the same position. The size of the finite element (the cubic root of its volume) ranges from 1.83 mm (in the connectors) to 1
= 25 mm (away from the connectors) (
Figure 5).
An isotropic damage model [
43] is chosen for the mechanical behavior of concrete blocks. The stress-strain relation is:
where
and
are the stress and strain components respectively,
is the fourth order elastic tensor and
is the damage variable. For the description of the damage evolution, an equivalent strain is introduced from the local strain tensor:
where
are the positive principal strains.
The loading surface
is defined by:
where the damage variable
is also the history variable which takes the maximum value reached by
during the history of loading
is defined by an evolution law which distinguishes the mechanical responses of the material in tension and in compression by introducing two scalars
and
and are the tensile and compressive parts of the damage, respectively. is the initial threshold from which damage grows, it is equal to the ratio between the tensile strength and the Young modulus. The weights and are computed from the strain tensor. They are defined as functions of the principal values of the strains and due to positive and negative stresses, respectively. The parameter reduces the effect of damage under shear compared to tension. and are model parameters characterizing the compression response of the concrete. They are determined to reproduce the compressive strength of the concrete.
Compared to the initial version of the model, for the calculation of
(Equation (6)), a Hillerborg energetic method is used to regularize the damage evolution for any element size [
33]. This method introduces the dependence of the behavior law on the concrete tension fracture energy
and on the element size
.
For the steel studs and beams, an elastic–plastic model with an isotropic hardening is chosen. For the reinforcement, an elastic–plastic law without hardening is used. The material parameters are obtained from experimental data [
42] (
Table 1,
Table 2 and
Table 3).
The loading and boundary conditions are then defined (
Figure 6). First, symmetry conditions are considered on both symmetry faces (zero normal displacements for (conditions a and b)). The concrete block is simply supported on the test set-up, and the vertical displacement is blocked on its bottom face (condition c). A vertical displacement is applied at the top of the steel beam (condition d), and an additional condition is finally imposed on a line at the base of the concrete block to eliminate rigid body movements (condition e).
Particular attention must be paid to bonding conditions at the interfaces between components (
Figure 7A). First, a perfect bond (same displacement at the interface) is imposed between the concrete and the reinforcement, which plays here a secondary role in the mechanical behavior. A perfect bond is also imposed between the stud heads and the concrete block (condition A, the detailed geometry of the stud heads is not modeled in this study; the bond is imposed on the face at the end of the cylinder) and between the stud feet and the steel beam (condition B). Partial bonds at the interface between the concrete block and the steel beam and between the concrete and the studs are then considered (conditions C and D, respectively). They suppose a contact relation that allows for normal separation and a free slip in the tangential directions. In case of contact, equal displacements are imposed on both materials. In the tangential direction, no friction is considered as the studs are oiled before the test.
The simulation is performed using the implicit finite element code Cast3M [
45].
The numerical evolution of the load per stud P as a function of the slip
δ is illustrated in
Figure 8a. A significant difference is noticed in the experimental result. In fact, despite a similar initial phase, a significant decrease in the numerical stiffness leads to an underestimation of the strength by around 20% compared to the experimental mean strength. After the peak, a brittle failure of the system is simulated. The damage distribution of the concrete, illustrated in
Figure 8b, shows an important localization of the damage, which remains concentrated in the concrete elements close to the connectors. In
Figure 9, the distribution of the cumulative plastic strain presents a poor yielding of the steel beam and the connectors, which is not in agreement with the experimental observations. In the following sections, improvements are proposed to overcome these two difficulties.
2.2. Improvement through a Regularization Method in Compression
Because of the highly compressed concrete zones around the connectors, the concrete behavior law needs to be improved. The local description of the mechanical behavior in compression is insufficient, as the stress–displacement evolutions are influenced by the element size. It is thus chosen to adapt the tensile regularization method to the compressive part of the model (
). This choice is made from the assumption that in compression, the slenderness of specimens influences the stress–strain curve but not the stress–displacement response, independently of the height of the specimen [
36,
37,
46,
47]. This justifies the development of a regularization of the concrete compressive behavior, in which the size of the finite elements is integrated into the constitutive laws. To do so, from the definition of
(Equation (7)), the model parameters
and
are calibrated from uniaxial compression simulations to obtain the same stress–displacement curves independently on the values of
(
Figure 10). From this calibration, evolution laws are deduced (polynomial interpolation) for both parameters and applied to the concrete model (Equations (10) and (11)). It is to be noted that this calibration obviously depends on the material properties (compressive strength and softening behavior) and should be recalculated when concrete changes.
Applied to the push-out test modeling, the global behavior of the system with this new concrete model is illustrated in
Figure 11a. A clear improvement is obtained for the load per stud–slip curve. At a slip of
, the numerical load is
with a difference of 4.7% with the experimental mean force. The observation of the concrete damage allows for identifying a larger spread (
Figure 11b), thus confirming the better distribution of the stress. In addition, several tests have been carried out in [
48] and show that the global response is practically independent of the mesh size.
For the post-peak behavior, the experimental failure mode is not reproduced numerically, although a shear pattern can be identified in
Figure 12. The simulation even provides forces that exceed the shear strength of the push-out test (167 kN) calculated from Equation (12) (from [
4] without considering the safety factor), underlining difficulties to reproduce the shear behavior of the steel connectors–steel plates interface.
2.3. Joint Elements for the Steel Connector–Steel Plate Interfaces
As mentioned in the previous section, the shear behavior at the steel connector–steel plate needs to be improved (condition D in
Figure 7). In the push-out test, the most common mode of failure observed experimentally is shearing of the stud near the interface with the steel beam flange. Although this degradation process could be modeled with classical finite element methods, the required spatial discretization would be so fine that it would be inapplicable in terms of numerical cost. For example, an element size of 0.5 mm would be needed to reproduce the pure shear behavior of a single steel bar welded on a steel plate (without concrete) tested in [
25], leading to a very large number of elements (
Figure 13). With a mesh discretization like the one used in the push-out modeling, an important overestimation of the system strength is visible.
To overcome this difficulty, additional junction elements are developed to represent this shear behavior with an acceptable computational cost. They are zero-dimensional spring elements, which connect each node of the stud to the associated node of the steel plate through an orthotropic constitutive law. In the longitudinal direction of the stud (normal to the cross-section), a linear elastic law is supposed. Its stiffness is chosen high enough (
) to reproduce the welding of the stud on the plate. In the tangential directions (respectively,
y and
z), an elastoplastic law is imposed. The initial stiffness is equal to the normal one, while the plastic criterion is classically written as a function of the force:
with
the hardening parameters in the directions
and
and
the shear strength of the steel stud, calculated from EC4 [
4] without the safety factor (Equation (14)).
where
is the ultimate tensile strength of a shear stud and
is the stud cross-section. For the hardening parameters, a linear kinematic behavior is supposed through
variable. Applied to the push-out test, these junction elements are added at the interface between the studs and the steel beam (condition B in
Figure 14). For the plastic behavior, the yield point is determined from Equation (14),
and the plastic slope is
to ensure a quasi-horizontal plateau.
The numerical evolution of the load per stud P as a function of slip
δ is illustrated in
Figure 15a. Experimental and numerical results agree, and the three major phases of the mechanical behavior are correctly reproduced. The elastic phase (phase I) and the degradation phase (phase II) meet the experimental results, and a horizontal plateau at the shear strength of the stud (
) is finally observed. It is to be noted that the softening behavior is not modeled in the constitutive law of the interface elements. That is why no softening behavior can be numerically obtained.
Figure 15b illustrates the damage evolution.
Significant damage is observed under the studs, which characterizes concrete crushing. The cumulative plastic strain distributions of the steel beam and of the steel studs (
Figure 16) show shear yielding. Large plastic strains develop at the interface for both elements. These qualitative observations confirm the capacity of the model to reproduce the shear behavior through the junction elements, which leads to a shear failure of the studs in agreement with the experimental observations.
With this refined modeling strategy, several other experimental push-out tests of the literature (different geometries and material characteristics) have been simulated [
48]. Numerical results are in good agreement with experimental ones.