INTRODUCTION

In butt-welded joints the geometrical profile and the fracto-mechanical material properties have a high influence on the resistance to fatigue. Certain geometrical factors, such as the radius of the weld toe (ρ) and the over thickness weld (s), affect the initial period of fatigue cracks ^{1}: after the initiation period of the crack, its propagation speed will depend, in a big deal, on the fracto-mechanical properties of the material. In welded joints, mainly, these properties do not remain constant in all areas of the joint, due to the thermic gradient that is generated in the welding process. Therefore, three well-defined zones with different grain size and microstructure can be observed, as a result of the microstructural coalition, named the fusion zone (FZ), the heat affected zone (HAZ) and the base metal (BM) ^{2}.

The surface cracks, which are generally present by fatigue of welded joints, are semi-elliptical in the radius of the weld toe. This geometry allows carrying out the crack behavior, by mathematical assessments, through Mechanical Fracture based on the stress distribution, deformation and displacements in front of the fracture through the stress intensity factor (K) ^{(}^{3}; it is also possible to assess the crack propagation by fatigue in welded joints after using the empirical relation proposed by Paris and Erdogan ^{4}:

As it is obtained:

Where da/dN is the crack growth per cycle; C and m are material constants for a specific stress ratio R; Δσ is the nominal stress range; β is a dimensionless function that depends on the geometry of the component and the crack size; ΔK is the stress intensity factor range; and a is the crack depth (the subindices i and f indicate the initial and final crack depth respectively). The fatigue strength in welded joints can be expressed as the quantity of necessary cycles for a semi-elliptical shape surface crack gets propagated through the thickness of the joint ^{(}^{5}.

In welded joints stress fields at the crack are more complex to determine due to microstructural alterations, typical of welded joints because of cooling thermic cycle ^{6}. An equation to calculate K in semi-elliptical surface cracks has been developed by ^{7}, describing a weight function through a surface crack on a plate and an edge crack in a semi-infinite plane. In ^{8} Maddox introduced a dimensionless factor Mk, which allows estimating the influence of stress concentrations generated by the geometric profile of fillet welded joints over the stress intensity factor. This analysis is based on semielliptical surface cracks by fatigue located around the weld toe, where the Mk factor is obtained by the relation of stress intensity factor estimated by the Finite Element Method and the nominal value of K (denominator of the equation), as shown in equation (3).

Where σ is the nominal stress.

According to a review ^{9} to estimate the fatigue life on welded joints is common to assess the phase of stable propagation of cracks only. In comparison to the initiation phase cracks, the propagation is extensive. Likewise, the crack propagation allows assessing, as a whole, the fracto-mechanics and geometrical properties of welded joints, as well as, the behavior of different structural elements and cracks through weight/element analysis of finite functions ^{10}^{-}^{4}. The Finite Elements Method allows determining the obtained stresses expressing them as a polynomic equation (4).

Where K can be expressed as shown in equation (5):

Where x is the distance front the crack tip; a is the crack depth; c is the semi-length of the crack and t is the thickness of the base plate.

In ^{12} the distribution of K at the crack tip was assessed for 27 semi-elliptical surface cracks located at the weld toe, which are subjected to eight types of main stresses throughout the analysis of finite elements utilizing a net of iso-parametric elements 20-Node in 3-D. However, as it relates to the analysis in the butt-welded joints did not take into account the influence of over thickness weld. On the other hand in ^{(5)} carried out a research which assessed a great set of geometrical parameters related to butt-welded joints and their influence on the crack propagation by fatigue. Throughout the Mechanics of Elastic Linear Fracture, the analysis of finite elements and superposition theories could estimate a mathematical model that can determine the fatigue resistance in butt-welded joints. There are several methods to get the K values in surface cracks, as it is shown on ^{13}, where a majority of these methods rely on the analysis of the finite elements. The latter allows generating results of high precision, even though an efficient program is required to generate the best tetrahedral mesh based on the type of crack and applied environmental conditions. To be able to utilize the method of weight function is vital to know the crack geometries and the welded joint. For instance, in ^{(13)} state an equation (6) for the weight function for K in the following manner:

Where σ is the normal stress applied in the crack plane; u is the respective displacement; E the elastic module and υ is the Poisson relation for the material. The exponents (1) are known reference solutions, and (2) is for arbitrary loads that should be calculated.

The integral of the left side of (6) is in function of the perimeter of the crack Γc and the right side is in function of the surface are of crack Ac.

To estimate K values based on finite element analysis requires a fine tetrahedral mesh around the

front of the crack or special tools that include the particularities of the stress in the tip of the crack.

Because the conventional elements do not consider the stress-deformation variation in the crack as it is explained in ^{14}. One of the methods used to improve the quality of the results to better assess the singularity, without reaching the limit of all refining elements was developed by ^{15}, which one central node is displaced at one side of the quadrilateral that holds the iso-parametric elements in an 8-noded manner, up to reaching a quarter node located in the crack. When the central node is located, one of the quadrilateral sides to a quarter of singularity even more precise results are obtained for K. The estimation of elastic linear deformation on ANSYS is obtained from the SOLID 186 elements with 3-D and 20-noded brick, because they allow to state, in a precise manner, the range of stress from the resulting singularity by the displacement of central nodes on one of the quadrilateral side to a quarter of singularity, as it is expressed in ^{16}. In this work, a study was carried out about fatigue failures in buttwelded joints for a structural steel to carbon ASTM A36, by using the electric arc welding process with a coated electrode E6013; in which the influence of the joint geometry throughout the analysis of finite elements based on the propagation of semi-elliptical cracks by fatigue in the weld toe. As a result from the study, a set of mathematical models was obtained for the weld magnification factor (Mk) for weldbutt joints, which it useful for the later analysis of tolerance to failure and the forecasting of fatigue life in the welded joints.

MATERIALS AND METHODS

An analysis that included three different levels for two geometrical factors: the radius of the weld toe and the excess thickness of the ϱ and s weld bead, respectively. Table 1 shows the different geometrical combinations used. In order to determine the resistance to fatigue for the butt-welded joints through the SMAW process, the parametrized geometry that appears on Figure 1 was utilized. The latter was the result of metallography tests and analysis of digital images of geometrical profiles from several butt-welded joints by utilizing CAD software, as shown on Figure 2. The levels of the factors used in the current experimental arrangement match to common real values of weld overthickness and radius of the weld toe measured experimentally. The material of the joint is defined as base structural steel ASTM A36, thickness of 6 mm, and elastic boundary of 262 MPa and stress resistance of 434 MPa. On the other hand, the input material is coated electrode E6013, 1/8 inch diameter, and elastic boundary of 360 MPa and stress resistance of 500 MPa.

For the welding procedure, the butt flat position, with a square joint design was used according to

^{17}, one voltage between 15 - 42 V, and current between 85-140 A (direct current). The welding speed was between 2 and 3 mm/s. The applied passes changed regarding the size of the excess thickness in the following way: a pass of weld for s = 1 mm and two welding passes for s = 2 and 3 mm, respectively. The general geometry analysis is shown in Figure 3. The fundamental goal to obtain these joints via experiments was the later digitalization of the over thickness weld profile, so that the solid model of the joint would simulate the real geometry with high fidelity.

One of the tools utilized to assess the propagation of cracks by fatigue in the butt-welded joints is the Linear Elastic Fracture Mechanics though the the Finite Elements Method. In this research, the ANSYS 14.5 software was utilized, with which it is expected to reach representative values of the stress intensity factor, and from (3) to establish an analytical model based on the Mk factor and the influence of the nine geometric combinations showed in Table 1. To reach M_{k} in function of the relation of crack size (a) and coat thickness (t). Through experimental results, the mechanical properties decided for three new materials in ANSYS's Workbench library, simulating three representative zones of butt-welded joints (FZ, HAZ and BM) according to with results obtained by ^{(18)}. The simulated cracks always propagated through the HAZ zone.

A tetrahedral mesh was selected for three most adjacent zones to the crack, by the restriction of the fracture module. In other two adjacent zones, a mesh of automatic generation was utilized. Moreover, a convergence analysis was realized to estimate the quantity of necessary elements, in order to reach a value for the stress intensity factor, independent from the mesh density, in each of the crack sizes utilized in the analysis. In average, 819 939 nodes and 553 283 elements were used per each case. The contour conditions and the location of the semi-elliptical crack can be observed in Figure 4 for a load ratio R = 0.05, an axial cyclical load of 12 120 N and fixed supports in the low end. For the size of the cracks, an aspect ratio was used a/2c=0.25, based on the experimental observations of analysis of the failures in butt-welded joints. The initial superficial semi-elliptical crack is located adjacent to the weld toe and in the middle plane of the plate. This site, close to the weld bead, has high local stresses and has been experimentally proven to be the site of highest probability of initiaton and spread of fatigue cracks ^{18}.

DISCUSSION AND RESULTS

The effect generated by the combination of the excess thickness s and the radius in the weld toe ϱ in butt-welded joints can be observed in Figures 5 and 6, for the combinations 1 and 3 from Table 1, respectively. Figure 5 shows a concentration stress in the weld toe of the over thickness weld, much less than that presented in Figure 6. It is important to highlight, that in these two combinations, the same value for ϱ used. However, it is possible to observe clearly that, increasing the value of can make the concentration of stress greater. Due to the fact that in the over thickness weld appear the greatest stress concentration. As reference, this location was utilized as to the different sizes of semi-elliptical centered crack, in order to carry out the simulations of fatigue cracks propagation.

In Figure 7 the behavior of the magnification factor is presented in the crack of the weld toe, in function of the dimensionless depth of the crack, for the 9 treatments of Table 1. The values have been obtained for the deepest point of the crack.

In the equation (7), the polynomial functions obtained analysis of regression are presented, for the curves in Figure 7 corresponding to the treatments 1, 3 and 5, respectively.

Using the Mk factor (see Figure 7) for the treatment number 5, a comparison is made with the reported results by different authors, for butt-welded joints 3D ^{19}, welded tubular welded structures ^{20} and the solution based on analysis by finite elements in 2D presented by ^{21}, as shown in Figure 8.

To assess the differences between three models of reference in Figure 8, a percentage variation analysis was made in equation (8) a function of dimensionless crack size (a/t). The results are shown in Table 2. It is important to highlight that the minimum percentage of variation is 2.74 % for the model of ^{(19)} and the maximum is 66.79 % for the model of ^{(21)}. These last two results are in the range a/t = 0.017-0.050.

Another relevant result to assess the characterization of fatigue is the behavior of the SIF in function of the perimeter of the crack. In the Figures 9 and 10 the behavior of the SIF appears for the conditions or treatments 1 and 3, in function of the position on the crack, as for semi-elliptical cracks, with initial aspect ratio a/2c=0.25. Likewise, KI behavior for eight sizes of crack shaped is shown. It can be seen that a progressive transition in KI behavior, for small cracks, the function is convex and the greatest value appears at the back of the crack, whereas for big cracks, the positions of the ends of the front of crack reach the maximum values for KI.

This effect makes different rates of crack propagation along its base. Therefore, a semielliptical surface crack of type will be diminishing its aspect ratio, as it becomes larger.

In Figure 11 the results of the stable crack propagation for the nine treatments from Table 1 are shown, obtained from (2). For ai=0.1 mm; a_{f}=2 mm; C=1.65x10^{-11} [m/cycles] and m=3, according to information supplied by ^{(21)}; finally, Δσ=192 MPa. In Figure 11, it is possible to observe the generated grouping between the analysis treatments. In this case, the three treatments with major fatigue life (treatments 1, 4 and 7), have the over thickness weld size equal to s=1 mm. On the other hand, the treatment 3 is the one resulting with less fatigue life, with over thickness weld size equal to s=3 mm. A difference in fatigue life as high as 42% is predicted between the two over thickness used in the present research.

CONCLUSIONS

The main contribution of the current research is the set of expressions for M_{k} obtained as a function of the geometric parameters over thickness and weld toe radius in butt-welded joints. For this, a 3D finite element model is used, where the differentiation of the mechanical properties of the BM, HAZ and FZ zones is performed. Also, the present work model emulates the actual geometric configuration of butt-welded joints.

It can be concluded the influence of the excess thickness of the bead weld is more significant in the fatigue life of the welded joint, compared with the effect that makes the radius of the weld toe. Although both geometric factors have a significant influence and, therefore, should be considered in an analysis of life management. A major excess thickness, inside the variation range used in the current study, means a reduction in the prediction of fatigue life of up to 42 % for the welded joint.

Analytical equations are obtained for Mk that can be used in models of life management and tolerance to the damage of butt-welded joints, on similar type, in function of the geometric characteristics of the joints. When other authors' results ^{(19-21)} are contrasted, M_{k} analytical functions result with low trend values in its behavior, for small cracks; then for a/t> 0.18 begin to differ in a minimal manner. The differences observed between the current study and those from other authors might be fundamentally due to particularities, such as the profile of the butt-welded joints, employed in the different models.

Finally, the influence of the geometry of the bead weld, in the behavior of the stress intensity factor in the crack perimeter is analyzed. It is shown, in every model, that a semi-elliptical surface crack reduces its aspect ratio, as it increases its size, due to the different magnitudes that reaches the stress intensity factor, which leads to different propagation rates on the perimeter of the crack vertex. The results reached in the present research should be used carefully, until they can be experimentally proved with more results.