Computational Study of Cold-Formed-Steel X-Braced ShearWalls

-e aim of this paper was to present a verified finite element method that represents the full-scale-braced shear walls under seismic loads and to study their ductility. -e models account for different types of material and geometric nonlinearities. -e screws that connect the cold-formed-steel (CFS) studs, tracks, gusset plates, and braces are considered explicitly in the model. -e deformation of the hold-downs under the horizontal load is considered. -e finite element program ANSYS (2012) is used to model and analyze the case studies. A parametric study is performed to investigate the responsemodification factor (R) of the CFS-braced shear walls. -e parametric study showed that the North American Specification is about 20% conservative in estimating the (R) factor.


Introduction
A noteworthy increase has occurred in the use of the light gauge cold-formed-steel framing in the residential buildings in the last few decades.In Egypt, cold-formed-steel is generally used in the industrial buildings as roof purlins and side girts.Recently, with the spread of the usage of the CFS in residential buildings, some buildings are constructed with CFS in Egypt like the Digital Library in Cairo University.International specifications like Canadian and North American specification concentrated on the use of CFS-braced shear walls depending on several researches.ese specifications are studied in this research.e use of cold-formed-steel has many advantages such as durability, lightweight, recyclability, and rapid construction.ese advantages are essential reasons for this growth in CFS construction.
A CFS strap-braced shear wall consists of vertical studs collected by top and bottom tracks.Diagonal strap braces are added to give the wall lateral stability.All these elements are connected with screws or welds.e shear wall components are designed to transfer the lateral earthquake load to the foundations.e diagonal strap brace was detailed to develop plastic deformations that would dissipate earthquake energy and allow ductile behavior.
Uang [1] derived the basic formulas for establishing the response modification factor R and the displacement amplification factor Cd used in the National Earthquake Hazards Reduction Program (NEHRP) recommended provisions.
ese terms are primarily functions of both the structural overstrength and structural ductility factors.
ese factors could be concluded from monotonic inelastic limit load analysis and widely used by researchers to investigate the reduction factor R.
Al-Kharat and Rogers [2][3][4] performed several full-scale tests on CFS strap-braced shear walls with different aspect ratios.Monotonic-and cyclic-braced walls tests showed that when the capacity design requirements were used, a ductile behavior was reached. is was achieved by designing the strap braces as a fuse member while designing other wall elements to sustain the expected brace capacity.ose experimental results are computationally verified in this study.
Casafont et al. [5] made an experiment on the screwed connection of the strap.ey found that the Eurocode formulas give good estimation for the connection failure.
Hatami et al. [6] conducted laboratory tests on 2.4 m × 2.4 m CFS shear walls with perforated straps.ey found that the brittle failure mode of net section fracture at connection screw holes locations disappeared when the perforated straps are used which resulted in ductile behavior.
Velchev et al. [7] evaluated typical weld-and screwconnected single-story strap-braced walls with respect to their ability to resist lateral in-plane loads in the inelastic range.e results were used to verify the new strap-braced wall seismic design provisions in AISI S213 [8].A total of 44 tension-only X-braced walls with aspect ratios from 4 :1 to 1:1 were tested under lateral loading using monotonic and reversed cyclic protocols.R factors were calculated based on the measured ductility and overstrength of the test walls and compared with the values recommended by AISI S213 [8].
Mahmoudi and Abdi [9] evaluated overstrength, ductility, and response modi cation factors in special moment-resisting frames with TADAS (triangular-plate added damping and sti ness) devices.e R-factor for special moment-resisting frames with and without TADAS devices has been determined separately.
Abu-Hamd and El-Samman [10] investigated the buckling strength of the built-up cold-formed I-sections made of two CFS back-to-back C-sections.ese columns are generally used as chord studs in CFS-braced shear walls.
Landolfo et al. [11] performed laboratory tests for twelve full-scale X-braced shear walls of dimensions 2.4 m (width) × 2.7 m (height) under monotonic and cyclic loading.ey concluded that when the capacity design criteria are performed, the undesirable brittle failures of connections, tracks, studs, and anchorages did not occur.ose monotonic test results are also computationally veri ed in this study.

Methodology and Scope of Work
Two main objectives are targeted in this research to perform nonlinear veri cation analysis for CFS-braced shear walls that were previously tested by other researchers and to perform parametric study using the nonlinear FE model that is already veri ed and thus investigate the response reduction factor R.  is model should investigate four main parameters: (1) the CFS shear wall behavior within the elastic range, (2) the wall strength at yielding, (3) the wall ultimate strength, and (4) the reason of failure.All parameters are compared with test results, namely, six veri cation specimens that were tested by Al-Kharat and Rogers [4] and by Landolfo et al. [11].
Using the program ANSYS, veri cation case studies are considered to insure the accuracy of our model.e main nite element used in the model is SHELL181 for the studs, tracks, gusset plates, hold-downs, and braces.SHELL181 is suitable for analyzing thin shell structures and is widely used to model CFS.
is element has good convergence and accounts for both geometric and material nonlinearities.is element is shown in Figure 1 and described in details in the manual of ANSYS [12].
e screws connecting the studs were modeled using "coupling set" in the out-of-plane while the shear nonlinear failure in-plane mode of the screws is modeled using two nonlinear spring elements COMBIN39.COMBIN39 is a unidirectional element with nonlinear generalized force-de ection capability that can be used in any analysis.e element has longitudinal or torsional capability in 1-D, 2-D, or 3-D applications.e longitudinal option is a uniaxial tension-compression element with up to three degrees of freedom at each node: translations in the nodal x, y, and z directions.No bending or torsion is considered.e forcede ection curve should be input such that de ections are increasing from the third (compression) to the rst (tension) quadrants.If the force-de ection curve is exceeded, the last de ned slope is maintained.e element input is shown in Figure 2, and more details are given in the manual of ANSYS [12].
e displacement occurs at the hold-downs, and the oor below the wall is also modeled using nonlinear spring COMBIN39 with di erent real constants input to be similar to that concluded by Buonopane et al. [13].Contact elements surface to surface (TARGE170 and CONTA174) are used to model the connections between the bracing and the gusset plate.Details about both elements are described in the manual of ANSYS [12].

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At rst, both compression and tension braces were modeled and then compared to tension bracing only.Much time in the analysis was clearly saved while having similar results.erefore, only the tension diagonal brace is considered in FEM to simplify the analysis as it is used only for monotonic loading.

Modeling of Boundary Conditions (Out-of-Plane Support).
As done in experiments, a horizontal out-of-plane roller support is assigned at each top track node to prevent the movement out of plane but allow the movement vertically and horizontally in-plane.

Modeling of Hold-Downs and Anchor Bolts.
From previous tests, there is a portion of the displacement that occurred due to the vertical displacement of the hold-down under the tension reaction.e reference nodes de ning the hold-down elements are connected to nodes on the ground in the vertical direction via a bilinear spring.is modeling    4 Advances in Civil Engineering choice is based on the study of Buonopane et al. [13] in which modeling the tension exibility of the hold-down is established.Herein, the tension sti ness of the hold-down is selected to be 10 kN/mm based on Leng et al. [14].e compression sti ness is chosen to be thousand times of the tension sti ness based on the assumption that axial force in chord studs is transferred by bearing to the foundation when the hold-down is in compression.
e bilinear spring connecting the reference node to a node on the ground is modeled by means of nonlinear spring element type COMBIN39 in ANSYS.Advances in Civil Engineering plates and the braces as a result of the inclination of the braces, it was decided to do the assembly by using contact element provided in ANSYS. is simulation is good enough because connections are always overdesigned, and failure will occur outside the connection, in the brace itself.

Screws Connection: Nonlinear
Behavior.As mentioned before, the screws connecting the studs modeled using "coupling set" in the out-of-plane while the shear nonlinear failure in-plane mode of the screws is modeled using two nonlinear spring elements COMBIN39.Serrette and Peyton [15] reviewed the design provisions for screw-fastened coldformed-steel connections in the United States.In addition, they examined the relationship between the connected elements, computed connection strength, and the strength of the connector.ey also prepared fastener-strength tables for the three manufacturers based on testing.Corner [16] predicted the tilting angle and the limit states of singlefastened cold-formed steel-to-steel shear connection.
According to the steel plate thicknesses studied in this research, the screw strength is modeled as shown in Figure 3.

Nonlinear Analysis
Steps.In order to consider the geometrical and material nonlinear behavior in such cases, two types of analyses are considered.e rst is an eigen buckling analysis that predicts the buckling modes and 6 Advances in Civil Engineering buckling frequencies.In this problem, the material behavior is assumed to be elastic, and the member is considered to have perfect geometry.e lowest buckling modes predicted from the eigen buckling analysis are subsequently used to model the geometric imperfections.To model the overall imperfections, typically L/1000 is used as the magnitude while the first global buckling mode shape is used for the distribution shape.On the other hand, local buckling magnitude is considered as half of the wall thickness according to Zeinoddini and Schafer [17] and using the first local buckling mode shape.e second type of analysis is a nonlinear loaddisplacement analysis of the real wall structures under the action of applied loads in the presence of initial geometrical imperfections and material nonlinearity.e ultimate strength and failure modes are determined from this analysis when they reach the limit point located on its equilibrium path.At this limit point, the corresponding load parameter value and deformed configuration provide the wall ultimate strength and failure mode.

Description of Al-Kharat's Case Studies
ree square specimens were tested with dimensions 2.44 × 2.44 m.Each specimen consists of 2 chord studs of built-up I-shaped CFS C-shaped studs.Five vertical intermediate C-shaped studs were spaced at 406 mm.All studs were collected using top and bottom U-shaped tracks using hex-washer-head self-drilling screws.X-braces were connected to tracks and chord studs using screwed gusset plates.e dimensions and materials of all elements differ from one specimen to another as shown in Table 1 and Figure 4 (in mms).

Material Model.
e material is modeled in ANSYS [12] as a linear isotropic material in the elastic range with elastic modulus 205 kN/mm 2 and Poisson's ratio 0.3.In the inelastic range, the material is defined to be bilinear isotropic with nominal yield stress from coupon tests according to Al-Karat and Rogers [4], as shown in Table 2.

Specimens FE Results
Discussion.In all the case studies, the reason of failure is the yielding of the brace material which is similar to the tests.e chord stud that is under compression has a buckling deformation that results in the decrease of the wall strength gradually which leads to excessive strains and failure.e existence of the stiffening parts in the top and bottom tracks is very important to exclude the possibility of having local failure.It is clear that the intermediate studs do not participate in the lateral shear wall strength; however, they have another important role to work as lateral support points at the point of connection with the bottom and top tracks.Besides that the gusset plates connect the braces straps to the shear wall, it also gives the connection between the chord studs and the tracks some rigidity.
Figure 5 indicates the main parameters that were investigated in verification case studies.V u and V y define the ultimate strength and the maximum elastic strength, respectively.∆ u and ∆ y define the ultimate displacement and the maximum elastic displacement, respectively.K p and K e define the wall plastic stiffness and the wall elastic stiffness, respectively.All previous parameters resulting from FE simulation model were compared with similar parameters from experiment.
e FE shows very accurate results compared with experimental results.Table 3 shows the FE results and the comparison with the experimental results.According to Table 3, e FE model can predict the wall strength with an average accuracy error of 4% and the wall lateral displacement with an average accuracy error of 10%.
ese results ensure that the developed FE model is reliable to simulate the inelastic behavior of the CFS shear walls and to be used in the parametric study.Figures 6-8 show the shear wall results and the load-deflection curves of different specimens.It is clear that all test specimens failed due to strap brace yield which indicates that all specimen components other than the braces were already overdesigned to guarantee that the strap brace achieve a plastic behavior.e FE was modeled to ensure that the failure will occur at the braces which are similar to what occurred at the test.

Description of Landolfo's Case Studies
ree typical wall configurations were defined according to both elastic and dissipative design criteria for three different seismic scenarios.e lateral in-plane inelastic behavior of these systems was evaluated by twelve tests performed on fullscale Cold-formed strap-braced stud wall specimens with dimensions 2400 × 2700 m subjected to monotonic loading.In our verification study, monotonic loading only is studied  Advances in Civil Engineering for the three wall configurations which are defined as follows: elastic light (WLE), dissipative light (WLD), and dissipative heavy (WHD) walls.e dimensions of the three walls are listed in Table 4. Wall configuration is shown in Figure 9. e lateral response of these systems was investigated by testing each of the three selected configurations by monotonic loading on full-scale wall specimens in size of 2400 × 2700 mm.Figures 10-12 show the shear wall results and the load-deflection curves of different specimens.From tests results, walls specimens WHE and WHD failed due to strap brace yield which is similar to the FE mode behavior.Specimen WLE failed due to net section fracture at the screws which is not considered in the FE model.In WLE specimen, the elastic range only is considered in the comparison.Table 5 shows the verification results.

Material Model.
e material is modeled in ANSYS [12] as linear isotropic material in the elastic range with elastic modulus 205 kN/mm 2 and Poisson's ratio 0.3.In the inelastic range, the material is defined to be bilinear isotropic with nominal yield stress from coupon tests according to Landolfo et al. [11], as shown in Table 6.

Parametric Study for the Response Modification Factor
Different codes use certain factor to reduce seismic forces on structures because structures can dissipate the same energy from earthquake with lower loads but more displacements depending on the overall structural ductility.e American Society of Civil Engineers ASCE/SEI 7-10 Standard [18] agrees to an R factor of 3.25 to be considered in the design of ordinary concentrically braced CFS frames.
e R factor can be increased to 4 if the capacity design approach is considered according to AISI S213 [8].e value of 4 of the R factor is also used by the US Army Corps of Engineers TI 809-07 Technical Instructions [19] which are used in the design of CFS systems.It also recommends that a capacity design approach should be followed.
In the National Building Code of Canada NBCC [20], R is called the force reduction factor which is defined by two factors R d and R o .
e ductility factor R d represents the capability of the structure to dissipate the earthquake energy which is located in the range from 1.0 to 5.0.e overstrength factor R o indicates the reserve in the element capacity.It is located in the range from 1.0 to 1.7, and it defines the overstrength resulting from member size, the resistance factor considered in design, the material overstrength, the material strain hardening, and the unconsidered resistance that structure retains before a total failure occurs.
Generally, the response modification factor depends on two parameters which are overstrength and ductility.Overstrength is the additional unconsidered strength over the ultimate design strength that occurred in most structures.Material overstrength, strain hardening, and strength reduction factors are the main causes of the overstrength (Ω): where V u is the ultimate shear strength, V d is the design shear strength.Ductility of a structure, or its members, is the ability to go through large inelastic deformations without major decrease of the strength or the stiffness.For the seismic loads, the ductility of the structure is an extremely important property.Newmark and Hall [21] state the ductility factor to be equal to the ratio between the ultimate deformation and the deformation at the initial yielding.ey provided the following equations in order to define the ductility reduction factor (R µ ): where ∆ u is the ultimate lateral displacement and ∆ y is the maximum elastic lateral displacement.Knowing that the fundamental time periods for CFS framing buildings are located in the range between 0.1 and 0.5 s, the ductility factor R μ can be presented as R μ � 2μ−1.

Capacity Design Approach.
e capacity design approach is to design all the structural elements of the shear wall other than the strap brace using an amplified force.is amplified force is calculated by overestimating the strength capacity of the strap (system fuse) by two amplification factors R y and R t .Values of R y and R t are listed for the Specially Concentrically Braced Frames (SCBF) in the Seismic Provisions for Structural Steel Buildings in AISC [22] and AISI S213 [8].ese factors are used in calculating the expected strength of the strap as follows: After determination of T n and T u , all other components in the shear wall (connections, studs, track, anchors, and hold-downs) should be designed to sustain the overexpected loads of the brace.

e Parametric Study.
In order to study the response modification factor (R) for the CFS-braced shear walls, a parametric study is performed on 19 shear wall models using the previously verified FE model.ree main parameters are studied: (i) e strap brace cross sectional area (t � 1 to 4.5 mm) (ii) e material yielding stress (2.3 and 3.6 MPa) (iii) e wall aspect ratio (1 : 1 and 1 : 2) e main objective of this study is to investigate the Response Modification Factor R of different wall parameters and compare R with R y .R y factor defines the overestimating design value of all shear wall elements other than the brace by overestimating the brace strength.According to AISI [23], R y is taken 1.1 for material yielding stress 3.4 MPa or more while equalling 1.5 for material yielding stress 2.3 MPa.
Two wall models are studied with two different aspect ratios.e first wall model has dimensions of 2.44 m width and 2.44 m height.e studs of dimensions 152.4 × 41.3 × 12.7 × 1.5 mm, chord studs, are made of assembly of two studs back-to-back.
e strap braces plate has 70 mm width and varying thickness.e second wall model has dimensions of 1.2 m width and 2.44 m height.e material is modeled as bilinear material with two different yield stress values.e first value is 360 MPa for R y 1.1.e second value is 230 MPa for R y 1.5.Figure 13 shows the walls' FE model.e parametric study results are listed in Table 7. Figure 14 shows R versus R y factors for different wall aspect ratios and yield stresses.V u is the ultimate shear strength, V d is the design shear strength, ∆ u is the ultimate lateral displacement, ∆ y is the maximum elastic lateral displacement, Ω is the overstrength factor, and R µ is the ductility factor.R y is the factor that overestimates the capacity of the brace according to AISI [23].
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Results and Discussion
For each wall aspect ratio, yield stress, brace thickness, and R y factor, the Response Modi cation Factor R is evaluated using the FE model.An eigen buckling analysis is performed to estimate the buckling length factor of the chord studs. is eigen buckling is performed rst for hinged-hinged column with the same chord stud length.Another eigen buckling is performed to the chord stud in the wall assembly under compression.From the comparison of both eigen buckling loads, it is found that the buckling length factor K for the chord stud is 0.5. is factor means that the gusset plates and the top track and the wall assembly give the studs rigid connections at ends.
For the same wall elements and varying strap brace thickness, di erent strap strengths to other wall elements strength ratios are calculated.ese ratios de ne R y factor for the walls which results in di erent response modication factors R.
Results are listed in Table 7 and shown in Figure 10.It is clear that, for walls with aspect ratio 1 : 1 and yield stress 3.6 MPa, the R factor is 5 at R y 1.1 which is greater than the value of 4 mentioned in speci cations.For walls with yield stress 2.3 MPa, the R factor is 6.2 at R y 1.5.
On the other hand, walls with aspect ratio equal 1 : 2 and yield stress 3.6 MPa have R 5.5 at R y 1.1 which is greater than the value of 4 mentioned in American speci cations.For walls with yield stress 2.3 MPa, the R factor is 5.2 at R y 1.5 which is greater than the value of 4 mentioned in American speci cations.

Conclusions
Based on the previous veri cation and parametric study, the following conclusions are reached: (i) e (R) value considered by American speci cations ASCE [18] is conservative.(ii) Using weak brace with su cient ductility and on the other side having strong connections, chord studs, and reinforced track and applying the capacity design approach, the R factor can be increased to 4.5 or even 5 for walls with aspect ratio 1 : 1 and 1 : 2. (iii) e nite element method gives an accurate simulation for the strap-braced shear walls in both elastic and inelastic ranges.It considers di erent material and geometric nonlinearities and accurately simulates the real behavior of the hold-downs.

Table 5 :
Results summary.(kN) V y (kN) ∆ u (mm) ∆ y (mm) K e kN/mm K p kN/mm V u (kN) V y (kN) ∆ u (mm) ∆ y (mm) V u V y ∆ u ∆ y Specimen failed due to connection failure after reaching the yielding limit.Connection failure is excluded in the FE model. *