Thin-Walled Structures 51 (2012) 64–75 Contents lists available at SciVerse ScienceDirect Thin-Walled Structures journal homepage: www.elsevier.com/locate/tws An experimental investigation on the lateral behavior of knee-braced cold-formed steel shear walls Mehran Zeynalian, H.R. Ronagh n School of Civil Engineering, The University of Queensland, Brisbane, Australia a r t i c l e i n f o a b s t r a c t Article history: Received 20 January 2011 Received in revised form 16 November 2011 Accepted 16 November 2011 Available online 8 December 2011 Experimental investigations were conducted to evaluate the lateral seismic characteristics of lightweight knee-braced cold-formed steel structures. In all, four full-scale 2.4 2.4 m2 specimens with different configurations were tested under a standard cyclic loading regime. This paper focuses on the specimens’ maximum lateral load capacity and deformation behavior and provides a rational estimate of the seismic response modification factor, R, of knee-braced walls. The study also looks at the failure modes of the system and investigates the main factors contributing to the ductile response of CFS walls. That is in order to suggest improvements so that the shear steel walls respond plastically with a significant drift and without any risk of brittle failure, such as connection failure or stud buckling. A discussion on the calculated response factors in comparison to those suggested in the relevant codes of practice is also presented. & 2011 Elsevier Ltd. All rights reserved. Keywords: Cold-formed steel Light steel frames Knee-braces Lateral performance Response modification factor 1. Introduction The cold-formed steel (CFS) construction is poised to make a significant impact in the low rise residual housing industry due to its unique advantages such as being cost-effective, light-weight and easy to work with. Although light-weight cold-formed steel walls are not new and have been used as non-structural components for many years, their application as load-bearing main structural frames is relatively new. As a result, appropriate guidelines that address the seismic design of CFS structures have not yet been fully developed and the lateral design of these systems is not covered in detail in the standards of practice. Hence, more research work is required in order to clarify the many different aspects of the seismic performance of CFS shear walls, including rational estimation of the response modification factor, R, as well as the achievable ductility and strength. Steel framed structures currently in use in Australia, are normally braced using face mounted thin straps, cross braces that are of the same shape as studs, or compressed cement boards screwed to the face of the walls. While, these are found adequate in low seismic regions of Australia, an investigation into the earthquake resistance properties of CFS have led authors to examine alternative bracing types that may present a more favorable ductile response. Knee braces that are specially designed for this purpose are introduced in the paper and studied in a specially designed testing n Corresponding author. E-mail address: h.ronagh@uq.edu.au (H.R. Ronagh). 0263-8231/$ - see front matter & 2011 Elsevier Ltd. All rights reserved. doi:10.1016/j.tws.2011.11.008 rig. Of particular interest in this study are the effects of kneeelement length and the use of brackets on the lateral performance. Knee elements maintain a considerable reserve of post-local buckling strength prior to yielding. Therefore, it is expected that their presence would facilitate a more ductile response. The brackets also add to the redundancy of the system and as such increase the ductility of the system in a similar manner. 2. Past studies In recent years, there have been many experimental research studies on the performance of different cold formed lateral resistance systems mostly on strap-bracing system. However there has not been any study made on the seismic behavior of knee-braced cold-formed steel shear walls. Some of these studies are summarized and presented below. Fulop and Dubina [1] investigated three full scale 3.6 2.44 m2 X-braced screw connected specimens under cyclic lateral loading. The walls consisted of cold-formed steel frames and double-sided 110 1.5 mm2 straps. The screw connection configuration was selected to facilitate yielding along the straps. Double stud members were chosen as the chords to limit inelastic deformations and ultimate failure of the walls. U profiles were used for the track to chord connections instead of plates or angles, which provided more capacity and rigidity for the frames. Local buckling of the lower track was observed during loading with damage being concentrated in corner areas. Although plastic elongation of the strap occurred, the results of the experiments may not M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 necessarily reflect the true ductility of a braced wall because the unexpected failure of the corners failure had been limited only to the straps. They suggested the ideal configuration of the corners would be such that the uplift force is directly transmitted from the brace or corner stud to the anchoring bolt, without inducing bending in the bottom track. Failure to strengthen the corners can have a significant effect on the initial rigidity of the system and can be the cause of larger than expected in-plane shear deformations of the wall and premature failure of the braced frame. Tian et al. [2] conducted experimental and theoretical studies on the racking performances of CFS walls including frames with single and double X straps. A total of five full scale 2.45 1.25 m2 frames consisted of strap braces riveted to the steel framing were tested. Brace size was either 60 1.0 mm2 or 60 1.2 mm2, which was installed on both sides of the walls. They investigated the failure modes and the lateral performances of the walls including: shear strength and frame’ stiffness. They reported that frames with straps on both sides have the best racking performance. Compression failure of the chord stud members was observed in the double sided specimens. Subsequent analyses of the test frames using an elastic slope deflection method were also performed to predict the failure loads and the initial shear stiffness. They concluded that it is possible to accurately predict the shear loads that were measured during testing; however the in-plane shear deformations of the walls could not be precisely determined with their calculation method. Gad et al. [3] presented a detailed investigation into the contribution of plasterboard in the seismic performance of CFS X-strap bracing walls be means of a shaker table together with numerical modeling. Cyclic loading tests on a real-scale 3D single storey X-strap bracing structure using shaker table tests were employed to address the nonlinear element properties as well as to simulate the influence of boundary conditions. Also, a numerical finite element model was used to find the theoretical capacity of a four-walled structure, which was compared with the experimental capacity of the same structure. The authors focused on comparing the theoretical and the experimental results and provided recommendations for improving the finite element model. By implementing the FE model, it was found that contributions to shear capacity from plasterboard and strap bracing are directly additive. However, considering the different inherent ductilities of strap braces and gypsum board panels (which reach their ultimate capacity at different displacements), it would seem that adding the shear capacity of plasterboard and strap bracing is irrational, as the Standard for cold-formed steel framing—lateral design [4] clearly illustrates. Serrette and Ogunfunmi [5] investigated the lateral performance of 2.44 2.44 m2 strap braced frames subjected to lateral monotonic loading. They tested three specimens with 50.8 0.88 mm2 screwconnected straps on one face, in addition to four specimens with strap braces on one face and gypsum sheathing board on the other side. It is also seen that one specimen with braces on both sides of the wall was investigated. In all cases, they used an 11 mm thick steel clip angle to the chord studs to act as a hold-down device. In addition, they implemented cold-formed steel gusset plates to connect the strap braces to the stud-track corner locations. They reported that one side strap bracing walls failed by extensive out-ofplane deformation, which is not a favorable scenario in terms of maintaining lateral stability of the braced frames, nor presents a ductile performance under inelastic shear deformations. They reported that gypsum panels provide a substantial increase in shear capacity compared with the 50.8 mm wide straps though the use of gypsum panels and strap braces together is not practical. It was also noted that in the design of X-braced walls, the engineers have to pay adequate attention to strap yield strengths in excess of the minimum specified value, which may result in connection or chord stud failure. 65 Kim et al. [6] performed a shaker table test on a full-scale twostory one-bay CFS shear panel structure. Each story consisted of two identical shear walls of 2.8 m length and 3.0 m height separated from each other by 3.9 m center to center. The two chords were constructed from three C-sections forming a two-cell closed section, and columns were welded to steel anchors and bolted to the slab through top and bottom tracks. A heavy square RC slab of 4.4 4.4 m2 by 200 mm thickness along with additional mass were placed at the top of each floor level, which made the total mass at each floor level equal to 256 kN. As the second story frame was identical to the first story, the damage occurred mostly in the first story as expected. Connections and anchors to the base beam were designed for the maximum over-strength of straps, based on TI 809-07 [7] code; however, no pre-tensioning was applied to the tension-only straps in spite of explicit recommendation in the code. The system was completely symmetrical and the centers of mass and stiffness were located at the same point and parallel to shear walls of the structure, to preclude torsional and out-of-plane responses. The structure was then loaded to a normalized accelerogram, which possessed spectral response acceleration equal to the design response spectrum around the fundamental period of the test specimen. The test caused significant yielding in the form of severe nonlinear behavior in the first floor straps along their entire length and yielding of studs near the anchors. The studs did not develop full flexural strength due to local buckling and this impaired their potential contribution to the story shear resistance. The studs’ contribution further decreased (about 15%) due to anchor deformation, which created a gap between the track and the slab. The results showed that during the large amplitude tests, the X-strap bracing showed very ductile, but highly pinched, hysteretic behavior. The results of this study can be considered conservative because the effect of non-structural gypsum board cladding was not considered in the test. Al-Kharat and Rogers [8] studied the inelastic performance of 16 X-strap braced 2.4 2.4 m2 CFS wall studs experimentally. For this purpose, they tested three different types of X-strap bracing, which were welded to the double stud chord sections under a cyclic loading regime. The main factor that was monitored and changed from one type to other was the cross-sectional area. Hence, they divided the specimens into light, medium and heavy strap-braced frame walls. By increasing the lateral drift, the shear resistance reduced, due to local failure at the hold-down location. While the main failure mode in the ‘heavy’ group was hold-down failure, other types of failure (like strap tearing, track buckling and track-to-chord connection failure) occurred in the ‘medium’ group of braced walls. The authors mentioned that these undesirable failure modes could have been avoided by proper design, as they would not allow straps to reach yield. Moreover, they concluded that the ductile performance of CFS walls, which is reflected in some codes with an R factor of 4, is not reliable and, for the medium and heavy walls, one should consider R¼3. This is similar to the provisions of ASCE7-05[9], which provides an R¼3 when adequate seismic research evidence is not available for the design. Moghimi and Ronagh [10,11] investigated nine full-scale CFS walls with four different strap-bracing systems under cyclic loading, in addition to gypsum board sheathed CFS frames. They tried to achieve failure of the frames by yielding of the straps, since this is a desirable ductile failure mode for CFS strap frames. They reported that gypsum board cladding alone is not reliable, especially when compressive vertical loads are present. Moreover, they used brackets at the four corners of the frames where the chords were connected to tracks and showed that this improved the walls’ lateral performance characteristics, such as strength, stiffness and ductility, when either single or double studs were 66 M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 used as the chords. They noted that, although using gusset plates provided ample room for straps to be connected to the panels and eliminated the possibility of failure in the strap-to-frame connection, this was not a practical method due to the potential esthetic problems it may cause, such as the unevenness of the covering plasterboard. 3. Code provisions One of the pioneer centers working on CFS framing systems is the American Iron and Steel Institute, AISI. The institute’s efforts in the development of construction standards started in the 1930s and culminated in the first publication of the AISI Specification in 1946 [12]. AISI has published several standards, including the following: Standard for Cold-Formed Steel Framing – Prescriptive Method for One and Two Family Dwellings [13]; North American Specification for the Design of Cold-Formed Steel Structural Members [14]; and a series of standards for cold-formed steel framing – General Provisions [15], Header Design [16], Lateral Design [4], Wall Stud Design [17] and Truss Design [18]. Although the design and construction of cold-formed steel structures shall comply with the North American Specification [14] and the General Provisions [15], seismic design regulations have been stipulated in the Lateral Design [7] along with some design guidelines for various special shear wall types and strap bracing [19–21]. The Lateral Design Standard does not enforce any special rule other than specifications and general provisions for shear walls when the response modification factor is considered as being smaller than 3 in design. However, for a response modification factor greater than 3, some additional requirements shall apply, mainly described for diagonal strap bracing members and anchorage of braced wall segments that resist uplift as well as perimeter members at opening. The alternative between R r3, with no special requirements, or taking the advantages of R43 in addition to some essential detailing, is permitted only for the seismic design categories A–C. In the seismic design categories D–F, using an R equal to or less than 3 is not permitted, and the designer must use the special seismic requirements with R greater than 3 to ensure that the system behaves properly in high seismic regions. Eventually, the code introduces seismic response modification factors for different basic seismic forceresisting systems; however, it does not cover all available lateral bracing systems, which are currently used in the CFS residential industry including the knee-bracing system. National Earthquake Hazard Reduction Program, NEHRP, is another American centers, which has published a few seismic provisions considering CFS contexts such as FEMA 450 [22] and FEMA P750 [23]. They specify that the design of cold-formed carbon or low-alloy steel members to resist seismic loads shall be in accordance with the requirements of AISI Specifications and AISI General Provisions. However, the allowable stress and load levels in AISI are incompatible with the force levels calculated in accordance with FEMA provisions. Therefore, it is essential to adjust the provisions of AISI for use with the FEMA provisions. It is mentionable that these modifications affect only designs involving seismic loads. The provisions affirm that all boundary members shall be designed to transmit the specified induced axial forces. In addition, connections for diagonal bracing members shall have design strength equal to or greater than the nominal tensile strength of the members being connected, or O\ times the design seismic force, in which O\ is the over-strength factor defined by the code. The pull-out resistance of screws also shall not be used to resist seismic forces. FEMA 450 gives the nominal shear strength for shear walls framed with cold-formed steel members based on different sheathing materials and fastener spacings at panel edges. Although the code provides the seismic response modification factors for some CFS framing systems, it does not cover all of the many different systems currently used in practice. As a consequence, for systems not mentioned in the code, the designer has to use the R factor corresponding to ‘‘Steel Systems Not Specifically Detailed for Seismic Resistance’’, which is 3. Another US standard on the cold formed steel structures is the Technical Instructions, TI 809-07 [7]. This code was originally developed for the design and construction of cold-formed steel military constructions and is used extensively by the US Army Corps of Engineers, USACE. The code is primarily based on FEMA 302 [24] though with some modifications in the design load considering over-strength of straps. TI 809-07 stipulates that shear panels shall be adequately anchored at their top and bottom to a floor diaphragm. Furthermore, when it comes to the tying of two lateral load resisting systems together, walls in orthogonal direction shall be anchored to the same floor diaphragm. The chords that support the vertical component of the strap load shall be selected from a single closed (tubing) section or built-up CFS section oriented to form a closed cross-section by means of intermittent welds. Although the code provides some general recommendations for seismic design of cold-formed steel shear walls, it mainly focuses on diagonal strap configurations. So, a seismic response modification factor is suggested only for CFS shear panels with diagonal strapping, which is 4. The code mentions that the R factor in the direction under consideration at any storey shall not exceed the lowest value for the seismic force resisting system in the same direction considered above that storey, excluding penthouses. Other structural systems, i.e. dual systems, may be used in combination with these CFS panels, but then the smallest R value for all systems in the direction under consideration must be used for determining the loads applied to the entire structure in that direction. Dual systems must be used with caution, particularly if differences in stiffness result in interaction effects or deformation compatibility problems. A different structural system may be used in the orthogonal direction with different R values, and the lowest R value of that direction shall be used in determining loads in that orthogonal direction. Uniform Building Code, UBC 97 [25], and International Building Code, IBC [26], highlight that the design, installation and construction of CFS structural and non-structural framing shall be in accordance with AISI. Also, the R factor shall be based on ASCE 7 for the appropriate steel systems, which are designed and detailed in accordance with the provisions of AISC. Although UBC allows a maximum height of five storeys for steel stud wall systems in seismic zones, provided that they comply with some specifications, IBC limits the use of CFS systems to up to two storeys in height considering AISI provisions. The codes restrict the thickness of CFS components to be in between 0.84 mm and 1.10 mm. According to IBC, a minimum of two studs back-to-back for the chord member is needed and the aspect ratio of the wall system shall not exceed 2:1. However, for some special applications, a maximum aspect ratio of 4:1 is acceptable. Moreover, studs shall be a minimum 41 mm (flange) 89 mm (web) with a 9.5 mm return lip, while minimum dimensions for tracks are 32 mm and 89 mm for flange and web, respectively. The code stipulates that bending in the track, overall buckling in stud and pull-out of strap connection shall be prevented. Moreover, the connection of diagonal bracing member and boundary members shall be designed such that the full tensile strength of the member, or O\ times the prescribed seismic forces, is developed. The Australian cold-formed steel structures standard, AS/NZS 4600-05 [27], requires that when cold-formed steel members are used as the primary earthquake resisting element, the selected response modification factor shall not be greater than 2, unless specified otherwise. However, as Australia is located in a low M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 67 seismic zone, wind loads often dominate the design of low-rise cold-formed steel buildings and therefore such a low value for R factor does not affect designs. Little research attention has been paid to the evaluation of R factors in Australia for the same reason. A simple but important conclusion from the above review is that there is not a universal agreement on the value of response modification factor, R, and in particular, there is no reference in the codes for the R factor of systems braced with knee-braces. More studies are required to clarify this matter. 4. Seismic response modification factor The term, ‘‘seismic response modification factor’’ was first introduced by the Applied Technology Council, ATC, in the ATC3-06 report [28] published in 1978. Since that time, other codes and provisions have adopted similar factors to consider the same concepts, although with different names [29]. The concept of a response modification factor is based on the argument that welldesigned structural resistant systems have a ductile behavior and are able to carry large inelastic deformation without collapse. In other words, designed seismic strengths given by earthquakeresistant design codes are typically lower than the lateral strength that is required to keep a structure in the elastic range in the event of earthquakes. Strength reductions from the elastic strength demand to real inelastic structural strength are taken into account using the reduction factors, R. They were considered to relate the ratio of the forces that would be developed under the particular ground motions if the lateral framing systems were to be totally elastic, to the prescribed design forces at the strength level, which was commonly assumed to be equal to the significant yield level. So, the R factor is ‘‘ y an empirical response reduction factor intended to account for damping, over-strength, and the ductility inherent in the structural system at displacements great enough to surpass initial yield and approach the ultimate load– displacement of the structural system’’ [30]. Hence, it is anticipated that for a low ductility structure, which would not be able to tolerate any considerable drifts further than the elastic range, the R factor would be close to 1 and its behavior would be approximately linear. On the contrary, a highly ductile building with a ductile structural system would be able to endure deformations significantly better, and therefore is anticipated to have a larger response reduction factor. The response modification factor is commonly expressed in terms of its two main components: ductility reduction factor (Rd) and structural over-strength factor (O\) [30,31]. The R factor is defined as R ¼ Rd O0 ð1Þ The components of the response modification factor are defined using Fig. 1, which indicate the actual and the elastic performance of a structural system as well as the idealized bilinear force–displacement curve, as Rd ¼ Ve , Vy O0 ¼ Vy Vs ð2Þ and the R factor can then be regenerated as R ¼ Rd O0 ¼ Ve Vy Ve ¼ Vy Vs Vs ð3Þ where Ve, Vy and Vs correspond to the structure’s elastic response strength, the idealized yield strength and the first ‘‘significant yield’’ strength, respectively. Fig. 1. General structural response, illustrating FEMA’s concepts. The evaluation of R factor and its components is a controversial structural concept, which has been discussed for many years; however, some defined approaches are more popular than others. In fact, the way that different parameters and an idealized bilinear curve would be addressed has significant effects on the estimated R factors. In this research study, the proposed method by FEMA [22,30,32] is used to evaluate the response modification factor for knee-braced systems. Fig. 1 illustrates the general structural response considering both positive and negative post-yield slope, and the method, which has been used to idealize a force–displacement curve based on FEMA 356 [32]. The idealized bilinear curve is formed by two lines. The 68 M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 line segments shall be located using an iterative graphical method that balances the size of the areas above and below of the curve. The initial secant stiffness is calculated using a base shear force equal to 60% of the idealized yield strength of the structure. The second segment line and the post-yield slope shall be determined by a line passing through the actual curve at the calculated target displacement, which is addressed as Dt. In this study, based on references [31,33–36], it is assumed that the target displacement is the maximum structure’s drift prior to a considerable fall in the structure’s strength. The code stipulates that the effective yield strength shall not be taken to be greater than the maximum base shear force at any point along the actual curve. 4.1. Ductility reduction factor, Rd Rd has received considerable attention amongst researchers and depends on the structural properties such as ductility, damping and fundamental period of vibration, as well as characteristics of the earthquake ground motion. Newmark and Hall [37] developed the set of Eqs. (5)–(7) defining Rd in terms of a structure’s ductility, which is expressed in terms of maximum structural drift, Dmax, and the drift corresponding to the idealized yielding point, Dn, as Ductility : m ¼ Dmax Dy 4.2. Over-strength factor, O\ The over-strength factor is intended to address possible sources that may contribute to strength beyond its nominal value. Basically, over-strength results from the following structural characteristics: Structural redundancy, which is a representative of the struc ture’s capacity to redistribute internal forces. Higher material strength than those prescribed by the designs. Use of strength reduction factors and load factors in design. Strain hardening. Deflection constraints due to serviceability limit state. Use of oversized members. Use of multiple loading combinations. Non-structural elements effects. Strain rate effect. FEMA 450 [30] has categorized the over-strength factor into three main components including: the design over-strength, O\, the material over-strength, OM, and the system over-strength, OS; and suggested a typical range for each. ð4Þ 5. Objective and scope of research 8 m > < Rd ¼ p ffiffiffiffiffiffiffiffiffiffiffiffiffi ¼ 2m1 R Newmark and Hall : d > :R ¼1 d T 4 0:5 s 0:1 o T o 0:5s ð5Þ2ð7Þ T o 0:03 s The Newmark and Hall method has been widely adopted by other researchers, and the offered equations have been verified by different real seismic records. In studies by Nassar and Krawinkler [38] and Miranda and Bertero [39], it has been shown that Rd is dependent on the ground motion frequency as well as the ground’s soil type. One potential lateral resistant system for CFS structures is the knee-braced system, which uses elements similar to studs or noggins at an angle that runs in between the studs to form a knee-brace. The behavior of these systems is not completely understood as yet, because most previous studies have been conducted on the strap-bracing system and shear walls with panel sheathing, as can be seen in the literature and codes. The aim of the current research is to evaluate the lateral seismic performance of different configurations of knee-braced systems including an estimation of the seismic response modification factor for different CFS Fig. 2. Testing rig diagram and notation convention. M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 knee-braced configurations followed by a comparison with the recommended code values for the R factor. It is necessary to mention that the walls studied here are unlined, and the positive effect of gypsum board on the lateral performance of the frame under cyclic loading is ignored. This is due to the fact that post-earthquake observations of timber frame structures in the Northridge earthquake have shown that many gypsum board shear walls failed under imposed dynamic load [5]. Also, some design codes [40] have recommended neglecting the gypsum board’s contribution and relying only on the bare steel frames. 6. Test setup 6.1. Testing rig and instrumentation The general configuration of the testing rig is shown in Fig. 2. Each specimen was installed on the rig between the fixed support beam at the bottom and a rigid loading beam at the top, using four M16 high-strength bolts in the vicinity of the chords and the 69 middle of the tracks either side. The bolts were tightened by a torque wrench to a torque of about 190 N m, corresponding to about 53 kN tension in the bolt. A strong combination of washers and nuts was used to ensure that there was no possibility of slip between the tracks and the beams. Also, as shown in the figure, four hold-down angles were used at the four corners of the wall in order to reduce the possibility of overturning and to provide a proper load path from the braces to the wall chords and studs. An accurate Horizontal Drift (HD) transducer was used to evaluate the horizontal displacement of the top track. To evaluate the amount of uplift, four transducers were placed at the four corners of the walls between the frame and tracks. Also, one load-cell was used to measure the racking resistance. All data from the transducers and load-cell were analyzed and transferred to the computer using Lab View Signal Express software [41]. The load– displacement curve of each frame was then plotted. 6.2. Loading protocol The cyclic loading regime that has been used in this study is based on Method B of ASTM Standard [42], which was originally Specimen N1 Specimen N2 Specimen N3 Specimen N4 Fig. 3. General configuration of specimens N1–N4. 70 M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 developed for ISO (International Organization for Standardization) standard 16,670. This loading regime consists of one full cycle at 0.5, 1, 2, 3 and 4 mm, and three full cycles at 8, 16, 24, 32, 40, 48, 56, 64 and 72 mm, unless failure or a significant decrease in the load resistance occurs earlier. The mentioned lateral amplitudes are corresponding to 1.25%, 2.5%, 5%, 7.5%, 10%, 20%, 40%, 60%, 80%, 100%, 120%, 140%, 160% and 180% of the ultimate lateral displacement of the walls. It is worth noting that Method B of ASTM E2126-07 stipulates that the amplitude of cyclic displacements has to be selected based on fractions of monotonic ultimate displacement. If this was applied here, the loading regime would vary for different specimen types since each specimen had its own ultimate displacement. However, as set out earlier, one of the current research objectives has been a comparison between different types of knee-braced configurations of the shear walls, which would necessitate the use of identical cyclic amplitudes for different walls. Hence, Method B is used in this study with lateral amplitude independent of monotonic testing. Moreover, although 75 mm, or 3.125%, inter-storey drift ratio was the maximum amplitude of the actuator, it was considered adequate, since the maximum allowable storey drift ratio specified by the Standard FEMA 450 is 2.5% [22]. The average loading velocity was about 2 mm/s, which is compatible with the ASTM E2126-07 recommendation that the loading velocity must be in the range of 1–63 mm/s. Table 1 Mechanical properties of the C-section stud. Nominal grade Nominal thickness Elastic modulus Yield stress, Fy 550 MPa 0.55 mm 169 GPa 592 MPa Yield strain Ultimate stress, Fu Ultimate strain Fu/Fy 0.45% 617 MPa 2.86% 1.04 7. Experimental program The program consisted of testing four 2.4 2.4 m2 full-scale frames to investigate the hysteretic lateral performance of different configurations of knee-braced walls shown in Fig. 3. Specimens N1 and N3 included concurrent knee-braced system and brackets in the four interior corners of the wall. This was to investigate the effects of brackets on the frames performance. In order to reduce the number of geometric variants, the length of knee elements and brackets pffiffiffi were considered equal. The kneeelements length was 300 2 mm, which is equal to 13 times the half wave-length (HWL)pof ffiffiffi local buckling of the stud section in specimen N1, and 200 2 mm (eight times the local buckling HWL) in specimen N3. The diagonal elements were connected to the middle of elements exactly as shown in Fig. 3. These walls were tested in the Structural Laboratory of the School of Civil Engineering at the University of Queensland using a specially made testing rig illustrated previously. All of the frame elements, such as top and bottom tracks, noggins, studs and KNEE-elements were made by an identical C-section of dimensions 90 36 0.55 with a lip of 6.6 mm. The section structural material properties are shown in Table 1, and the detailed section geometry is shown in Fig. 4. All components were connected together at each flange using just one rivet with the shear strength capacity and tensile strength capacity of 3.3 kN and 3.8 kN, respectively. The effects of different components, such as different configurations or numbers of knee-elements, use of double studs, etc., were monitored and investigated in this research by changing them from one specimen to another. 8. Experimental results Based on the observations made during the tests, the common failure mode for all of the specimens was plastic local buckling in the knee-elements to studs connections (as shown in Fig. 5), which was followed by rivet pull-out for specimens N2 and N4. The rivet pull-out failure did not happen in specimens N1 and N3 due to the presence of brackets, which brings about more structural flexibility and higher energy dissipation through studs’ deformations, rather than rivet pull-out phenomenon. As depicted in Fig. 3, the first specimen, N1, consisted of a wall panel with four brackets in the interior corners. To prevent buckling in the side chords, double studs sections were used. Fig. 4. Detailed dimension of stud C 90 36 0.55 in mm. Fig. 5. Plastic local buckling in the knee-elements to studs connection. M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 2500 Shear Resistance (KN) Interestingly, the panel performance was perfect and no failure mode was observed up to the end of the test that was corresponding to maximum drift cycle of 74 mm, though some plastic local buckling occurred in the knee-elements’ connections at the central part of the frame, which was followed by plastic bending in the middle of the brackets. The hysteretic envelope curves and load–deflection Hysteretic Cycles for all Specimens are presented in Figs. 6–10. The envelope curves are derived from the load– deflection hysteretic cycles, which are obtained from racking tests using accurate transducers and Lab View software [41]. For specimen N2 (presented in Fig. 3), after the application of the lateral loads, early plastic local buckling occurred in the kneeelements connections; however the frame lost its capacity only after the rivet pull-out at the end of diagonal braces. This was 1500 500 -100 -50 -40 2500 500 1500 20 -1500 -2500 Lateral Displacement (mm) 40 60 N1 N3 80 N2 N4 Shear Resistance (KN) 2500 500 -500 0 -100 -50 -500 0 50 100 -1500 Fig. 10. Load–deflection hysteretic cycles for specimen N4. 1500 -50 500 -2500 Lateral Displacement (mm) Fig. 6. Hysteretic envelope curve for all specimens. -100 100 Fig. 9. Load–deflection hysteretic cycles for specimen N3. 1500 -20 -500 0 50 -2500 Lateral Displacement (mm) Shear Resistance (KN) Shear Resistance (KN) -60 -500 0 -1500 2500 -80 71 50 100 -1500 -2500 Lateral Displacement (mm) considered as the main failure mode of the frame and was corresponding to the third cycle of 56 mm drift in the upward cyclic loading. Next specimen was N3 (shown in Fig. 3). It was similar to specimen N1 with a smaller length for knee-elements and brackets. Again for specimen N3, no specific failure mode was observed up to the end of the test. The only phenomenon was plastic local buckling in the knee-elements’ connections followed by plastic bending in the brackets. The major failure mode for the last shear wall, N4, was a plastic global buckling in the longer Knee elements, which followed by the rivet pull-out corresponding to the second cycle of 48 mm drift. Fig. 7. Load–deflection hysteretic cycles for specimen N1. 9. Evaluation of R factor Shear Resistance (KN) 2500 1500 500 -100 -50 -500 0 50 -1500 -2500 Lateral Displacement (mm) Fig. 8. Deflection hysteretic cycles for specimen N2. 100 The specimens’ hysteretic envelope curves are used to determine the response modification factors by following these steps: Firstly, the idealized bilinear curve is evaluated using the method presented in FEMA 356 [32]. The idealized curves of Specimens N1–N4 in the positive side of the envelope curves are depicted in Figs. 11–14. Secondly, the ductility reduction factor, Rd, is evaluated via the first part of Eq. (2). The equation requires both Vs and Vn, which can be estimated based on Fig. 1. Vs is calculated based on the concept of equal energy and Vn is evaluated using the idealized bilinear curve, which is explained in detail in part 4 of this paper. A comparison between the ductility reduction factors obtained this way and those calculated based on Newmark and Hall’s formulations is presented in Table 2 where a good agreement is evident between the two methods. For the calculation of Rd based on Newmark’s method, the ductility factor, m, is 72 M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 Shear Resistance (N) 2500 Table 2 Ductility reduction factors, Rd. 2000 1500 1000 0 20 40 60 Lateral Displacement (mm) 80 2500 Shear Resistance (N) N2 N3 N4 la rb Graph (Ve/Vy) Newmark’s method Eq. (6) Differences (%) 1.88 1.88 0 1.83 1.90 3.7 1.98 1.97 0.5 1.66 1.67 0.6 1.84 1.86 1.1 0.132 0.130 – b Fig. 11. Idealized bilinear curve for specimen N1. 2000 1500 1000 500 0 0 20 40 60 80 Lateral Displacement (mm) Fig. 12. Idealized bilinear curve for specimen N2. 2500 Shear Resistance (N) N1 a 500 0 2000 1500 1000 500 0 0 20 40 60 Lateral Displacement (mm) 80 2500 2000 1500 1000 500 0 0 20 40 60 Lateral Displacement (mm) Fig. 14. Idealized bilinear curve for specimen N4. m: average. s: standard deviation. calculated using Eq. (4), which requires the idealized bilinear curve to be drawn first in order to determine Dmax and Dy. Here Eq. (6) can be used, as the fundamental period of CFS structures is usually assessed to lie in between 0.1 and 0.5 s [3]. The third step is to establish the over-strength factor, O\, using the second part of Eq. (2), employing Vy and Vs. The authors here have made use of reverse calculations in order to find out the design capacity of the tested frames looking at the mechanism with the smallest failure load, which happens in this case to be the rivet pull-out as observed in the tests. According to the design formulas of AS4600, the design pull-out capacity of the rivets used in this experiment is 705 N. This value is basically the ultimate pull-out resistance of one rivet reduced by a capacity reduction factor of 0.5 as advised in AS4600. Kneebraces are connected to studs using two rivets on the side flanges and therefore the capacity of every knee-bracing element under pull-out failure mechanism is taken to be 1410 N. In order to relate this capacity to the lateral load applied to the frame, a model is generated in SAP2000 [43] using normal frame elements capable of flexure and axial tension or compression. To illustrate this, the model of specimen N2 is shown in Fig. 15 and its lateral defection in Fig. 16. Using the model, the lateral load at which the first element reaches its pull-out capacity is derived and recorded as VS. Having this information, the values of O\ and R factors are then calculated. These are listed in Table 3 for all specimens. The R factors presented in Table 3 indicate that the response modification factors for knee-braced systems would range between 2.80 and 3.61; with the average being 3.18. These values show that the prescribed value of 3 for the R factor of CFS frames as advised in some design codes (such as AISI and FEMA) is reasonable while the suggested R factor of 2 in the Australian standard (AS4600), is too conservative (Figs. 17–19). 10. Conclusion and recommendation Scrutinizing the obtained outcomes and comparing the results to other experiments performed both by the authors and by other researchers, it is concluded that although knee-braced cold formed frames have relatively high maximum drifts, Dmax, their strengths are not as high as strap bracing systems. Hence, the use of a knee-stud bracing system is possible only in low seismic regions where the earthquake loads, and thus the required lateral resistance capacity, are not high. According to current research results and by comparing the associated envelope curves in Figs. 6–10, the following conclusions can be made: Fig. 13. Idealized bilinear curve for specimen N3. Shear Resistance (N) Specimen’s name 80 1. Having a larger enclosed area in the hysteretic curves of kneebraced frames represents a more favorable lateral response for these frames as frames with larger enclosed curves dissipate more energy. 2. Using brackets at four interior corners of a knee-braced wall panel improves the lateral performance of the panel considerably, including both the shear strength and the panel M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 73 Fig. 15. SAP2000 model of K4, 3D view. Fig. 16. Lateral deflection of K4. Table 3 The evaluated response modification factors based on FEMA provisions. No. Specimens Dy (mm) Dmax (mm) O0 Rd R 1 2 3 4 N1 N2 N3 N4 33.0 24.4 30.2 24.4 74.8 56.5 74.0 46.4 1.62 1.78 1.83 1.68 1.88 1.83 1.98 1.66 3.05 3.26 3.61 2.80 1.73 0.095 1.84 0.132 3.18 0.346 Average Standard deviation ductility. Besides supporting the chords and the tracks against buckling by reducing the buckling length of the members, one great advantage of using brackets is to use the plastic bending capacity of the brackets as an additional energy dissipating mechanism in the frame. It is necessary to mention that using double stud sections for the chord members is essential to improve the lateral performance of the walls when brackets are incorporated as it increases the chord buckling capacity. 3. It is noted that the frame performance depend on the accuracy of the manufacturing of LSF elements. Existing gap 74 M. Zeynalian, H.R. Ronagh / Thin-Walled Structures 51 (2012) 64–75 2.2 2.1 2.0 5. 1.9 1.8 N1 N2 N3 N4 6. Fig. 17. Maximum strength of the specimens (KN). 4.0 3.0 7. 2.0 8. 1.0 9. 0.0 N1 N2 N3 N4 Fig. 18. Maximum lateral drift ratio (%). 6.0 R factors Average R 5.0 4.0 3.0 specific failure modes were observed during the tests and the ultimate drifts were approximately similar, the maximum shear load for specimen N3, which had shorter knee-elements was higher than that of N1. As is evident in Fig. 6, the area, which is enclosed by the Equivalent Energy Elastic Plastic (EEEP) curve and the capacity of energy dissipation for specimen N3 is higher than other specimens. Comparing the envelop curves of specimens N2 and N4, it is seen that a shorter knee-element leads to a greater shear strength for the wall but at the expense of a lower ductility. That is because larger knee-elements provide more post-local buckling reserve, which allows the walls to deform further under the lateral loads. Investigating the test results and the final failure modes for different specimens, a suggestion would arise with regard to preventing the brittle failure of the walls (with no bracket) associated with rivet pull-out, and this is to use appropriate washers under the rivets or use a rivet with a wider head. This suggestion has been implemented in the current study and confirmed by the favorable results [44]. Considering the evaluated R factors, while the prescribed value of R ¼3 for a knee-braced system in AISI is reasonable, the R¼2 suggested by AS4600 seems to be too conservative. A combination of different structural characteristics and dissipating energy mechanisms affect the R factor. While the strength and maximum drift of one specimen can be higher than the other, the R factor could be lower. Considering the aforementioned results and comparing those with the results of strap bracing performed by Moghimi and Ronagh [11], it is concluded that the performance of kneebracing systems under cyclic loads is not satisfactory. That is because, even after preventing some undesirable failure modes like rivet pull-out and shear failure mode in the rivets, there still remains the buckling failure mode in the knee-elements, which is an undesirable failure. Based on the graphs shown in Figs. 7–10, which show that there is neither adequate ductility nor a measurable energy dissipating mechanism for the knee-braced system, it is concluded that knee-bracing is not a preferable lateral resistant system, especially in medium to high seismic regions. 2.0 1.0 References 0.0 N1 N2 N3 N4 Fig. 19. R factor. (the lack of continuity of the web element) in the kneeelements to stud elements connections causes the early plastic local buckling in the connections that finally leads to undesirable failure modes such as tearing in the connections; and as such the real capacity of frame cannot be utilized. Also, as the bending capacity of studs is low, it is essential to connect different knee-elements at the same point or as close to each other as possible to prevent any lever arm and bending moment development in the studs. 4. The performance of the Knee Brace lateral resistant system would be improved pffiffiffi by decreasing the length of knee-elements from 300 2 mm (13 times the half pffiffiffi wave-length of local buckling of the stud section) to 200 2 mm (eight times the local buckling half wave-length). In another word, although the lateral performances of both specimens N1 and N3, which include the brackets were acceptable and no [1] Fulop LA, Dubina D. 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