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## Latin American Journal of Solids and Structures

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*On-line version* ISSN 1679-7825

### Lat. Am. j. solids struct. (Online) vol.8 no.2 Rio de Janeiro June 2011

#### https://doi.org/10.1590/S1679-78252011000200004

**Analysis of the steel braced frames equipped with ADAS devices under the far field records**

**Mahmoud Bayat ^{*}^{,I}; G.R. Abdollahzade^{II}**

^{I}Department of Civil Engineering, Shirvan Branch, Islamic Azad University, Shirvan, Iran

^{II}Department of Civil Engineering, Babol University, Babol, Iran

**ABSTRACT**

The usefulness of supplementary energy dissipation devices is now quite well-known in earthquake structural engineering for reducing the earthquake-induced response of structural systems. The seismic behavior of structures with supplemental ADAS devices is concerned in this study. In this paper, the ratio of the hysteretic energy to input energy is compared in different structural systems. The main purpose of this paper is to evaluate the behavior of structures equipped with yielding dampers (ADAS), located in far fields based on energy concepts. In order to optimize their seismic behavior, the codes and solutions are also presented. Three cases including five, ten and fifteen–story three-bay Concentric Braced Frames (CBF) with and without ADAS were selected. The PERFORM 3D.V4 software along with three earthquake records (Northridge, Imperial Valley and Tabas) is used for nonlinear time history analysis and the conclusions are drawn upon energy criterion. The effect of PGA variation and height of the frames are also considered in the study. Finally, to increase the energy damping ability and reduce the destructive effects in structures on an earthquake event, so that a great amount of induced energy is damped and destruction of the structure is prevented as much as possible by using ADAS dampers.

**Keywords:** yielding dampers (ADAS); steel braced frame, energy dissipation devices.

**1 INTRODUCTION**

Development and subsequent implementation of modern protective systems, including those involving passive energy dissipations, has changed the entire structural engineering discipline significantly. Various energy dissipation devices such as devices which modify rigidity, masses, dampers or forms which absorb energy in ductile structures are used to control the structural vibrations induced by earthquakes or wind excitations. In general, structural control devices can be divided into three categories; passive control, active control and semi-active control [20]. An active control device is known as a system which typically requires a large power source for operation of actuators which apply control forces to the structure. A semi-active control system is similar to active control systems but the external energy requirements are orders of magnitude smaller than typical active control systems [6, 19, 20]. A passive control system is defined as a system which does not require an external power source for operation. Practically, efficient application of energy dissipating devices in earthquake engineering has two important aspects; the device should have a stable and sufficiently large energy dissipation capacity and also it's cyclic behavior should be known with a representative model. A number of novel approaches have been developed to redress the static procedure of conventional seismic design. Adding energy absorbers to a structure is one of these approaches. The goal of the application of energy absorbers in a structure is to concentrate hysteretic behavior in specially designed and detailed regions of the structure and to avoid inelastic behavior in main gravity load- resisting structural elements. Kelly [9] developed and extensively tested the devices which their function were based on the plastic deformation of mild steel. Friction devices of several types have been the subject of a number of research programs, and now they have been utilized in several real buildings. The Pall-type friction damper has been used in three buildings in Canada; two new buildings and the retrofitting of a school building damaged in the 1989 Saugenay earthquake [13-15]. By the middle of 1991, Sumitomo-type friction dampers had been incorporated in two 31- and 22-story buildings, both in Japan. Lead extrusion dampers were used in a recently completed 17-story building, and also in an 8-story building, both in Japan.

The first U.S. application of ADAS elements for seismic retrofitting of a building was completed in San Francisco in early 1992 [3]. Viscoelastic dampers have been used in several tall buildings for wind vibration control. The dampers contain a highly dissipative polymeric material which has well-defined material properties and behavioral characteristics [10]. The most notable applications are the twin 110-story towers of the World Trade Center in New York City, where dampers had been installed for 20 years [11]. Several other high-rise buildings in the U.S. also are equipped with viscoelastic dampers for wind vibration control [8]. In Tokyo, a 24-story building was recently completed with bituminous-rubber viscoelastic dampers, providing the structure with increased damping to resist earthquake loadings [26]. One of the effective mechanisms available for the dissipation of energy input to a structure caused by earthquake is through inelastic deformation of metals. Many of these devices use mild steel plates with triangular or *X* shapes so that yielding is spread almost uniformly throughout the material. These devices exhibit stable hysteretic behavior; they are insensitive to thermal effects, and extremely reliable. A typical *X*-shaped plate damper or ADAS (added damping and stiffness) device is shown in Fig. 1. Other configurations of steel yielding devices, used mostly in Japan, include bending type of honeycomb and slit dampers and shear panel type. Implementation of metallic devices in full-scale structures has taken place after their performance had been characterized through experimental researches. The earliest applications of metallic dampers in structural systems occurred in New Zealand and Japan. Some of these interesting applications are reported in [5, 18]. More recent applications include the use of ADAS dampers in the seismic upgrade of existing buildings in Mexico [12] and in the USA [16]. The seismic upgrade project discussed in [16] involves the retrofit of a Wells Fargo Bank building in San Francisco, CA. The building is a two-story nonductile concrete frame structure originally constructed in 1967 and subsequently damaged in the 1989 Loma Prieta earthquake. A total of seven ADAS devices were employed, each with a yield force of 150 kips. Both linear and nonlinear analysis were used in the retrofit design process. Further, three dimensional response spectrum analysis, using an approximate equivalent linear representation for the ADAS elements, furnished a basis for the redesign effort. The final design was verified with DRAIN-2D nonlinear time history analyses. The role of a passive energy dissipator is to increase the hysteretic damping in the structure.

This study mainly focuses on the effects of application of ADAS devices – discussing the basic concepts of energy. To show the effects and performance of ADAS devices when severe earthquakes occur, three cases consist of five, ten and fifteen-story 3-bay Concentric Braced Frames equipped with and without ADAS devices have been considered. The assumed detail and arrangement of typical ADAS devices are shown in Figure 1.

**2 BASIC CONCEPTS OF INPUT ENERGY TO A STRUCTURE**

By considering a viscous damped SDOF system subject to horizontal earthquake ground motion (Figure 2), the equation of motion can be written as:

Where *m* = mass, *c* = viscous damped coefficient, *ƒ*_{s} = restoring force, *ü _{t}* =

*ü*+

*ü*= absolute (total) displacement of mass ,

_{g}*u*= relative displacement of the mass with respect to the ground,

*u*= earthquake ground displacement.

_{g} By letting *ü _{t}* =

*ü*+

*ü*, Equation (1) may be written as

_{g}Therefore the structural system in Figure 2a can be conveniently treated as the equivalent system in Figure 2b with a fixed base and subject to an effective horizontal dynamic force of magnitude -*mü _{g}* . Although both systems give the same relative displacement, this "convenience" does cause some confusion in the definition of input energy so there are two methods for evaluation of input energy of structures. The first one is "Absolute energy method" and the second one is "Relative energy method" [22].

**2.1 Derivation of "absolute" energy equation**

Integrate Eq. (1) with respect to u from the time that the ground motion excitation starts:

For the first term of the above equation, we have;

Then the Eq. (3) can be written as follow;

The first and second term of the Eq. (5) is the "absolute" kinetic energy;

The second term of the Eq. (5) is the "absolute" damping energy

The third term in Eq. (5) is the absorbed energy (*E _{A}*), which is composed of recoverable elastic strain energy and irrecoverable hysteretic energy:

The right-hand side term in Eq. (5) is, by definition, the absolute input energy (*E _{I}*).

The absolute energy method can be applied to structures with base excitation underground acceleration and it physically represents the work done by the total base shear at foundation level relative to foundation displacement [22].

**2.2 Derivation of "relative" energy equation**

Integrate Eq. (1) with respect to *u*:

The first term in Eq. (10) is "relative" kinetic energy;

The second term of the Eq. (10) is the "relative" damping energy

The third term in Eq. (10) is the absorbed energy (*E _{A}*), which is composed of recoverable elastic strain energy and irrecoverable hysteretic energy:

The right-hand side term in Eq. (8) is, by definition, the absolute input energy ().

And

The relative energy method is applied to structures with fixed-bases that sustain a horizontal dynamic force (-*mü _{g}*) and it physically represents the work done by the static equivalent lateral force (-

*mü*) on the relative displacement that it neglects the effects of rigid body movement of the structure [22].

_{g}The "absolute" input energy and "relative" input energy are close to zero for structures with very long and short fundamental periods respectively [22] and they are very similar for periods between 0.2s to 5s [1]. Akiyama and Bertero [22] have shown that the evaluation of "absolute" and "relative" input energy to a SDOF system can be a very good estimate of the input energy to multi-story buildings since the input energy to SDOF and MDOF systems with the same period is almost equal [1].

In this paper, the "relative" energy method is adopted for evaluation of input energy of structures and the total input energy of structures are compared at the time when the earthquake is over and the motion of structure is damped.

The application of Eq. (15) in the design process has been developed by a number of researchers [4, 7, 21, 24]. The goal is to increase *E _{H}* so that, for a fixed , the elastic strain energy in the structure becomes minimized. It means that the structure will undergo smaller deformations for a certain level of input energy in comparison with the case that does not include energy dissipators. Consequently, increasing

*E*permits

_{H}*E*to be reduced for a higher level of .

_{S}

**3 OVERVIEW OF DESIGNING ADAS **

**3.1 Characteristics of ADAS devices**

Tasi *et al* [21] illustrates that the ADAS devices exhibit nonlinear behavior under noticeable ground motions.We can simulate the seismic behavior of ADAS devices with a bilinear behavior between shear force and relative displacement is concluded (Figure 3). Thus, the ADAS devices bearable forces are given as;

*a* = an unknown coefficient to be determined from the experimental data

*K'* = elastic stiffness of the ADAS devices

*δ** _{R}* = maximum relative displacement

*δ** _{y}* = yield displacement of the ADAS devices

The ADAS devices by possessing the stable hysteretic loops resulting from the yielding of steel plates provide reliable energy dissipation.

The ductility ratio *µ* is defined as;

Let *N* represent the number of steel plates and *K* represent the stiffness of a steel plate. Where *K'* = *NK*. Substituting Eq. (16) into Eq. (17) leads to

The stiffness of a steel plate, *K* can be determined in accordance with the geometric shape of the steel plates; for example,

And

*E* = elastic modulus of steel

*B* = base width

*T* = thickness

*H* = height of the steel plates

**3.2 Seismic forces and the effects of ADAS device design**

The bracing members are considered rigid in stiffness during design of a structure with damping devices. The reactive forces due to seismic impact on the building mainly include column shear forces and ADAS-absorbed forces (*F _{C}* and

*F*in Fig. 4). The ADAS devices are designed to be able to absorb impact to keep the column shear forces less than the designed column shear forces at any time. Generally, ADAS devices are designed after the Concentric Braced Frames has been designed to meet the seismic building requirements. Let

_{R}*F*be the maximum story shear forces of structures without ADAS devices on each story during earthquakes,

_{T}*F*be the designed column shear forces and

_{D}*F*represent the resistant forces of ADAS dampers that are aimed to be designed. If

_{R}*F*>

_{T}*F*, the goal of using the dampers is to absorb

_{D}*F*–

_{T}*F*so that

_{D}*F*will not exceed

_{C}*F*during the earthquake. The above implies

_{C}

Further, in Eq.(18), we use the designed ductility ratio *µ*_{d} instead of the resulting ductility ratio *µ* when *N* plates are used. Eqs. (18) and (21) lead to Eq. (22) to the number of steel plates for the ADAS devices to achieve the above goal:

**4 STUDY ON THE EFFECTS OF THE ENERGY DISSIPATING SYSTEMS**

In order to show the effectiveness of the damper, the same structures without any dampers have been analyzed too. The frames were designed prior to this study in accordance with Uniform Building Code 97 requirements, based upon the static analysis using following criterias.

1. Soil type is assumed Sc (very dense soil and soft rock) according to UBC97 [23] code.

2. Earthquake source and structures distance from active fault is 10 km according to type A of UBC97.

3. It is assumed that structures are located in zone 4, according to UBC97.

4. The P-Delta effect is included in the analysis.

The Poisson's ratio, elastic modulus and yield stress for the structure are equal to 0.3 , 2.0 × 10^{6} kPa and 2400 Kg/cm^{2}, respectively. The ADAS devices are fabricated on each floor and are supported by chevron bracing. The value of *a* in Eq. (16) is considered to be 0.12, and the range of the ductility ratios for the ADAS dampers is controlled between 3 and 5 [25].

The ADAS devices lower 80 percent of the column shear forces using this procedure when the whole system is subjected to different Earthquake ground movements. Nonlinear time history analysis involves the computation of dynamic response at each time increment concerning due consideration given to the inelasticity in members. Hysteretic energy under cyclic loading is evaluated and tabulated. During strong and mediocre earthquakes, structures enter the plastic range. Therefore, it is essential to perform a nonlinear analysis. For this purpose, numerical simulations were carried out by PERFORM 3D.V4 [17]. The damping ratio of structures is selected 5%, proportional to mass and stiffness matrix. The plastic hinges in analysis are assumed elastic-perfectly plastic. The non-linear behavior of models is assumed from FEMA273 [2]. Beams and columns are modeled as beam-column elements with a strain hardening of 3%. Bracings are considered as a truss-element that have capability of yielding in tension and buckling in compression and have a strain hardening of 3%. For modeling ADAS an equivalent prismatic beam is used. The mass of structure concentrated in the joints and distributed loads on the beams are applied as fixed end moments on end joints of beams.

**4.1 Characteristics of earthquake records used**

Unscaled earthquake records are tabulated in Table 2. In this study, scaled records are used for nonlinear dynamic analysis with PGA scaled to 0.4g, 0.6g and 0.8g. Figures 6 to 8 represent the acceleration recorded during three earthquake records (Tabas, Northridge and Imperial Valley) with PGA = 0.4g.

**5 BASIC ASSUMPTIONS IN PERFORM 3D**

**5.1 PERFORM F-D relationship**

Most of the inelastic components in PERFORM-3D have the same form for the F-D relationship. Figure 9 shows a trilinear relationship with optional strength loss. Strength loss is ignored in non-linear analysis of systems.

There are key points in the relationship; Y point represents the first yield point, where significant nonlinear behavior begins. U point shows the ultimate strength point, where the maximum strength is reached. L point is the ductile limit point, where significant strength loss begins.

R Point is the residual strength point, where the minimum residual strength is reached and the X Point is usually at a deformation that is so large that there is no point in continuing the analysis.

**5.2 Hysteresis loops**

Two hysteresis loops are shown in Figure 10. In one loop the stiffness degrades and in the other loop it does not. For the degraded loop the amount of energy that is dissipated (the area of the loop) is smaller. The amount of stiffness degradation has the most effect on the amount of energy degradation.

We accounted for the stiffness degradation in the hysteresis loop because the seismic response of a structure is sensitive to the amount of energy dissipation.

**5.3 Dynamic analysis**

For step-by-step dynamic analysis, because the stiffness and energy degradation is important in our analysis we accounted for directly, by changing the shape of the hysteresis loop as indicated in Figure 8.In PERFORM-3D we can do this by specifying Energy Degradation Factors for inelastic components. In Figure 10 the Energy Degradation Factor is the ratio between the area of the degraded hysteresis loop and the area of the non-degraded loop. For a typical component, this area ratio is 1.0 for small deformation cycles (no degradation) and gets progressively smaller as the maximum deformation increases (increasing degradation).

**5.4 Time step**

The analysis is performed using step-by-step integration through time, using the constant average acceleration method (also known as the trapezoidal rule or the Newmark β = ¼ method). We specified the integration time step. The number of steps is the total time divided by the time step, unless the analysis terminates before the end of the earthquake. Since dynamic earthquake analyses can be time consuming, it is natural to want to use as large a time step as possible. A 0.005s time step is used for all non-linear analysis of models.

**6 RESULTS AND DISCUSSIONS**

**6.1 Input energy**

The energy exerted on the structure under earthquake vibrations is a function of time and in order to investigate the vibration behavior of different systems in earthquakes, one can compare the incremental input energy at each time step or the total input energy of those systems. The behavior of the systems varies with the input energy for each time step due to their corresponding nonlinear behavior, transient change in the frequency content of the earthquake, and also the systems' vibration-period changes during earthquake as an effect of the aforementioned nonlinear behavior. Furthermore, total input energy is more meaningful in the design of the structures and earthquake engineering; therefore, in this study, we have utilized the maximal total input energy in the structures to compare their behavior.

**6.2 Hysteretic energy**

As previously mentioned about the input energy, hysteretic energy or plastic energy in a structure also is a function of time and for comparing the performance of different systems under earthquake records, the maximum total hysteretic energy at the end of the earthquake is considered.

For the purposes of illustration and obtaining better conclusions about the performance of the CBF systems and ADAS systems, we focus on the ratio of the hysteretic energy to the input energy and the effect of different parameters like the height of structures, increasing and decreasing of the PGA's and the effects of the different records, is inspected too.

**6.3 Effect of increase or decrease in structure height on the ratio of hysteretic energy to input**

Height of the structure has the most influence on the shape of maximum total input energy for systems. Also Considering an average diagram with respect to earthquake records and type of systems, yields Figure 14, which shows the effect of height variation on input energy.

Fig. 14 demonstrates the effect of changes in the structure height on the input energy in the ADAS and CBF systems, under the records of the far field. As appear from Figs. 11-13, the input energy in both systems decreases with an increase in height. This decrease is specifically higher in the ADAS system than that in the CBF system, which implies better performance for the ADAS system in tall structures. Moreover, it is evident from this figure that the ratio of hysteretic energy to input in an ADAS system is bigger than that in a CBF one.

**6.4 Effect of PGA variation on the ratio of the hysteretic energy to input energy **

Figs. 15-17 depict the impact of variations of maximum acceleration of the earthquake on the ratio of hysteretic energy to input under records of the far field for 5, 10, 15 story buildings under far field records with PGA 0.4g, 0.6g, 0.8g. As it is indicated in the figures the value of the ratio (Eh/Ei) in the steel braced frame equipped with ADAS devices is more than the CBF system. It is considerable that the performance of the ADAS systems is better than the CBF systems. As seen from Figs. 15-17, the hysteretic-to-input ratio is almost constant for the ADAS system with increasing PGA which means nothing but limitation for an ADAS system in absorption of the hysteretic energy in high values of PGA; nonetheless, the value of hysteretic-to-input ratio is much higher in the ADAS system than that in a CBF one.

Fig. 18 shows the increasing rate of hysteretic-to-input ratio with respect to increase in PGA and has been plotted for both of these structural systems in the far field. Apparently, according to the figure, Hysteretic-to-input ratio for the ADAS system under records of the far field is not affected by the increase in PGA value, whereas for the CBF, it increases with PGA increase. In fact, this ratio slightly dwindles with height increase in the ADAS system, contrary to the CBF case where it asymptotically rises with PGA increase. Generally, we can conclude that in the records of the far field, performance of the ADAS systems outstrips that of the CBF ones.

**7 CONCLUSION**

The current study shows the difference of building behaviors with and without damper during earthquake vibrations under the far field records.

1. Having investigated the effect of the building height on the input energy and the plastic energy of the CBF and ADAS systems, we have observed that the vibration behavior of the buildings located in the far field of the fault, based upon the frequency content of the earthquake, depends on the geometric specifications of the building including its height.

2. Increase or decrease in the maximum acceleration does not appear to have much impact on the general form of the comparative graphs of input energy for different systems; as well, PGA increase leads only to a boost in the deviations of the input energy between different systems.

3. With a higher earthquake energy absorption capacity and a larger ratio of the plastic energy to input energy, the ADAS system has a superior vibration performance compared to that of the CBF structural system, esp. under records of the far field.

This study implements the commercial package PERFORM 3D.V4, information regarding the seismic hazard, passive control system and nonlinear structural response. The ADAS devices significantly increase the resistance of the structure components to the dynamic loads and they are effective in reducing the seismic response of the structures. The benefits of the energy dissipaters have been clearly demonstrated by these comparative data and the improvement in performance of structures during earthquake excitation have been proved. In addition, the considerable effect of the ADAS dampers in absorbing hysteretic energy is illustrated. The passive control system absorbs the vibrations automatically without the need of an electrically controlled system. Passive control systems are generally low in cost and effective for support of buildings subjected to dynamic vibrations. It will allow practicing engineers to design and use cost-effective seismic dampers in the preliminary design phase effectively, letting them explore the cost factors by comparing different building seismic performance objectives throughout design.

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Received 4 Dec 2010

In revised form 22 Jan 2011

* Author email: mbayat14@yahoo.com