Effect of Dampers on Seismic Demand of Short Period Structures

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Effect of Dampers on Seismic Demand of Short Period Structures

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Jordan Journal of Civil Engineering, Volume, No., 21 Effect of Dampers on Seismic Demand of Short Period Structures Nazzal S. Armouti Associate Professor of Civ il Engineering. Un iversity of Jordan. Email: armouti@ju.edujo ABSTRACT Seismic behavior of 8 single bay frame with diagonal damper that represents short period structures is evaluated in response to the excitation of a set of earthquake records. The ft-ame system is modeled as a Generalized Single Degree of Freedom (GSDOF) systcm, and is subjected to nine earthquake records representative of the range of dominant site conditions. The relcltionship between the force modification factor and the global ductility demand for short pel-iod stl"llctures. in the presence of dampers, tends to approach those of long period ones. Dampers with high damping ratios tend to keep the structural response in the elastic range even for high values of foi'ce reductions. Seismic code provisions should be revised to account for short period efceet under seismic excitation. KEYWORDS: Ductility demand, Seismic demand, Short period, Dampers. INTRODUCTION Earthquake-resistant structures are generally designed with strength much less than their elastic strength demand due to earthquake excitation According to modern seismic codes, typically well-detailed structures may be designed with strength capacity as low as 12% of their elastic strength demand (!BC, 26). This reduction in strength demand is possible due to many factors such as ductility, energy dissipation and frequency shift. In general, such strength reduction imposes special demand on structures in terms of detailing to achieve specified levels of ductility and energy dissipation which are function of the specified levels of strength reduction. Seismic codes, in general, utilize parameters such as force modification factor, R, and global ductility demand, )..tj, to implicitly account for strength reductions. Force modification factor is Aeecpli.:d for Publication on 15/1 /2 I O. defined as the ratio of elastic strength demand to actual yield force of the structure, whereas, global ductility demand IS defined as the maximum inelastic displacement under seismic excitation to the actual yield displacement of the structure. However, the codes do not explicitly address the damping of structures which is an indication of the energy dissipation capacity of the structme. FUl1hermore, codes do not distinguish between short period and long period structures in their treatment of strength and ducti Iity requirements for the design of eat1hquake-resistant structures. Many research results on seismic demand indicate that even though ductility demand is feasible for long period structures (tall buildings), they impose high levels of ductility for Shl1 period structures which may not be achievable (Nassar and Krawinkler, 1991). FUl1hermore, research results also indicate that ductility demand is very sensitive to strength reduction for short period structures (Armouti, 23). Consequently, shot1 period structures should rely on factors other than ducti lity to achieve strength reduction - 367-21 JUST All Rights Reserved.

Effect of Dampers... Nazzal S. Armouti such as energy dissipation. Therefore, this study focuses on examining the effect of explicit damping on ductility demand on one hand, and on the feasibility of dampers as an alternative to ductility requirements for short period structures on the other. Dampers are widely used in structures to alleviate the harmful effect of earthquakes on structures. Dampers are known to be used in new buildings (Nagarajaiah and Narasimhan, 27), in bridges (Madhekar and Jangid, 29) and in retrofit of existing structures (Malhotra et ai., 2; Potty and Nambissan, 28). Dampers have proven to be effective systems for reducing earthquake forces in structures (Chandra et ai., 2; Raju et ai, 25). In order to examine the effect of dampers on the behavior of short period structures under seismic excitation, a typical one bay frame with a diagonal viscous damper is considered for this study to examine the effect of viscous dampers on the R-ld relationship. A frame with a damper having a coefficient of damping, C, is subjected to a horizontal component of ground motion, u g, as shown in Fig. I. In order to get a better understanding of the effect of ductility and energy dissipation as outlined above, and to be consistent with previous studies on this subject, the frame is modeled as a generalized Single Degree of Freedom (SDOF) system, and subjected to nine earthquake records used in previous studies (Armouti, 23). Consequently, the force reduction factor, R, and the global ductility demand, fill, are valuated and compared with previous studies to examine the effect of damping on the ductility demand as an indicator of the behavior of short period structures. To achieve these objectives, a parametric study using inelastic dynamic analysis is performed by varying the period and the intensity of earthquake excitation. The parameter variation includes five periods, five levels of relative yield ing of the hysteresis model and four damping ratios for each of the nine earthquake records. This parameter variation results in 9 pairs of Rand fid values as a result of 225 runs of elastic dynamic analysis and 9 runs of inelastic dynamic analysis which are grouped and evaluated. For completeness of presentation, a description of the structure, the earthquake records used and the inelastic dynamic analysis procedures, including the hysteretic model of the frame, are presented. STRUCTURAL MODEL As previously mentioned, the structural model is selected as a frame having four nodes I through as shown in Fig. 1. The frame consists of one bay firame fixed at both supports. The frame is provided with explicit diagonal viscous damper with coefficient of damping, C, between nodes 2 and. The frame may be modeled as a Generalized Single Degree of Freedom (GSDOF) system by assuming the total mass to be lumped at one node, node 2, as shown in Fig. 2. The generalized degree of freedom in this case is the mass displacement in the direction of u at node 2. The generalized resistance of the frame without the damper is obtained due to an induced displacement of the mass in direction, u, as a generalized spring force, Fs', whereas the component of the reactive force of the damper in the direction of displacement, 1I, is obtained due to induced velocity in the direction of, U, as the generalized damping force, FD'. In case of elastic analysis, the generalized stiffness, k', is simply evaluated by subjecting the frame to a unit displacement in direction of, u, which can be easily obtained by any structural analysis software. The generalized coefficient of damping, C', can be obtained as function of the damper coefficient of damping, C, with reference to Fig. 3 as follows: Since damper velocity is UD = U cos e The force in the damper is given as. FIJ = C. UD = C cose u The generalized force of the damper in the direction of, u, becomes: Fu' = FIJ cos e = U = C' U Therefore, the generalized damping becomes: c = c. co/ e - 368

Jordan Journal of Civil Ellgilleerillg, Volume, No., 2 I u, U, U 2.,..-;::,.----3-----------,3 H Damper C (J L Figure I: Frame layout Fs m* u, u, u H Damper C Figure 2: Lumped mass as GSDOF L Figure 3: Generalized damping due to velocity, U (J Fs' Fo* Ft.-7 m* u, u, u Figure : Generalized SDOF Soft Deep cohesion less,'..... Rock site 1 2 3 5 6 Frequency (rad Is) Figure 5: Distribution of power spectral density of earthquakes according to their site conditions - 369

Effect of Dampers... NazzJl S. Armouti Normalized acceleration Acceleration history o 5 1 IS -/ Time (sec) 2 Fourier Amplitude, L ft.6..2 - - - rier amplitude spectrum o o 1 2 SO 3 6 Frequency (rad Is) Figure 6: Properties of synthetic record Dl.nsa Restoring Force, F Displacement, U Figure 7: Bilinear hysteresis model - 37

Jordan Journal of Civil Engineerillg, Volume, No., 2 1 1 ::..: t5 c.q ro u l;:= '6 E OJ t! LL 9 8 7 6 5 3 2 T =.1 s T =.2 s.6. T =.3 s o T =. s JI( T =.5 s,., I" A ;:( ;( A 1: ;:( ';t Ao :( ) " A, 1: 2 6 8 1 Global ductility demand, ld Figure 8: Relationship between force modification factor and global ductility demand at a damping ratio of2% :: t5 c. u " E OJ u LL 1 9 8 7 6 5 3 2 I T =.1 $' =.2 l:;, $' =.3 1o $' =. ",;r. :(.: $' =.5... :c. S... ;r )''8.... :( i I o. o '*.tj.... 2 6 8 1 Global ductility demand, Pd Figure 9: Relationship between force modification factor and global ductility demand at a dam ping ratio of % - 371

Effect of Dampers... Nazzal S. Armouti Parameter C 3 Nassar and Krawinkler Curve Post yield stiffness =1% C, = 5% typical 2. L.5 1.5 2 2.5 3 Period (sec) I Figure 1: Relationship between parameter C and period (Nassar and Krawinkler, 1991) Force modification factor. R 7 Data point 6 _ Regression 5 3 2 5 2 2 3 Global ductility demand, Pd Figure 1 I: Sample nonlinear regression curve for C value at a period of.1 sec and a damping ratio of 2% The frame system, therefore, can be represented by a [n case of elastic analysis system with a generalized single dynamic degree of m*u + C*u + k" u = -m'u g freedom consisting of a lumped mass subjected to u+2t;(jju + oju=-u g generalized forces and displacements as shown in Fig. where. The equation of motion in this case takes the form : u = generalized displacement. F/+ Fu' + Fs' = -m' iig u = generalized velocity. - 372

Jordan Journal of Civil Engineering, Volume... 21 ij = generalized accelej'3tion. u g = ground acceleration (ealihquake). m' = generalized mass. F/ = generalized ineliial force. "= generalized coefficient of damping. Fv" generalized damping force. k * -= generalized stiffness. Fs' = generalized spring force. (1)= frequency of the generalized system. ; = damping of the generalized system. Since the parametric study uses predefined values of period and damping ratios, the exact values of these parameters, in this study, become immaterial. Therefore, the values of mass, stiffness, damping and level of ground motion are adjusted to produce the intended parameter values of the study. Consequently, the force reduction factor, R, is defined as the ratio of the elastic strength demand of the structure, Fe, to tile actual yield strength, F l', whereas global ductility demand, ld, is defined as the ratio of the maximum displacement that is reached during the excitation history, u nlox, to the actual yield displacement of the structure, u)'. These ratios are given in mathematical form as follows: R = Fe F ' y U max jjd = --. U y RECORDS OF EARTHQUAKES In view of alihquake characteristics, ealihquake l'ecords are selected to be representative of the dominant site conditions found in reality; namely, rock sites, sand sites and clayey sites. In order to be comparative, the nine synthetic records that are used in this analysis were adopted from previous studies (ArmoLlti, 23). The records are based on the PSO distribution given in Fig. 5. Using this PSO distribution, nine synthetic records are generated and grouped into 3 subgroups; rock-based, deep cohesion less-based and soft so il based. If the letter (R) indicates rock site, the letter () indicates deep cohesionless site and the letter (S) indicates soft site for future reference, these records are designated as R I.nsa, R2.nsa, R3.nsa, Ol.nsa, 2nsa, 3.nsa, S I.nsa, S2.nsa and S3.nsa. A sample of these records, Ol.nsa, with its associated FOUl-iel' amplitude spectrum are shown in Fig. 6. INELASTIC DYNAMIC ANALYSIS The purpose of this study is to examine the effect of viscous dampers on the relationship between R and d for short period structures. Since the relationship between R and Pd can be only evaluated in a statistical sense due to the extreme randomness and Llnceliainty of ealihquake characteristics, inelastic dynamic analysis (C lough and Penzien, 1993) is needed to generate a data base for this purpose. In addition to the selected nine earthquake records, the parameter variation includes five periods, five ductility ratios and four damping ratios resulting in 9x5 x5x=9 data points. The inelastic dynamic analysis can be performed using SAP2 software (CS[, 28) under Time History Function. The GSOOF frame may be modeled in SAP2 as direct elasto-pl:lstic link, whereas the damper is modeled as damper link. The parameters of the link and the damper are selected in view of the intended parameter variation values in conjunction with the equation of motion which is given before as: m *ii + C" U + k* u = -n/ ii 9. In case of inelastic dynam ic analysis, the stiffness will not be constant, and hence the frame resistance is taken as a reactive generalized restoring force, Fs", hence the equation of motion take its final form as: m*ii +C* u + F. \ = -m' ii 9 where u = generalized displacement of the mass III the direction of the single degree of freedom. U = generalized mass velocity. ii = generalized mass acceleration. ii g = horizontal ground acceleration. Ill' = general ized total mass. C* = generalized coefficient of viscolls damping. Fs' = generalized restoring force (hysteresis model). - 373 -

Effect of Dampers... Nazzal s. Armouti Parameter C - N& r z = 2% 3 t z = % o 2 I :!( -+-- o z = 6% l :.: z = 8% I o. 7!------------ :!(o L o o 5 1.5 2 2.5 3 Period (sec) Figure 12: Values of parameter C for different periods from this study against reference model from N&[( Parameter C 2 - N& z = 2% z = % z = 6% :I( z = 8% o J * o.1.2.3..5.6 Peri od (sec) Figure 13: Values of parameter C for different periods from this study against reference model from N&K The structural response is rep resented by a bilinear is selected as 1 kn/m, whereas th e mass is calibrated hysteresis model with post yielding stiffness equal to fo r each case to obtain the desired period since the 1% of its initial stiffness as shown in Fig. 7. The period is given as: properties of the hysteresis model are included in SAP T h J::. 2 through th e el asto-plastic link nonlinear propeliies. A yield force of 1 kn and yield The generalized damping coefficient is calculated in displacement of.1 m are used for this purpose. Since view of the desired damping ratio and the selected mass the model propeliies are required arbitrarily to obtain a and stiffness as follow s. predefined period, the elastic stiffne ss, ko, of the model The critical damp ing, e'er, is calculated as: - 37

Jordan JOllmal ofcivil Engineering, Volume, No., 2 I The damping coefficient, C', is then calculated as function of damping ratio, c" and critical damping, e 'CR, as: are shown in Fig. 8 for 2% damping I'atio and in Fig. 9 for % damping ratio. It can be noticed that the data points still exhibit the level of randomness associated with such analysis, NASSAR AND KRA WINKLER MODEL The five periods of the model al'e chosen by adjusting the mass to produce the desired period. Since the R- l <I relationship is targeted in th is study for short period structures, the five periods used in this study are.1,.2, 3 and. seconds. A fifth period of.5 second is also included in the study as it marks the bordel' line between short and long period values of structmes under typical ealihquake excitation. In order to obtain various levels of R values, the yield level of the frame is kept constant whi Ie changing the intensity of the ecllihquakes; i,e. the peak ground accderation of the ealihquakes. Accordingly, the parameter variation is generated by taking a different level of peak ground acceleration for (,<lch period and each c:arthquake record. The elastic strength demand; i,e. the maximum elastic foi'ce,, and the maximum elastic displacement, u e, are then obtained using elastic dynamic analysis; i.e. Time History Analysis with infinite yielding. For each value of, Fe, an R-value is calculated as follows: For each value of R obtained above and for each level of damping of the damper, inelastic dynamic analysis; i,e. Time History Analysis with yielding force, at 1 kn, is performed to evaluate the maximum displacement demand during the time of excitation, u m,, Knowing umo< and u y, d is calculated as follow s: U max Pd=--. u y A total number of 9 pairs of R and Id from the above procedmes are obtained. Samples of such results An extensive study resultl:d in a large data base of seismic dcmand chal'actel'istics using fifteen actual eliihql'dke records, Nassar and Krawinkler, N&K, (Nassar and i..rawinkler, 1991) have proposed the following cxprcssion for a relationship between Rand ijd factors: where C is gi en as R = [C (Prl) + I}' ( T" b Cm = --+-. 1+ T" T For a bilinear model with 1% post yielding stiffness and typical damping ratio of 5%, &K have used nonlinear regression analysis to produce values of (a = 8) and (b.29). Us ing these values, a plot of the parameter C ver:;us the period T is shown in Fig. 1. This figure will be used in this study as the reference relationship between R and ld for a bilinear hystcrisis model under the excitation of eatihquake records. It is worthwhile to mention that when the value of the parameter C = I, the R-Pd relationship tends to the well known equal dispjacement criterion (R = I-Id); and when the value of the parameter C = 2, the R-flJ relationship tends to the well known equal energy criterion (R=). It is wolihwhile also to point out that, in the statistical sense, the C-T relationship shown in Fig. 1 seems to become stcady in the long period region (T >.5 sec). FOI' long period regions, where parameter C is low (C< I), ductility demand is usually low and stcady, whereas, for sholi period regions where parameter C is high ( > I), the seismic demand becomes sensitive and high. This type of behavior is known to be a characteristic behavior of stl'ltctures in response to ealihquake excitation. It should also be pointed out that when the value of C is - 375

Effect of Dampers... Nazzal S. Armouti greater than one, the ductility demand becomes more than the force reduction values, and when the value of C is smaller than one, the ductility demand becomes less than the force reduction values. ANALYSIS OF NUMERICAL RESULTS Evaluation of the numerical results obtained as outlined previously IS accomplished through comparison with N&K model which is established by finding the parameter C at the selected periods of the system under the excitation of the selected earthquake records at a each damping ratio. The resulting values of the parameter C will then be compared with C-T plot results from N&K model. Figure II shows one sample of nonlinear regression curve used to find the parameter C for a period of.1 sec at a damping ratio of2%, for which a value ofc = 2.75 is obtained. Similar nonlinear regression analysis is conducted to produce the rest of the C-values for the selected periods as given in Table I. Table 1: Nonlinear regression results for parameter C Period (second) Damping ratio 2% % 6% 8%.1 2.75 2.35 2.9 1.88.2 1.2.89.56.31.3 1.8.63.35.18..8.31 *** ***.5 1.3.67.39.17 Fig. J2 and Fig. 13 show a comparison between the obtained C-values from this study and the reference N&K model. It can be seen that the results from this study lie below the reference curve. It can also be noticed that the C-values for the period of.1 second remain above the value of one which means that, for this period even with high values of damping, the ductility demand remains higher than force reduction. However, high damping brings the level of demand closer to a value of two which is the equal energy criterion. Fig. 12 and Fig. 13 aiso indicate that 2% damping has reduced the ductility demand, but not with great va lues. However, except for the period of O. I second, damping ratios of % and higher bring the ducti lity demand of short period structures to comparable values of long period structures, and even to lesser values. Referring to Fig. 8 and Fig. 9, the scatter of data can be observed which is reflected by the extreme randomness of earthquakes and their random effect on the response of structures. Careful examination of these two figures shows that the data points of Fig. 9 (% damping) seem to shift to the left of the data points of Fig. 8 (2% damping), indicating less ductility demand with increased damping. FLilihermore, it should be noticed that many responses of the structure remain elastic at reduced force values which are marked by the values of(r > I) and the values Of(ld < I). Compal'ison between Fig. 8 and Fig. 9 indicates also that the points which remain elastic at reduced force are much more for the case of % damping than for the case of 2% damping. It can be noticed also that the structure with % damping remains elastic at higher values of R (R>3) than the structure with 2% damping (R<3 ). Tn other words, the reduction of elastic strength demand is simply shared between the system ductility and the damper. CONCLUSIONS Response of structures to ealihquake records is known to impose high ductility demand for short period structures much higher than those of long period structures. Such high demand for short period structures may not be even feasible to achieve. Seismic codes, in general, overlook this issue and do not distinguish between long and short periods in relation to this matter. In order to shed light on this issue, this study evaluates the effect of explicit dampers as a mean of alleviating the high ductility demand for short period structures through a parametric study on one bay frame with diagonal damper. This paper examines this issue through the relationship between the force modification factor and the global ductility demand under seismic - 376 ----- -- ---

Jordan Journal ofcivil Ellgilleering, Volume, No., 2 I excitation as defined by most modern seismic codes (lbc, 26). This relationship constitutes the basic relationship for defining seismic design forces and the associated required ductility capacities. Tn view of the extreme randomness of earthquake characteristics and the reflection of this randomness on the response of structures, the results presented in this paper indicate, in statistica I sense, that the response of short period structures to ealthquakes after yielding is in fact sensitive and highly demanding. In addition, they indicate that th e dampers with damping ratios up to 2% of critical damping tend to reduce the ductility demand consistently with the period values without any significant change. However, dampers with higher critical damping more than 2% seem to bring the behavior of sholt period structures to levels of the behavior of long period ones. Even more, they show that higher damping improves the behavior of ShOlt period structures to levels that are fea sibly achievable in practice. ft has also been found that the higher the damping presence in the structure, the higher will be the presence of elastic behavior of the structure at even highel' values of force reduction. It can be concluded that the response of sholt period stl"uctures without damping, and of course without seism ic isolation, is difficult to control and difficult to design with reasonable levels of safety. As this issue is overlooked in seismic codes, structures with sholt periods should be carefully designed taking into consideration additional meas ures other than ductility to include some acceptable levels of safety. FLllthennore, seismic codes ought to revisit the concept of force reduction and distinguish between long period structures and sholt period structures. Short period structures may need additional provisions to provide them with enough safety measures. REFERENCES Armouti, N. S. 23. Response of structures to synthetic earthquakes, Proceedings of the 9 'h Arab Structural Engineering Conference, I: 331-339, Abu Dhabi, UAE. Chandra, R., Masand, M., Nandi, S., Tripathi, c., Pall, R. and Pall, A. 2. Friction-dampers for seismic control of La Gardenia towers south city, Gmgaon, India, Proceedings of the 121 World Conference on Earthquake Engineering, Auckland, Paper 2S, New Zealand. Clough, R.W. and Penzien, J. 1993. Dynamics of structures, 2"d Ed., McGraw Hill, New York. CSI. 2S. Structural analysis program, SAP 2 nonlinear version 12, Computers and Structures, Inc., Berkeley, Cal ifornia.!bc. 266. International building code, International Code Council, Washington, DC. Madhekar, S. and Jangid, R. 29. Variable dampers for earthquake protection of benchmark highway bridges. Smart!\I!ateria!s and Structures, IS( II), 115 II (IS). Malhorta, A., Carson, D. Gopal, P, Braimah, A., Giovanni, G. and Pail, R., 2. Friction dampers for seismic upgrade of St. Vincent hospital, Ottawa. Proceedings of the 13 'h World Conference on Earthquake Engineering, Vancouver, Paper No. 1952, B.C., Canada. Nagarajaiah, S. and Narasimhan, S. 27. Seismic control of smart base isolated buildings with new semiactive variable damper. Earthquake Engineering and StruC'lura! Dynamics, 36 (6): 729-79. Nassar, A.A. and Krawinkler, H. J991. Seismic demands for SDOF and MDOF systems, Report No. 95, The John A. Blume Ealthquake Engineering Center, Stanford University, California. Potty, N. and Nambissan, S. 2S. Seismic retrofit of elevated steel water tanks. Proceedings of the International Conference on Construction and Building Technology, 99-1 OS, Kuala Lumpur, Malaysia. Raju, K., Prasad, A., Lakshmanan, N., Muthumani, K., Jagadish, D. and Amuthasheela, R. 25. Optimum distribution of viscous fluid dampers in structural systems. Journa! ofthe!nstilulion ofengineers (!ndia), S6: 13-IOS. - 377 -