Report - PEER - University of California, Berkeley

Report - PEER - University of California, Berkeley Report - PEER - University of California, Berkeley

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Yield Strength Coefficient, Cy*1.61.4Elastic Design Spectrum1.2Ductility = 21.0Ductility = 40.8Ductility = 80.60.40.380.2µ=2.30.0*∆ y = 0.1040.0 0.1 0.2 0.3 0.4 0.5Base Shear/Weight0.40.350.30.250.20.150.10.05Cy = 0.329Yield Drift = 1.11%00 1 2 3 4(b) Roof Displacement/Height (%)(a) Yield Displacement, mFigure 5. (a) YPS for design of 3-story frame, and (b) capacity curve obtainedfrom pushover analysis.where g= the acceleration of gravity. (If the capacity curve exhibits early softening,formulas such as those in ATC-40 can be used to relate the initial and effectiveperiods of vibration.)As an example, the design of steel moment-resistant frames is typicallycontrolled by drift. Suppose that the roof drift of a 3-story frame is to be limited to2.5% of the building height and that story heights are 4 m. Assuming that the roofdrift at yield is 1.1% of the height, the system displacement ductility limit is µ =2.5/1.1= 2.3. The roof drift at yield is estimated to be ∆ y = (1.1%)(4 m)(3) = 0.132 m.The ESDOF yield displacement is estimated to be ∆ y * = 0.132/1.27 = 0.104 m, basedon an estimate of Γ 1 from Table 1.Using the YPS of Figure 5a, the required yield strength coefficient, C y * , is 0.38.The corresponding base shear coefficient (at yield) is C y = 0.38(0.90) = 0.34, based onan estimate of α 1 from Table 1. The corresponding period, T, is 1.05 s according toEquation (4).A design nominally satisfying these requirements is the 3-story moment-resistantframe designed for Los Angeles in the SAC steel project. The capacity curve for thisframe, corresponding to the “M1” model in which beam-column elements extendbetween nodes located at the intersections of member centerlines, is given in Figure5b. The base shear coefficient is 0.329 and fundamental period is 1.01 sec, making theframe slightly stiffer than is needed on the basis of the estimated properties. Theactual values of Γ 1 and α 1 (1.27 and 0.83, respectively) can be used to refine the yielddisplacement estimate to ∆ y * = (1.11%)(4 m)(3)/1.27 = 0.104 m and the required baseshear coefficient to 0.38(0.83) = 0.32. The actual base shear coefficient slightlyexceeds the required base shear coefficient, resulting in a slightly lower period ofvibration and a smaller displacement ductility demand, indicating acceptableperformance. Further refinement of the design is not warranted at this stage.The preceding illustrates that in a single step the strength can be selected tosatisfy limits on roof drift and system ductility. This is simpler than other proposalsfor performance-based design and current design procedures, which often requireseveral design cycles to satisfy code drift limits. This simplicity is possible when487

Yield Strength Coefficient, Cy*1.61.41.21.00.8Elastic Design SpectrumDuctility = 2Ductility = 4Ductility = 80.60.40.2µ=2.30.0*∆ y = 0.104* ∆u0.0 0.1 0.2 0.3 0.4 0.5Yield Displacement, m(a)Yield Strength Coefficient, Cy*1.61.4Elastic Design Spectrum1.2Ductility = 21.0Ductility = 40.8T= 1.05 sec Ductility = 80.60.40.20.0*∆ y*∆ u0.0 0.1 0.2 0.3 0.4 0.5Yield Displacement, mFigure 6. The influence of strength on peak displacement response (indicated by an“x”) for (a) a given yield displacement, and (b) a given period.demands are represented using YPS and design is based on an estimate of the yielddisplacement. As indicated by Equation (4), the period is a consequence of thestrength required to satisfy the performance specification. Figure 2 illustrates that theyield displacement typically is independent of the strength provided. Therefore, had adifferent roof drift limit, a different hazard level, or a number of performanceobjectives been considered, the required base shear strength would have differed, butthe associated yield displacement would have remained constant or nearly so.More generally, the influence of lateral strength on peak displacement response isillustrated in Figure 6. Given a yield displacement estimate, one simply selects thestrength that results in acceptable displacement and ductility demands (Figure 6a). Incontrast, if the period is presumed to be known, the influence of strength ondisplacement is as illustrated in Figure 6b. In this case, the equal displacement ruleapplies, indicating that strength affects displacement ductility demands but not peakdisplacement. Consequently, proposals for design that use period as a fundamentaldesign parameter must assume the period is unknown and can be varied (inconjunction with strength) to achieve the desired performance. In reality, a continuumof yield points exist that will satisfy the performance objective. The engineer,however, generally does not have the latitude to provide the strength and stiffnessassociated with a particular yield point, selected arbitrarily from the continuum thatsatisfies the performance objective. Thus, proposals that use period as a fundamentaldesign parameter inevitably will be iterative, as infeasible yield points are tried anddiscarded in the search for an acceptable design. The stability of the yielddisplacement is exploited here to reduce or eliminate the need for iteration in design.The base shear strength required of alternative structural systems may beevaluated in this fashion to determine the system best-suited to any particularapplication. Once the best-suited system has been identified, member depths andspans can be adjusted (within architectural constraints) to modify the yielddisplacement in order to reduce the required base shear strength (and cost).(b)488

Yield Strength Coefficient, Cy*1.61.4Elastic Design Spectrum1.2Ductility = 21.0Ductility = 40.8Ductility = 80.60.40.380.2µ=2.30.0*∆ y = 0.1040.0 0.1 0.2 0.3 0.4 0.5Base Shear/Weight0.40.350.30.250.20.150.10.05Cy = 0.329Yield Drift = 1.11%00 1 2 3 4(b) Ro<strong>of</strong> Displacement/Height (%)(a) Yield Displacement, mFigure 5. (a) YPS for design <strong>of</strong> 3-story frame, and (b) capacity curve obtainedfrom pushover analysis.where g= the acceleration <strong>of</strong> gravity. (If the capacity curve exhibits early s<strong>of</strong>tening,formulas such as those in ATC-40 can be used to relate the initial and effectiveperiods <strong>of</strong> vibration.)As an example, the design <strong>of</strong> steel moment-resistant frames is typicallycontrolled by drift. Suppose that the ro<strong>of</strong> drift <strong>of</strong> a 3-story frame is to be limited to2.5% <strong>of</strong> the building height and that story heights are 4 m. Assuming that the ro<strong>of</strong>drift at yield is 1.1% <strong>of</strong> the height, the system displacement ductility limit is µ =2.5/1.1= 2.3. The ro<strong>of</strong> drift at yield is estimated to be ∆ y = (1.1%)(4 m)(3) = 0.132 m.The ESDOF yield displacement is estimated to be ∆ y * = 0.132/1.27 = 0.104 m, basedon an estimate <strong>of</strong> Γ 1 from Table 1.Using the YPS <strong>of</strong> Figure 5a, the required yield strength coefficient, C y * , is 0.38.The corresponding base shear coefficient (at yield) is C y = 0.38(0.90) = 0.34, based onan estimate <strong>of</strong> α 1 from Table 1. The corresponding period, T, is 1.05 s according toEquation (4).A design nominally satisfying these requirements is the 3-story moment-resistantframe designed for Los Angeles in the SAC steel project. The capacity curve for thisframe, corresponding to the “M1” model in which beam-column elements extendbetween nodes located at the intersections <strong>of</strong> member centerlines, is given in Figure5b. The base shear coefficient is 0.329 and fundamental period is 1.01 sec, making theframe slightly stiffer than is needed on the basis <strong>of</strong> the estimated properties. Theactual values <strong>of</strong> Γ 1 and α 1 (1.27 and 0.83, respectively) can be used to refine the yielddisplacement estimate to ∆ y * = (1.11%)(4 m)(3)/1.27 = 0.104 m and the required baseshear coefficient to 0.38(0.83) = 0.32. The actual base shear coefficient slightlyexceeds the required base shear coefficient, resulting in a slightly lower period <strong>of</strong>vibration and a smaller displacement ductility demand, indicating acceptableperformance. Further refinement <strong>of</strong> the design is not warranted at this stage.The preceding illustrates that in a single step the strength can be selected tosatisfy limits on ro<strong>of</strong> drift and system ductility. This is simpler than other proposalsfor performance-based design and current design procedures, which <strong>of</strong>ten requireseveral design cycles to satisfy code drift limits. This simplicity is possible when487

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