a practice-oriented method for estimating elastic … · kieran haymes1, timothy j. sullivan2 and...

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116 Bulletin of the New Zealand Society for Earthquake Engineering, Vol. 53, No. 3, September 2020 A PRACTICE-ORIENTED METHOD FOR ESTIMATING ELASTIC FLOOR RESPONSE SPECTRA Kieran Haymes 1 , Timothy J. Sullivan 2 and Reagan Chandramohan 3 (Submitted November 2019; Reviewed December 2019; Accepted March 2020) ABSTRACT A practice-oriented modal superposition method for setting elastic floor acceleration response spectra is proposed in this paper. The approach builds on previous contributions in the literature, making specific recommendations to explicitly consider floor displacement response spectra and accounts for uncertainty in modal characteristics. The method aims to provide reliable predictions which improve on existing code methods but maintain simplicity to enable adoption in practical design. This work is motivated by recent seismic events which have illustrated the significant costs that can be incurred following damage to secondary and nonstructural components within buildings, even where the structural system has performed well. This has prompted increased attention to the seismic performance of nonstructural components with questions being raised about the accuracy of design floor acceleration response spectra used in practice. By comparing floor acceleration response spectra predicted by the proposed method with those recorded from instrumented buildings in New Zealand, it is shown that the proposed approach performs well, particularly if a good estimate of the building’s fundamental period of vibration is available. INTRODUCTION The objective of this work is to develop a practice-oriented prediction method that is suitable for the definition of both floor acceleration response spectra and floor displacement response spectra. The scope of this work is currently limited to structural systems that respond elastically. The proposed method is based on the concept of modal superposition. Modifications are made to the amplification factor shape proposed by Kehoe and Hachem [1] as adopted in ASCE 7-16 [2], with further work building on the proposals by Calvi and Sullivan [3], and Welch and Sullivan [4]. The method developed was verified against data recorded by instrumented buildings in New Zealand from the GeoNet Structural Array [5]. This work is motivated by the recognition by the earthquake engineering industry that despite decades of improvement in the seismic design of buildings, the damage and disruption caused by earthquakes remains high [6; 7]. The losses associated with damage to nonstructural components are recognised to be par- ticularly high, causing disruption and posing a safety hazard to occupants [8]. Significant losses incurred by nonstructural components have at times attracted scrutiny over the future of otherwise repairable structures [6]. In a broader context, poor seismic performance of nonstructural components does not fall solely with the inability to predict de- sign accelerations. Instead, the poor performance may be due to a lack of bracing, failure to follow standards, or lack of con- sideration. Baird and Ferner [9] found that many components that failed in the Kaik ¯ oura earthquake were not braced at all, and those that were performed well. Ferner et al. [10] found that in New Zealand the responsibility for the seismic design and con- struction of bracing for nonstructural components is typically not within the scope of project engineers, instead falling to those with limited familiarity with seismic requirements such as contractors, architects, and service engineers. Poor consideration may be due in part to building consent authorities often not requiring specific seismic design or construction review producer statements. Ap- plied Technology Council [11] found similar issues in the USA. This paper acknowledges that a holistic approach to the seismic performance of nonstructural components is required. Further, an aim of this research is to produce a method for predicting de- sign accelerations which is able to be used by those with limited knowledge on the structural properties of the structure. Reliable seismic design of nonstructural components is impeded by the difficulty in accurately predicting the acceleration and displacement demands imposed on them. These demands can be estimated using either empirical floor acceleration response spectrum prediction equations or advanced dynamic analyses. Current methods for defining floor acceleration response spectra in design standards, however, have been seen to be inaccurate [7; 12; 13], posing the need for improved code provisions. Recently proposed floor acceleration response spectrum predic- tion methods have generally focussed on modal response spec- tral analyses. Several studies have developed procedures (e.g., [1; 3; 4; 14]) which were verified against numerical simulations. The focus of previous work has been predominantly on floor acceleration response spectra, with the notable exception of the work by Calvi [15] on floor displacement response spectra. This paper is differentiated through its consideration of both floor acceleration response spectra and floor displacement response spectra, its verification against instrumented structure data, and through its aim to enable simple use by practicing engineers. 1 Corresponding Author, Student, University of Canterbury, Christchurch, [email protected] (Member) 2 Professor, University of Canterbury, Christchurch, [email protected] (Member) 3 Lecturer, University of Canterbury, Christchurch, [email protected] (Member)

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Page 1: A PRACTICE-ORIENTED METHOD FOR ESTIMATING ELASTIC … · Kieran Haymes1, Timothy J. Sullivan2 and Reagan Chandramohan3 (Submitted November 2019; Reviewed December 2019; Accepted March

116

Bulletin of the New Zealand Society for Earthquake Engineering, Vol. 53, No. 3, September 2020

A PRACTICE-ORIENTED METHOD FOR ESTIMATINGELASTIC FLOOR RESPONSE SPECTRA

Kieran Haymes1, Timothy J. Sullivan2 and ReaganChandramohan3

(Submitted November 2019; Reviewed December 2019; Accepted March 2020)

ABSTRACT

A practice-oriented modal superposition method for setting elastic floor acceleration response spectra isproposed in this paper. The approach builds on previous contributions in the literature, making specificrecommendations to explicitly consider floor displacement response spectra and accounts for uncertaintyin modal characteristics. The method aims to provide reliable predictions which improve on existing codemethods but maintain simplicity to enable adoption in practical design. This work is motivated by recentseismic events which have illustrated the significant costs that can be incurred following damage to secondaryand nonstructural components within buildings, even where the structural system has performed well. Thishas prompted increased attention to the seismic performance of nonstructural components with questionsbeing raised about the accuracy of design floor acceleration response spectra used in practice. By comparingfloor acceleration response spectra predicted by the proposed method with those recorded from instrumentedbuildings in New Zealand, it is shown that the proposed approach performs well, particularly if a good estimateof the building’s fundamental period of vibration is available.

INTRODUCTION

The objective of this work is to develop a practice-orientedprediction method that is suitable for the definition of both flooracceleration response spectra and floor displacement responsespectra. The scope of this work is currently limited to structuralsystems that respond elastically. The proposed method is basedon the concept of modal superposition. Modifications are madeto the amplification factor shape proposed by Kehoe and Hachem[1] as adopted in ASCE 7-16 [2], with further work building onthe proposals by Calvi and Sullivan [3], and Welch and Sullivan[4]. The method developed was verified against data recordedby instrumented buildings in New Zealand from the GeoNetStructural Array [5].

This work is motivated by the recognition by the earthquakeengineering industry that despite decades of improvement in theseismic design of buildings, the damage and disruption causedby earthquakes remains high [6; 7]. The losses associated withdamage to nonstructural components are recognised to be par-ticularly high, causing disruption and posing a safety hazardto occupants [8]. Significant losses incurred by nonstructuralcomponents have at times attracted scrutiny over the future ofotherwise repairable structures [6].

In a broader context, poor seismic performance of nonstructuralcomponents does not fall solely with the inability to predict de-sign accelerations. Instead, the poor performance may be dueto a lack of bracing, failure to follow standards, or lack of con-sideration. Baird and Ferner [9] found that many componentsthat failed in the Kaikoura earthquake were not braced at all, andthose that were performed well. Ferner et al. [10] found that inNew Zealand the responsibility for the seismic design and con-struction of bracing for nonstructural components is typically notwithin the scope of project engineers, instead falling to those with

limited familiarity with seismic requirements such as contractors,architects, and service engineers. Poor consideration may be duein part to building consent authorities often not requiring specificseismic design or construction review producer statements. Ap-plied Technology Council [11] found similar issues in the USA.This paper acknowledges that a holistic approach to the seismicperformance of nonstructural components is required. Further,an aim of this research is to produce a method for predicting de-sign accelerations which is able to be used by those with limitedknowledge on the structural properties of the structure.

Reliable seismic design of nonstructural components is impededby the difficulty in accurately predicting the acceleration anddisplacement demands imposed on them. These demands canbe estimated using either empirical floor acceleration responsespectrum prediction equations or advanced dynamic analyses.Current methods for defining floor acceleration response spectrain design standards, however, have been seen to be inaccurate[7; 12; 13], posing the need for improved code provisions.

Recently proposed floor acceleration response spectrum predic-tion methods have generally focussed on modal response spec-tral analyses. Several studies have developed procedures (e.g.,[1; 3; 4; 14]) which were verified against numerical simulations.The focus of previous work has been predominantly on flooracceleration response spectra, with the notable exception of thework by Calvi [15] on floor displacement response spectra. Thispaper is differentiated through its consideration of both flooracceleration response spectra and floor displacement responsespectra, its verification against instrumented structure data, andthrough its aim to enable simple use by practicing engineers.

1 Corresponding Author, Student, University of Canterbury, Christchurch, [email protected] (Member)2 Professor, University of Canterbury, Christchurch, [email protected] (Member)3 Lecturer, University of Canterbury, Christchurch, [email protected] (Member)

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117

(a) Mode shapes of the building.

Overview of the proposed method.

(a) Mode shapes of the building.

(b) Proposed floor spectrum.

m1

m2

2nd

mode shape

of building with

period T2 and

damping ξ2

NS component, period TNS and damping ξNS

Input ground acceleration

1st

mode shape of building with

period T1 and

damping ξ1

Peak acc.n of

floor due to

mode 1

Peak acc.n of

floor due to

mode 2

Spectrum

for ground

acceleration

Contribution

of mode 2 to

floor spectrum Contribution

of mode 1 to

floor spectrum

Total floor spectrum predicted

by using maximum of SRSS of

modal contribution & ground

spectrum demands

Acceleration

Period T 2 T1

(b) Proposed floor spectrum.

Figure 1: Overview of the proposed method.

PROPOSED FLOOR ACCELERATION RESPONSESPECTRUM PREDICTION METHOD

The floor acceleration response spectrum represents the peak ac-celeration demand imposed on a nonstructural element located ata floor as a function of its fundamental period of vibration, TNS.Figure 1 provides an overview of the method for constructingfloor acceleration response spectra proposed in this work. Thenew approach can be seen as an extension to the work proposedby Calvi and Sullivan [3], and Welch and Sullivan [4]. Theapproach uses the mode shapes and periods of the building (Fig-ure 1(a)) to first compute the peak floor acceleration demandsfor each mode. Subsequently, dynamic amplification factors thatdepend on the damping ratio of the nonstructural componentand the ratio of the nonstructural element fundamental period toeach building period are used to establish the contributions ofdifferent modes to the total floor acceleration response spectrum(Figure 1(b)). Finally, the predicted floor acceleration responsespectrum is taken as the maximum spectral acceleration consid-ering the acceleration response spectrum at the ground and thesquare-root-sum-of-squares (SRSS) of all of the modal contribu-tions at each nonstructural period, TNS. To assist in more easilyestimating the parameters required, a number of assumptionsand simplifications can be made, as further discussed below.

Modal Contribution Equation

In the prediction method, the contribution of mode i, at floorj, to the floor acceleration response spectrum at the period ofvibration of the nonstructural component, TNS, is computed usingEquation 1:

SFA,i, j(TNS,ξNS) = |Γiφi, j|SGA(Ti,ξstr)DAF(rT,i) (1)

where Γi is the participation factor of mode i;φi, j is the modal shape coordinate of mode i, at floor j;SGA(Ti,ξstr) is the ground acceleration response spectral ordi-nate corresponding to the period of vibration of mode i, scaledto the damping of the structure, ξstr, of 5%; andDAF(rT,i) is the Dynamic Amplification Factor used to describethe resonant behaviour between the fundamental mode of vibra-tion of the nonstructural element, TNS, and mode of vibration iof the building, Ti.

Equation 1 follows the form of previous methods, where the peakfloor acceleration, Γiφi, jSGA(Ti,ξstr), is multiplied by a factoraccounting for resonance between the nonstructural componentand the building, the dynamic amplification factor DAF [1; 2; 4;7; 14].

The appendix of this paper provides values for approximateparticipation factors and modal coordinates that could be used inlieu of results from accurate eigenvalue analysis.

Dynamic Amplification Factor

The phenomenon that most governs the shape of the floor accel-eration response spectrum is resonance between the modes ofvibration of the structure and the fundamental mode of vibrationof the nonstructural component. Where the fundamental periodof vibration of the nonstructural element, TNS, is close to thatof any mode, i, of the building, Ti, dynamic amplification is ex-pected. To represent this amplification a term is used called theDynamic Amplification Factor, DAF . This factor is a functionof the ratio of the nonstructural component’s fundamental periodof vibration to the building’s period of vibration of mode i, rT,i,given by Equation 2.

rT,i =TNS

Ti(2)

At low period ratios, where the nonstructural component is rigid,there is no dynamic amplification and the acceleration demand isthe same as the peak floor acceleration. Near resonance betweenthe modes of vibration of the structure and the fundamental modeof vibration of the nonstructural component the dynamic amplifi-cation tends upwards towards a peak at rT,i = 1. Beyond this, thecomponent is more flexible and the shape decays towards zero.

In this work DAF is modelled as a piecewise function, shown inFigure 2, similar to that defined in the “Alternate Floor ResponseSpectra” approach in ASCE 7-16 [2]. The shape of DAF) hasbeen modified in this work to have a more narrow amplificationpeak in the rT,i range between rT,A to rT,D where DAF > 1. Thiswas based on empirical trial and error of the prediction methodverified against the instrumented building records discussed laterin this paper. At period ratios beyond the amplification peakDAF was modified from the value of 1 used in ASCE 7-16[2] to a decay towards zero to more accurately represent theshape observed when a floor acceleration response spectrum isintegrated into a floor displacement response spectrum.

As seen in Figure 2, DAF involves a maximum dynamic amplifi-cation factor term, DAFmax which varies the peak amplification. This is set as a function of the damping of the nonstructuralcomponent, ξNS (hereinafter called "nonstructural damping") toaccount for the increased amplification in response expected inless-damped components. There is support in the literature forincluding DAFmax values for a range of nonstructural dampingvalues back to early contributions to this research [16]. Kehoeand Hachem [1] provide DAFmax at 2% nonstructural damping,while ASCE 7-16 uses DAFmax set at 5. The method proposedhere uses the maximum dynamic amplification expression ofWelch and Sullivan [4], which is dependent on both structuraland nonstructural damping, ξ str and ξNS, respectively. Includ-ing provision for ξstr aims to predict the increased dynamicamplification observed for buildings which provide lower struc-

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118

Figure 2: Dynamic Amplification Factor used to compute thecontribution of a given mode of vibration of the building to

the floor acceleration response spectrum.

tural damping, such as steel frame buildings. It is this thereforethis equation that is recommended for use by practitioners. Inthis paper it is assumed that the predominantly-concrete instru-mented buildings can be characterised by 5% damping. Therecommended expression is given in Equation 3:

DAFmax = [0.5ξstr +ξNS]−2/3 (3)

These expressions were empirically derived [4; 7] where thedynamic amplification was assessed from floor acceleration re-sponse spectra computed from nonlinear time history analysesfor a set of ground motions. It should be noted that the accuracyof the proposed method is limited by the significant record-to-record variation in dynamic amplification that was observed inprevious studies [4; 11], showing uncertainty in the amplificationexpected.

The shape of DAF is defined by a piecewise function boundby limits defined by period ratios rT,A to rT,D. Where rT,i is0, the component is rigid and moves with the floor, thus theDAF(rT,i = 0) value of 1 reflects the peak floor accelerationgiven by Γiφi, jSGA(Ti,ξstr). The ranges rT,A to rT,B and rT,C torT,D are linear from a value of 1 to the peak amplification valueplateau between rT,B and rT,C, following the shape given inASCE 7-16 [2]. A decay curve for DAF(rT,i > rT,D) is proposedto provide more accurate floor velocity response spectra and floordisplacement response spectra when the acceleration spectrum isconverted, as discussed further in a later section titled Conversionto Displacement and Velocity Spectra. The DAF function shownin Figure 2 can be described in equation form as:

DAF =

1 rT,i ≤ rT,ArT,i−rT,ArT,B−rT,A

(DAFmax−1)+1 rT,A < rT,i < rT,B

DAFmax rT,B ≤ rT,i ≤ rT,CrT,i−rT,CrT,D−rT,C

(1−DAFmax)+DAFmax rT,C < rT,i <T,D1

((1−rT,D)+rT,i)2 rT,D ≤ rT,i

(4)

The values of rT,A to rT,D define the width of the DAF shape.Broad ranges of period ratios are recommended considering theuncertainty in the periods of vibration of the supporting structureand the fundamental period of the nonstructural element. Theamplification peaks in elastic floor acceleration response spectraare often narrow, however, and the use of broad values, such asthose prescribed by ASCE 7-16, could be conservative. Thiswork attempts to find a balance by retaining a broad plateauat DAFmax while narrowing the period ratios used in ASCE 7-16. The period ratios adopted in this work are compared withthose from ASCE 7-16 in Table 1. As will be shown later, thevalues shown in Table 1 were found to provide reasonably good

estimates. Where there is only low certainty in the prediction ofthe periods of vibration of the structure, broader peaks wouldbe required. Optimising these period ratio values to vary basedupon the certainty of simplified approaches could be an area forfurther research.

Table 1: Period ratios used to define DAF shape.

Peak Width rT,A rT,B rT,C rT,D

ASCE 7-16 0.5 0.75 1.25 2.0

Adopted 0.6 0.8 1.2 1.6

Combination of Modal Contributions

The floor acceleration response spectrum at the floor level j,SFA, j, is defined by taking the maximum value of theSRSS combination of the modal acceleration contributionscomputed using Equation 1, at each nonstructural period,SFA,i, j(TNS,ξNS), and the ground acceleration response spectrum(GRS), SGA(TNS,ξNS), as given by Equation 5:

SFA, j = max

[√∑

iSFA,i, j(TNS,ξNS)

2,SGA(TNS,ξNS)

](5)

This is illustrated in Figure 3, where each of the modal contri-butions, ground acceleration response spectrum, and combinedfloor acceleration response spectrum are shown. A minimumof three modes in each fundamental direction is recommended,where fourth and fifth modes should be considered for build-ings with long fundamental periods [1; 2]. It is common thatnonstructural components can be thought of as rigid where thenonstructural component period less than 0.06 s [17]. It is there-fore recommended that structural modes with periods below0.06 s do not need to be considered.

Taking the SRSS of modal contributions has been widely pro-posed [3; 4; 14]. This was adopted herein instead of the maxi-mum of each contribution, as used in Kehoe and Hachem andASCE 7-16 [1; 2], as it provided better peak floor accelerationpredictions for structures with significant higher mode contri-butions. This approach is thought to balance better predictionswith simplicity, contrasted to taking the maximums of the con-tributions or using the complete-quadratic-combination (CQC)method [3; 14].

Taking the maximum of combined modes and the ground accel-eration response spectrum has been widely adopted [1–4]. Theuse of the ground response spectrum is supported by the notionof rigid body motion discussed in Pozzi and Der Kiureghian[18], where it was observed that lower levels of the structure donot filter the ground acceleration response spectrum as upperlevels do, retaining the same spectral shape. There is some evi-dence in the floor acceleration response spectra computed fromthe instrumented building records that even at upper levels theground acceleration response spectrum demands are still presentdue to rigid body motion of the building. For simplicity, themaximum of the ground acceleration response spectrum and themodal contributions are taken for any floor, j, in the building.

Nonstructural Component Damping

Several studies have recognised the importance of incorporatingthe influence of damping of the nonstructural component, ξNS,into floor acceleration response spectrum prediction methods[3; 4; 7; 11; 14]. Significant amplification of the modal peaks

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119

0

0.1

0.2

0.3

0.4

0 0.5 1 1.5 2

Acc

eler

atio

n,

SFA(T

NS,

5%

) (g

)

Component period, TNS (s)

Mode 1

Mode 2

Mode 3

GRS

Prediction

Figure 3: Combination of modal contributions of modes 1,2,and 3, with the ground acceleration response spectrum (GRS)to determine floor acceleration spectrum at floor 4 of the UCPhysics building for the longitudinal direction in the M4.8

October 2010 earthquake.

within the response spectra at lower damping values has beenrepeatedly observed.

Quantifying the nonstructural damping without testing poses achallenge for design. Empirical data has been gathered throughrelatively simple testing using accelerometers and impact ham-mers [19]. Despite this, the research on nonstructural damping isstill sparse for many components, particularly at the high inten-sities of design interest where damping is assumed to be greater[11]. Rigid components, such as machinery, are likely to havelow damping and, therefore, the assumption of a nonstructuraldamping ratio of 5% would lead to under-prediction of the flooracceleration response spectrum demands.The work presented inthis paper uses nonstructural damping ratios, ξNS, of 2% and5%. Further research into component damping is proposed forgreater confidence in the use of floor spectra as a design basis.

Two ground acceleration response spectra are required to predictfloor acceleration response spectrum using the proposed method,one of which is the site-specific ground acceleration responsespectrum scaled to the damping of the structure, SGA(T,ξstr).As noted earlier, ξstr = 5% is used for all modes to maintainsimplicity, as this is a common assumption for many buildings.This spectrum corresponds to the unscaled design ground accel-eration response spectrum specified in codes such as NZS1170.5[20]. This recommendation follows the conclusion by ATC thatdamping of the structure does not play a large role in componentresponse [11]. This spectrum is used to assess the spectral ac-celeration of each of the modes, SGA(Ti,ξstr) which is used tocreate the peak floor acceleration in Equation 1.

The second spectrum required is the site-specific ground accel-eration response spectrum scaled to the damping of the non-structural component, SGA(TNS,ξNS) used in Equation 5. Thiscorresponds to the amplification expected from the componentresponding to the rigid body motion of the building not filteringthe ground acceleration response spectrum. This is assessedby multiplying the 5%-damped design ground response spec-trum by a scaling factor, η . Several empirical expressions forη exist, such as that given in Equation 6 from Eurocode 8 [21],where ξ is the nonstructural damping value of interest, given asa percentage.

η =

√10

5+ξ≥ 0.55 (6)

If the floor acceleration response spectrum is required for a spe-cific earthquake ground motion, ground acceleration responsespectra should be produced at both at 5% structural damping andat the nonstructural damping level of interest as required. Thiswas undertaken in this work for the verification of the predic-tion method using the records from instrumented structures, as

discussed later in this paper.

Nonstructural Component Period

The period of the nonstructural component, TNS, is the dependantvariable for assessing demands using floor response spectra. Non-structural components are assumed to be simple single-degree-of-freedom (SDOF) oscillators with a vibrational period, thoughthis may not always be valid. Components themselves can becomplex and may have complex interactions with bracing andsupports. The commentary to NZS1170.5 [20] recommends test-ing or analysis of the component to establish the period. Kehoe[17] notes, however, that this is rarely the case in practice dueto these complexities. Further, as discussed by Kehoe [17], thevibration characteristics of components found through testingonly represents a small fraction of available components. Non-structural period elongation may also occur due to softening,which risks lengthening the period into resonant behaviour withthe structural modes. The influence of this on the floor responsespectrum, as well as the associated ductile response of the com-ponent, is beyond the scope of this work and is a possible areaof future research.

In this work, floor response spectra are generated which accountfor uncertainty in the fundamental period of the structure, T1,but not the component period, TNS. This results in floor accelera-tion response spectra with peaks and troughs over small periodintervals. It is cautioned that over-prescription of the componentperiod to capture troughs may result in unrealistic predictionsof design accelerations. It is therefore recommended that thefloor response spectra generated using this proposed method isused with cautious consideration of uncertainty of the compo-nent period. There is an opportunity for further work to refinethis method to avoid these potential issues.

Conversion to Displacement and Velocity Spectra

Displacement or velocity sensitive components may be designedusing elastic floor response spectral analysis. This work makesexplicit consideration to the derivation of these spectra from thefloor acceleration response spectrum prediction. To convert froma floor acceleration response spectrum at floor j, given in abso-lute acceleration as SFA, j , to a floor velocity response spectrum,SFV, j or a floor displacement response spectrum SFD, j, givenrelative to the floor, Equations 7 and 8 are used, respectively.

SFV, j =SFA, jTNS

2π(7)

SFD, j =SFA, jTNS

2

4π2 (8)

The amplification shape for any given mode, i, in a floor velocityresponse spectrum, SFV,i, j, and a floor displacement responsespectrum, SFD,i, j, can be seen in Figure 4, where the spectraare normalised by a unit value of peak floor acceleration (PFA).This aims to closely match the spectral shapes observed fromrecorded floor velocity response spectra and floor displacementresponse spectra.

Recommendations Aimed at Maintaining a Simplified Ap-proach

Given that the approach requires characterisation of variousmodal parameters, efforts are made to enable easy practical useof the approach through simplified mode shape and buildingperiod estimates.

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(a) PFA-normalised velocity spectrum for mode i.

(b) PFA-normalised displacement spectrum for mode i.

Figure 4: Modal components of the velocity and displacement spectra generated by a unit value for peak floor acceleration (PFA).

Fundamental Period of Vibration of the Building

The fundamental period of vibration of the building in the direc-tion of interest, T1, is a key parameter in the determination offloor acceleration response spectra. Significant dynamic amplifi-cation of acceleration, velocity, and displacement floor responsespectra around the fundamental period of vibration has beenwidely observed [3; 11]. Accurate estimation of the fundamentalperiod of vibration is important to obtain accurate predictionswith any method that uses modal superposition to predict flooracceleration response spectra. It is recognised that there is uncer-tainty in estimating T1. It is the intention that this uncertainty iscaptured by the broadness of the plateau at the maximum valueof the dynamic amplification factor (DAF), as shown in Figure 2.

Simplified methods for determining T1 would help to enableeasy use of the proposed method. A means for this may bethe empirical approaches for estimating T1 that are available inmany codes, such as the commentary of NZS1170.5 [20], ASCE7-16 [2], and Eurocode 8 [21]. These empirical methods usethe structural typology of the lateral force resisting system andthe total height of the structure. The potential impact of usingthese methods will be reviewed herein with reference to the flooracceleration response spectra of instrumented structures.

Higher Modes of Vibration

It has been observed from numerical models and instrumentedstructures that responses of higher modes of vibration of a build-ing (hereinafter called "higher modes") can make considerablecontributions to the demands described by a floor accelerationresponse spectrum [3; 4; 7; 13; 14; 22]. There is value in generat-ing more accurate predictions for the higher mode periods, THM ,as this changes the placement along the x-axis of the high modecontributions to the floor acceleration response spectrum and theground acceleration response spectral ordinate, SGA(THM ,ξstr).Better period estimations will directly decrease the uncertaintyof floor spectrum predictions in the shorter period range. Thiseffect is most pronounced in floor acceleration response spectraas floor displacement response spectra are often dominated bythe response of the fundamental mode [15].

It is recommended that values for higher mode periods fromeigenvalue analysis be used where available. In this work, valuesfor higher mode periods, THM , were determined for each direc-tion of the instrumented buildings by multiplying the fundamen-tal period of vibration, T1, assessed using frequency responsefunctions, with standard ratios for THM/T1 defined for givenlateral force resisting typologies, as given in Table 2. Thesewere used to investigate the sensitivity of the floor accelerationresponse spectra predictions to simplified approaches.

Table 2: Simplified higher mode ratios used for a simplifiedimplementation of the prediction method.

Typology T2/T1 T3/T1

Wall 1/5 1/10

Frame 1/3 1/6

The contribution of mode i, at floor j, to the floor accelerationresponse spectrum, given by Equation 1, involves using theproduct of the modal participation factor and mode shape, Γi φi, j .It is recommended that values for modal participation factors andmode shapes from eigenvalue analysis be used where available.

It was found in this study that the accuracy of the mode shapedoes not make a significant contribution to the accuracy of thefloor acceleration response spectrum. The simplified approachin Miranda and Taghavi [23] is therefore recommended in lieu ofmodal analysis results, where the typology of the lateral force re-sisting structure in the direction of interest is the only parameter,assuming constant lateral stiffness at all building heights. In thiswork, values for the dimensionless parameter α0 which controlsthe degree of participation of overall flexural and overall sheardeformations in Miranda and Taghavi [23] were taken as 12.5 formoment resisting frame structures and 1.25 for shear wall struc-tures corresponding to the average value for these typologiesgiven in their work.

The participation factor for each mode i, Γi, can be computedusing Equation 9:

Γi =Φi

T [M]

ΦiT [M]Φi

(9)

where Φi = mode shape vector for mode i at all floors; andM = global mass matrix.This may be further simplified where the masses of the floorscan be assumed to approximately equal, as was assumed in thiswork, to reduce to Equation 10:

Γi =∑φi, j

∑φi, j2 (10)

where φi, j is the mode shape of mode i at floor j.

To enable easy adoption of the method outlined in this paper,values for the mode shapes and participation factors for modes1, 2, and 3 at each floor for structures between 1 and 20 storeys,along with the corresponding participation factors, are given inAppendix A. These values were computed using the methodproposed in Miranda and Taghavi [23] with an α0 value of 3.125.

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This corresponds to the average for dual moment resisting frameand wall structures which is thought to be sufficiently represen-tative of typical building structures for the use of this simplifiedmethod.

Floor Diaphragm Flexibility and Torsion

The floor and roof diaphragms were assumed to be rigid. Varia-tion of demands due to diaphragm flexibility is assumed negligi-ble and thus the predictions generated using the proposed methoddo not vary horizontally across the floor. ATC [11] (amongst oth-ers) report that significant amplification can be produced at themidspan of flexible diaphragms, and at the perimeter of torsion-ally sensitive structures with rigid diaphragms. However, theyconcluded that the complexity required in a prediction methodto account for this is beyond the scope of a simplified method.Likewise, building irregularities were deemed too complex tomodel using a simplified method, and should be accounted forusing a more rigorous method such as time-history analysis.

VALIDATION OF THE PREDICTION METHOD USINGOBSERVED DATA

To validate the performance of the proposed method, floor accel-eration response spectra and floor displacement response spec-tra were predicted and compared with data from instrumentedbuildings in New Zealand recorded in recent earthquakes. Thebuildings identified for this purpose form part of the GeoNetStructural Array [5]. The structures examined in this researchare the two seismically-separated Avalon GNS buildings (Units 1and 2), the BNZ CentrePort Harbour Quays building, the Univer-sity of Canterbury Physics (UC Physics) building, and the MBIEStout St building, a summary of which can be seen in Table3. In each building the longitudinal and transverse responseswere recorded at each instrumented floor by triaxial accelerome-ters. Further information on the instrumentation can be found atGeoNet [5].

The UC Physics building recorded motions from the 2010/2011Canterbury earthquake sequence (M4.7 to M6.3), where minorcracking of the concrete structure was observed [24]. The GNSand BNZ buildings recorded motions in the 2013 Seddon (M6.5)and Grassmere (M6.6) earthquakes. In these events significantnonstructural damage was observed in the BNZ building [25].The 2016 M7.8 Kaikoura earthquake motions were recordedby the GNS, MBIE and BNZ buildings. The BNZ buildingexperienced structural damage in this earthquake and is beingdemolished at the time of this paper. All other buildings areassumed to have remained within the elastic range. All mo-tions examined in this work are from earthquakes with far-fieldepicentres.

The intensity of the events examined can be contextualised withthe 5% damped ground acceleration response spectra in the lon-gitudinal and transverse axes of the buildings used are plotted

in Figure 5. The fundamental periods in each of the orthogonaldirections, taken as the mean from the values inferred from thefrequency response functions (discussed below) are identifiedin the figure. The 500-year return period Ultimate Limit State(ULS) and 25-year return period Serviceability Limit State (SLS)intensity design ground acceleration response spectra are alsoplotted in Figure 5, as prescribed in NZS1170.5:2004 [20] andNZS1170.0:2002 [26] assuming a 50-year design life at impor-tance level 2. It should be noted that all buildings except theBNZ CentrePort building were designed prior to current stan-dards, which came into effect in 2004, and thus these spectra areprovided merely for context. The intensities of the events experi-enced by the UC Physics and Avalon GNS buildings appear tobe approximately at or below the SLS intensity level. The MBIEStout St building experienced shaking above SLS intensity andbelow ULS intensity. In the Kaikoura 2016 earthquake the BNZbuilding experienced shaking similar to ULS intensity.

Processing of Accelerometer Data

Accelerograms were downloaded from the GeoNet server andextracted into the recorded x, y and z directions. The records inthe horizontal directions were reoriented from the recorded ori-entation of the instruments to longitudinal and transverse axes ofthe building. Any static offsets in the recordings were removed.The accelerograms were zero-padded and filtered using acausalfourth-order Butterworth filters with corner frequencies of 0.1 Hzand 20 Hz, following the procedure employed by Chandramohanet al. [25].

One accelerogram for each orthogonal direction was calculatedper floor in each event. To infer responses at points across thefloor it was assumed that the floors behaved as rigid diaphragms.At a floor where three linearly independent measurements wererecorded, the torsional response of the building was calculatedand removed from the longitudinal and transverse accelerograms.At a floor where only two linearly independent recordings wereavailable, the longitudinal and transverse accelerograms weretaken directly from the processed measurements. Where thenumber of linearly independent measurements exceeded three,however, the system was overdefined, and a least squares ap-proach was required. The least squares approach was used forthe UC Physics and Avalon GNS buildings to compute recordsat the geometric centre of the floor. Accelerometers on the south-west wall of BNZ building were used, where the longitudinal andtransverse floor records were taken directly from the processedaccelerograms and the torsional response was neglected due tothe sparsity of instrumentation.

Assessment of Structural Properties

Fundamental periods of vibration in each horizontal directionwere inferred from peaks in frequency response functions, com-puted as the ratio of the Fourier amplitude spectrum at eachinstrumented storey to the Fourier amplitude spectrum at the

Table 3: Overview of GeoNet instrumented buildings used as case studies.

Building Location Storeys Lateral load resisting sytem Yearbuilt

Yearinstr.ed

Floorsinstr.ed

Instrumentsavailable

UC Physics Christchurch 8 Coupled RC shear walls 1961 2007 3 10

Avalon GNS U1 Lower Hutt 3 RC MRF 1973 2007 1 4

Avalon GNS U2 Lower Hutt 3 RC MRF 1973 2007 2 5

BNZ CentrePort Wellington 5 RC MRF 2009 2009 5 14

MBIE Stout St Wellington 9 Concrete-encased steel MRF 1940 2014 9 16

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0

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0.6

0.8

1

1.2

1.4

0 0.5 1 1.5 2 2.5 3

SG

A(T

, 5

%)

(g)

T (s)

NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

22 Feb 2011 (Lyttelton)

13 Jun 2011a

13 Jun 2011b

Other events

T1 Longitudinal direction

(a) UC Physics – Longitudinal Direction.

0

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0.6

0.8

1

1.2

1.4

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SG

A(T

, 5

%)

(g)

T (s)

NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

22 Feb 2011 (Lyttelton)

13 Jun 2011b

23 Dec 2011bOther events

T1 Transverse direction

(b) UC Physics – Transverse Direction.

0

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0.6

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1

1.2

1.4

0 0.5 1 1.5 2 2.5 3

SG

A(T

, 5

%)

(g)

T (s)

NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

L - Seddon

L - Grassmere

L - Kaikōura

T1 Longitudinal direction

(c) Avalon GNS Unit 1 – Longitudinal Direction.

0

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0.6

0.8

1

1.2

1.4

0 0.5 1 1.5 2 2.5 3

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A(T

, 5

%)

(g)

T (s)

NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

T - Seddon

T - Grassmere

T - Kaikōura

T1 Transverse direction

(d) Avalon GNS Unit 1 – Transverse Direction.

0

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1

1.2

1.4

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A(T

, 5

%)

(g)

T (s)

NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

L - Seddon

L - Grassmere

L - Kaikōura

T1 Longitudinal direction

(e) Avalon GNS Unit 2 – Longitudinal Direction.

0

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0.6

0.8

1

1.2

1.4

0 0.5 1 1.5 2 2.5 3

SG

A(T

, 5

%)

(g)

T (s)

NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

T - Seddon

T - Grassmere

T - Kaikōura

T1 Transverse direction

(f) Avalon GNS Unit 2 – Transverse Direction.

0

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1

1.2

1.4

0 0.5 1 1.5 2 2.5 3

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A(T

, 5

%)

(g)

T (s)

NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

L - Seddon

L - Grassmere

L - Kaikōura

T1 Longitudinal direction

(g) BNZ CentrePort – Longitudinal Direction.

0

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1

1.2

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A(T

, 5

%)

(g)

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NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

T - Seddon

T - Grassmere

T - Kaikōura

T1 Transverse direction

(h) BNZ CentrePort – Transverse Direction.

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, 5

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NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

L - Kaikōura

T1 Longitudinal direction

(i) MBIE Stout St – Longitudinal Direction.

0

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A(T

, 5

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NZS1170.5:2004, 500 yr

NZS1170.5:2004, 25 yr

T - Kaikōura

T1 Transverse direction

(j) MBIE Stout St – Transverse Direction.

Figure 5: Acceleration response spectra from accelerograms recorded at ground level of the instrumented buildings.

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Table 4: Fundamental periods (s) in orthogonal directions in events studied, as inferred from frequency response functions.

UC Physics Avalon GNS U1 Avalon GNS U2 BNZ CentrePort MBIE Stout St

Event Long Trans Long Trans Long Trans Long Trans Long Trans

M4.8 - 19 Oct 2010 0.41 0.56 - - - - - - - -

M4.7 - 26 Dec 2010 0.39 0.58 - - - - - - - -

M6.3 - 22 Feb 2011 (Lyttelton) 0.46 0.63 - - - - - - - -

M5.0 - 16 Apr 2011 0.41 0.55 - - - - - - - -

M5.3 - 13 Jun 2011a 0.47 0.58 - - - - - - - -

M6.0 - 13 Jun 2011b 0.46 0.59 - - - - - - - -

M4.9 - 09 Oct 2011 0.40 0.59 - - - - - - - -

M5.8 - 23 Dec 2011a 0.45 0.61 - - - - - - - -

M5.9 - 23 Dec 2011b 0.44 0.63 - - - - - - - -

M6.5 - 21 Jul 2013 (Seddon) - - 0.34 0.39 0.32 0.37 1.00 1.10 - -

M6.6 - 16 Aug 2013 (Grassmere) - - 0.33 0.40 0.32 0.37 1.30 1.20 - -

M7.8 - 14 Nov 2016 (Kaikoura) - - 0.35 0.39 0.34 0.39 1.50 1.40 0.75 0.80

ground. This is illustrated in Figure 6 where the roof motionsof the Avalon GNS Unit 2 building from the 2013 M6.5 Sed-don earthquake were used, and the peak corresponding to thefundamental mode of vibration is identified. A summary of thefundamental periods inferred is presented in Table 4.

The ground spectral accelerations were computed for each mode,SGA(Ti,ξstr), from the ground acceleration response spectrumrecorded at the ground level in each orthogonal direction. Thisis illustrated in Figure 7 using the Avalon GNS Unit 2 build-ing ground acceleration response spectra from the 2013 M6.5Seddon earthquake, where each of the periods of vibration areindicated.

COMPARISON OF OBSERVED AND PREDICTEDFLOOR RESPONSE SPECTRA

A floor acceleration response spectrum was computed in thelongitudinal and transverse directions at each floor where datawas available. This was done by stepping through the accelero-gram processed in one orthogonal direction at a floor, solving theequation of motion for series of SDOF oscillators with differentperiods with a given nonstructural damping value, and taking themaximum acceleration responses.

The floor acceleration response spectra examined herein have

similar characteristics and are thought to be representative ofthe form of most floor acceleration response spectra. At verylow periods, below 0.1 s, the spectral acceleration approachesthe peak floor acceleration of the structure. Above 0.1 s, peaksin spectral acceleration from superposition of modes can beobserved around the periods of vibration of the structure. Atplaces the floor acceleration response spectrum is similar to theground acceleration response spectrum due to rigid body motionof the structure. This often dominates the floor accelerationresponse spectrum beyond the peak due to the fundamental modeof vibration of the structure, which is best observed in a floordisplacement response spectrum.

The performance of the prediction method is assessed throughcomparison of the observed spectra to those predicted using therecorded ground acceleration response spectra. To illustrate this,Figure 8 compares the floor acceleration response spectra andfloor displacement response spectra predicted and recorded inthe MBIE Stout St building during the M7.8 Kaikoura 2016earthquake. This figure shows the floor acceleration responsespectra and floor displacement response spectra in the longitudi-nal direction at floors 1, 3, 6, and 9, at 2% and 5% nonstructuraldamping. Ground acceleration and displacement response spec-tra in the longitudinal direction are also plotted at 2% and 5%nonstructural damping.

0.1

1

10

100

0.01 0.1 1 10

FR

F

T (s)

T1

(a) Longitudinal Direction.

0.1

1

10

100

0.01 0.1 1 10

FR

F

T (s)

T1

(b) Transverse Direction.

M6.5 2013 Seddon

M6.6 2013 Grassmere

M7.8 2016 Kaikoura

Figure 6: Frequency response functions (FRF) computed from the Avalon GNS Unit 2 building’s roof motions from the 2013Seddon, 2013 Grassmere, and 2016 Kaikoura earthquake records with the fundamental period in the longitudinal and transverse

directions inferred from peaks.

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0

0.05

0.1

0.15

0.2

0 0.5 1 1.5 2 2.5 3

SG

A(T

, 5%

) (g

)

T (s)

GRS

Mode 1

Mode 2

Mode 3

(a) Longitudinal Direction.

0

0.05

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0.15

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0 0.5 1 1.5 2 2.5 3

SG

A(T

, 5%

) (g

)

T (s)

GRS

Mode 1

Mode 2

Mode 3

(b) Transverse Direction.

Figure 7: Input SGA(Ti) values found for the first three modes of the Avalon GNS Unit 2 building from the ground response spectra(GRS) recorded in the 2013 Seddon earthquake.

Table 5: Comparison between values for the fundamental period of vibration, T1, given by the commentary of NZS1170.5 and bythe frequency response function, FRF, where the structure performs at or below the serviceability limit state intensity, SLS, as

given in NZS1170.0.

Longitudinal Transverse

Building NZS1170.5Simplified

AverageElastic FRF

NZS1170.5Simplified

AverageElastic FRF

UC Physics T1 = 0.65 s T1 = 0.42 s T1 = 0.65 s T1 = 0.60 s

Avalon GNS Unit 1 T1 = 0.44 s T1 = 0.34 s T1 = 0.44 s T1 = 0.39 s

Avalon GNS Unit 2 T1 = 0.44 s T1 = 0.33 s T1 = 0.44 s T1 = 0.38 s

BNZ CentrePort T1 = 0.80 s T1 = 1.00 s T1 = 0.80 s T1 = 1.10 s

MBIE Stout St T1 = 1.04 s T1 = 0.75 s T1 = 1.04 s T1 = 0.85 s

Figure 8 shows that the proposed method provides floor acceler-ation response spectra and floor displacement response spectrapredictions that are similar to those observed from the instru-mented floor records. The position of the prediction modal con-tributions are close to the periods of the observed correspondingpeaks. The predicted spectral acceleration of the fundamentalmode contribution was similar to that in the observed spectra, al-though the predicted spectral acceleration of higher mode contri-butions was not. At long periods, greater than 2 s, the predictionclosely matches the observed data, as this is where rigid bodymotion dominates.

The influence of the mode shapes on floor acceleration responsespectra can be observed in the recorded spectra in Figure 8 bycomparing the peaks in spectral acceleration around the periodsof vibration of the structure at different floors. The mode shapeof the fundamental mode is observed by the significant increasein spectral acceleration with floor height between periods TNS= 0 s to 2 s. The influence of higher modes can be observedbetween approximately TNS = 0.1 s to 0.5 s. The shape of thesecond mode response is observed by comparing the floor ac-celeration response spectra at the period range of approximatelyTNS = 0.3 s to 0.5 s. The shape of the second mode implies thathigher spectral accelerations should be expected in this range atapproximately one-third of the building height and at the roof,with a lower amplitude at two-thirds of the building height. Thisis observed in the peaks in spectral acceleration in the floor ac-celeration response spectra of floors 3 and 9, and the absence ofthe peak in the floor acceleration response spectra of floor 6.

Recall that the proposed floor spectrum method makes explicitconsideration of the width of amplification peaks using the DAF

with the period ratios rT,A to rT,D. Examining the contribution ofthe fundamental mode to the floor acceleration response spectrain Figure 8, it appears the first regions of the DAF, the flat andlinear-increase shapes, fit well with the amplification observedfrom the recorded spectra. This implies rT,A and rT,B are welllocated. It can further be seen that the proposed plateau issufficiently broad enough to capture the peak intensity of theamplification of spectral acceleration due to the fundamentalmode. At periods greater than the fundamental period of thebuilding (between 1 s and 2 s) there is, however, significantamplification of spectral acceleration that is not well capturedby the prediction method. This may imply that rT,D should beat a longer period ratio to widen the linear decay shape if thisresponse corresponds to amplification due to the fundamentalmode. It may, however, be a torsional response that this work hasnot accounted for. This observation was not made in all cases,however. As seen later, Figure 10 shows that the width of theDAF defined by the period ratios used in this work predicts afloor acceleration response spectrum that fits well to the spectrumobserved at the roof level of the UC Physics building in theLyttelton earthquake. These observations evidence that furtherwork to define the period ratios may be required.

The floor acceleration response spectrum at floor 1 in Figure 8shows no signification variation from the ground accelerationresponse spectrum. This characterises the rigid body motion oflower levels in the building observed in prior studies [4; 18]. Thisobservation supports constructing the predicted floor accelerationresponse spectrum using the maximum of both the combinedmodal response and the ground acceleration response spectrum.

The influence of rigid body motion on floor acceleration response

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0

0.5

1

1.5

2

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0 1 2 3 4 5

SFA(T

NS)

(g)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(a) Acceleration FRS – Floor 9.

0

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0 1 2 3 4 5

SF

D(T

NS)

(m)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(b) Displacement FRS – Floor 9.

0

0.5

1

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2

2.5

3

0 1 2 3 4 5

SFA(T

NS)

(g)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(c) Acceleration FRS – Floor 6.

0

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0 1 2 3 4 5

SF

D(T

NS)

(m)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(d) Displacement FRS – Floor 6.

0

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2

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0 1 2 3 4 5

SFA(T

NS)

(g)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(e) Acceleration FRS – Floor 3.

0

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SF

D(T

NS)

(m)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(f) Displacement FRS – Floor 3.

0

0.5

1

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0 1 2 3 4 5

SFA(T

NS)

(g)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(g) Acceleration FRS – Floor 1.

0

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D(T

NS)

(m)

TNS (s)

Recorded - 2% Damp

Recorded - 5% Damp

Predicted - 2% Damp

Predicted - 5% Damp

(h) Displacement FRS – Floor 1.

0

0.5

1

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2

2.5

3

0 1 2 3 4 5

SG

A(T

) (g

)

T (s)

Recorded - 2% Damp

Recorded - 5% Damp

(i) Acceleration GRS – Ground.

0

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0 1 2 3 4 5

SG

D(T

) (m

)

T (s)

Recorded - 2% Damp

Recorded - 5% Damp

(j) Displacement GRS – Ground.

Figure 8: Recorded and predicted acceleration and displacement floor response spectra (FRS) for the MBIE Stout St building forthe Kaikoura 2016 earthquake in the longitudinal direction of floors 1, 3, 6, and 9, at 2% and 5% nonstructural component

damping. Ground acceleration and displacement response spectra (GRS) are also plotted at 2% and 5% nonstructural damping.

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0

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7

8

9

10

0 1 2 3 4 5

SFA(T

NS)

(g)

TNS (s)

Predicted - 2% Damp

Predicted - 5% Damp

(a) Acceleration FRS.

0

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0.4

0.6

0.8

1

1.2

1.4

0 1 2 3 4 5

SF

D(T

NS)

(m)

TNS (s)

Predicted - 2% Damp

Predicted - 5% Damp

(b) Displacement FRS.

Figure 9: Acceleration and displacement floor response spectra using the proposed method to design level earthquake in UCPhysics Building at the roof in the transverse direction at 2% and 5% nonstructural damping.

spectra and floor displacement response spectra is observed at allfloors at long periods. In the floor displacement response spectrain Figure 8, where TNS is longer than 2 s (approximately 2.5T1)only minor amplification from the ground response spectrumwith increasing floor height can be observed. This amplificationis assumed negligible for practical engineering applications. Asshown in Figure 8, taking the maximum of the combined modalresponse and the ground acceleration response spectrum providessufficiently accurate predictions at these periods.

The peak floor acceleration of the floor acceleration responsespectra at floors 3 and 9 in Figure 8 (near TNS = 0) are predictedat lower intensities than the recorded spectra. This may be dueto uncertainty in the assessment of the spectral acceleration ofeach mode of the building used in Equation 1, SGA(Ti,ξstr). Asobserved in Figure 7, the recorded ground response spectra havelarge spectral acceleration differences across small incrementsof period. Consequently, the scaling of the modal contributionsby SGA(Ti,ξstr) is sensitive to the exact period value assumed.In practice, however, the floor acceleration response spectrumwould be estimated using a code-derived design ground acceler-ation response spectrum and thus such uncertainties would notbe as significant.

In practice, the proposed method will likely be used with a designground acceleration response spectrum prescribed by a standard.Figure 9 shows the design floor acceleration response spectrumand design displacement response spectrum computed usingthe design ground acceleration response spectrum for the UCPhysics building given in NZS1170.5 [20]. The figure shows thespectra produced for the transverse direction, taking T1 = 0.60 s,at 2% and 5% nonstructural damping. These spectra show thesmoother shape that is computed using design methods. It can beobserved in the design floor displacement response spectrum thatthe ground response spectrum quickly dominates the spectrumfor periods longer than approximately 0.8 s. As noted earlier,these design floor response spectra have large variations oversmall intervals of nonstructural component period. Uncertaintyin the nonstructural component period should be consideredwhen using these spectra, as an overly prescriptive period todesign to lower spectral ordinates may not be realistic.

Influence of Uncertainty in Fundamental Period Predictionson Floor Spectra Predictions

Much of the quality of the prediction relies on predicting thefundamental period of the building, T1, accurately. As discussedearlier, empirical methods for predicting T1 are available in many

codes. The fundamental periods of the instrumented buildingswere computed using the empirical method in the commentaryof NZS1170.5 [20]. These are given in Table 5 alongside the cor-responding T1 values determined using the frequency responsefunction (FRF) method. It can be observed that the code methodover-predicts T1 in all except the BNZ CentrePort building. Thisis contrary to the general trend noted in the commentary [20] thatthe empirical method would give a shorter fundamental periodwhich thus provide a conservative design spectral acceleration.

To illustrate how the accuracy of the prediction of T1 can impactthe floor acceleration response spectra produced using the pro-posed method, floor spectra for the longitudinal direction of theUC Physics building are examined herein. This example waschosen since the fundamental period assessed by the empiricalNZS1170.5 method disagreed most with that inferred using theFRF method. The empirical method was used assuming thewalls and coupling beams acted as a wall system. The periods ofmodes 2 and 3 were predicted using the ratios given in Table 2,and are summarised in Table 6.

To compare performance, the proposed method was applied topredict the response in the M6.3 Lyttelton 2011 earthquake at theroof using the T1 values from empirical code and FRF methods.The 5%-damped floor acceleration response spectra predictedare shown in Figure 10. The DAF is only wide enough to capturethe spectral acceleration near the observed fundamental period(between 0.3 s to 0.7 s) for the floor acceleration response spec-trum prediction where T1 was inferred by FRF, failing to do sofor the spectrum predicted using T1 from the empirical method.In both floor acceleration response spectrum predictions the peakspectral acceleration of the fundamental mode is lower than theobserved response. This is likely due to the ground level spectralordinates that correspond to the fundamental periods inferred

Table 6: Periods of vibration used to determine the flooracceleration response spectra in the UC Physics building

using the frequency response function (FRF), the empiricalequation given for T1 in the commentary NZS1170.5, and

eigenvalue analysis.

Method T1 (s) T2 (s) T3 (s)

FRF 0.46 0.15 0.08

NZS1170.5 0.65 0.13 0.08

Eigenvalue 0.28 0.10 0.08

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using these methods.

An eigenvalue analysis was undertaken as an alternate means toassess the modal properties required by the proposed method.This was computed using a 2D frame model of the longitudinaldirection of the UC Physics building adapted from McHattie [24].The cracked flexural stiffnesses of the walls and coupling beamswere assumed to be 50% of the uncracked state, corresponding tothe effective stiffness properties recommended at serviceabilitylimit state intensity with the assumed ductility µ = 3 for wallsand coupling beams given in NZS3101:2006 [27]. The periodsof vibration found using eigenvalue analysis are shown in Ta-ble 6. Figure 10 shows the performance of the proposed floorspectrum using the periods of vibration found using the FRF andeigenvalue analysis methods. Here, as the eigenvalue analysisunder-predicted T1, the assessed peak again falls outside of thefundamental mode amplification range observed from the record.

Potentially more accurate predictions of T1 can be achieved inpractice through instrumentation of a building where the struc-tural system has been constructed, such as in design for theretrofit of components within an existing structure. A low-costaccelerometer could be mounted at the roof level to record am-bient building motion caused by strong wind or low intensityearthquakes. This could be processed to determine the fundamen-

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Figure 10: Floor acceleration response spectra for the UCPhysics building for the Lyttelton 2011 earthquake record inthe longitudinal direction at the roof. Predicted accelerationspectra are overlaid made using the proposed method usingthe fundamental periods inferred by the frequency response

function (FRF) and the method proposed in the New Zealandstandard NZS1170.5. Spectra are given at 5% nonstructural

damping.

tal period for use in the proposed method, potentially improvingthe accuracy of the floor acceleration response spectra calculated.The prediction may be affected by additional sources of stiffnessat low intensities which may be different at the design responsefor design hazard intensities. This would likely result in a shorterfundamental period predicted which would be conservative whenused with a design ground acceleration response spectrum. Thisdiscrepancy may not make significant difference to a predictedfloor acceleration response spectrum due to the broad nature ofthe amplification region of the DAF.

Comparison of the Proposed and Code Floor Spectra Meth-ods

Figure 11 compares the performance of the proposed methodagainst the international code methods Eurocode 8 [21],NZS1170.5 [20], and the ASCE 7-16 alternate method [2]. Thisfigure shows the floor acceleration response spectra and floordisplacement response spectra computed for the UC Physicsbuilding M6.3 Lyttelton 2011 earthquake record in the trans-verse direction at the roof at 2% and 5% nonstructural damping.The proposed method can predict the high amplification of thefundamental mode where the code methods do not. The highermode ranges are captured where Eurocode 8 neglects them. Thepeak floor acceleration, at SFA,i, j(TNS = 0,ξNS), is more accu-rately represented than the over-conservative NZS1170.5 ap-proach. The less conservative design acceleration requirementswill result in lower costs for rigid components. This is especiallyrelevant for heavy plant components for which design in accor-dance with current requirements can be prohibitively expensive.Beyond the T1 amplification peak, between 0.8 s and 1.5 s, theproposed method again follows closer to the recorded spectrathan the code approaches which are conservative for that periodrange. At longer periods in the displacement spectra the codepredictions do not follow the physical behaviour, while the pro-posed method is able to provide more reasonable estimates. Theproposed method is further able to capture increased dynamicamplification at lower values of nonstructural damping whereasthe international code methods cannot.

Application of Proposed Method to Inelastic Building Re-sponses

To gauge the applicability of this method to inelastically respond-ing buildings, the response of the BNZ CentrePort building inthe Kaikoura 2016 earthquake was examined. As can be seenin Figure 5(h), the Kaikoura 2016 event was near the ULS de-sign intensity level at the spectral acceleration correspondingto the transverse elastic fundamental period. This resulted in

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Figure 11: Acceleration and displacement floor response spectra for the UC Physics building Lyttelton 2011 earthquake record inthe transverse direction at the roof at 2% and 5% nonstructural damping. Predictions at these damping values are shown for theproposed method, Eurocode 8, NZS1170.5, and the ASCE 7-16 alternate method, the latter three not varying with nonstructural

damping.

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Figure 12: Acceleration and displacement floor response spectra (FRS) for the BNZ CentrePort building for the Kaikoura 2016earthquake in the transverse direction at floor 5 at 2% and 5% nonstructural damping.

the structural system responding inelastically [25]. Figure 12shows the predicted and recorded floor acceleration responsespectrum and floor displacement response spectrum for in thetransverse direction at floor 5. This uses a fundamental period of1.20 s, inferred from the FRF of the M6.6 Grassmere 2013 earth-quake motion records. The fundamental period appears to haveelongated to approximately 1.40 s, widening the correspondingamplification peak. The recorded peak spectral acceleration andpeak spectral displacement are lower than that predicted by theelastic prediction method, as suggested by methods proposed inliterature [4; 7; 14]. Future research aims to incorporate a meansof accounting for inelastic building behaviour in the methodproposed here.

Quantifying the Error in Predicted Floor Spectra

To assess the overall performance of the proposed method, theestimated and recorded floor acceleration response spectra at theroof level of each building are compared to the correspondingcode predictions for the events listed in Table 4. Both orthogonaldirections are examined at 2% and 5% nonstructural componentdamping. The predictions used the fundamental periods inferredusing FRF, as summarised in Table 4. To measure the errorbetween the recorded and predicted spectra the mean percentageerror (MPE) was calculated using Equation 11:

MPE(%) =100%nTNS

nTNS

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| SFA,Predict,n−SFA,Record,n |SFA,Record,n

(11)

where nTNS is the number of TNS points in the spectrum.

After approximately TNS = 1.5 s significant divergence betweenall of the code approach floor acceleration response spectra andthe recorded spectrum is expected. Where spectra are computedwith periods longer than TNS = 2 s, the mean percentage errorsmeasured are dominated by the long period ordinates. Thisdomination is not clearly visible in plots with linear axes as bothrecorded and predicted spectra have low spectral accelerationat long periods. Instead, this divergence can be observed in thefloor displacement response spectra in Figure 11(b). To enablereasonable comparison between the methods, therefore, the flooracceleration response spectra produced for error measurementwere created from TNS = 0.01 s to 2 s, with an interval of 0.01 s.The results of this error measurement method are presented inFigures 13 and 14 for 2% and 5% nonstructural damped spectra,respectively.

It can be observed in both Figures 13 and 14 that the proposed

method generally performs better than the code approaches inboth orthogonal directions for the UC Physics building and theAvalon GNS buildings. The proposed method was, on average,28% lower than the best performing international code methodfrom these cases, Eurocode 8. The modifications made to theASCE 7-16 method which comprise the proposed method, themodified DAF shape and modified maximum DAF, resulted inreliably improved acceleration response spectrum predictions.This was evidenced by the significantly lower error measured forspectra predicted using the proposed method compared to theASCE 7-16 method.

Previous literature has reported the Eurocode 8 method mayperform poorly as it neglects amplification of demands at highermodes of the building [7]. This is observed in the high errormeasured for the Eurocode 8 method compared with the pro-posed method for most buildings in Figures 13 and 14. There isthe notable exception of the BNZ building, for which the errorcomputed was significantly lower than the other methods, partic-ularly in the longitudinal direction. This case is investigated inFigure 15(a), where the code method predictions, the proposedmethod prediction, and recorded floor acceleration responsespectra are shown for the Kaikoura earthquake motion recordedin the longitudinal direction of the BNZ building, at 2% and 5%nonstructural damping. Here no strong higher mode responsesare recorded, which Eurocode 8 assumes. The shape of theEurocode 8 spectrum is also seen to better capture the changesin the floor acceleration response spectrum due to the structurebehaving inelastically, although the spectral accelerations are fartoo low. This includes better following the wide fundamentalmode amplification of spectral accelerations due the elongationof the fundamental period, and the lower spectral accelerationsobserved than predicted by the proposed and ASCE 7-16 meth-ods which use elastic modal properties. The limited benefit ofusing the Eurocode 8 prediction method, however, was observedin the poorer measured performance for predicting the responseof the other buildings. This is particularly relevant where highermode responses are more dominant, which is the case for thelongitudinal directions of the UC Physics building and the MBIEStout St building. This can be seen by comparing the Eurocode 8predictions and recorded floor acceleration response spectra forthese cases in Figures 11(a) and 16(a).

The error measured for the MBIE Stout St building is interestingas all methods performed almost equally as well, as seen inFigures 13 and 14. Figure 16(a) shows the predictions andrecorded floor acceleration response spectra for the Kaikouraearthquake motion recorded in the longitudinal direction at 2%

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Figure 14: Mean percentage error each event for the case study buildings at the roof level in each orthogonal direction at 5%nonstructural damping, using the T1 determined in each event using FRF.

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and 5% nonstructural damping. This illustrates that the modalmethods make good approximations to the fundamental modeamplification peak, though fail to assess the correct intensity ofthe higher mode responses. The proposed method also reducestoo quickly after the fundamental mode plateau in this case. TheEurocode 8 and NZS1170.5 methods are off by approximatelythe same amount for all spectral ordinates, though follow thegeneral shape and thereby have similar error measurements to themodal approaches. These differences appear to have averaged toproduce similar error measurements. This suggests a possibleissue with how the error is quantified, as Figure 16 (a) makesthe proposed and ASCE methods appear far more reflectiveof the recorded spectra than the Eurocode 8 and NZS1170.5approaches.

Measured Impact of using Simplified Estimates of T1

As explained earlier, one means of maintaining a simplified floorresponse spectrum approach could be to use simplified estimatesof T1. To assess how this may impact accuracy, the variousprediction methods were applied again using the simplified pe-riod expressions from the commentary of NZS1170.5, and errorvalues recomputed. The results are presented in Figures 17 and18 for 2% and 5% nonstructural damped spectra, respectively.Although the NZS1170.5 floor acceleration response spectrummethod does not rely on T1, and thus the error does not change,it is presented here for comparison with the other approaches.

The direct correlation of the quality of the assessment of T1 tothe floor acceleration response spectrum produced by these sim-plified methods can be observed by comparing error measured inthe spectra predicted using T1 inferred from FRF, Figures 13 and14, with those predicted using T1 predicted using the empirical

method, Figures 17 and 18. It is most clear by comparing forthe longitudinal and transverse directions of the UC Physicsbuildings. In the longitudinal direction, where the empiricalcode prediction of T1 is far from the average FRF T1, 0.65 s to0.42 s respectively, the proposed method error averaged acrossthe events increased dramatically. In contrast, the empiricalcode assessment of T1 is far closer to the average FRF T1 inthe transverse direction, 0.65 s to 0.60 s respectively, whichresulted in a relatively minor increase in error. This shows forsmall uncertainty in assessing T1, the width of the DAF allowsfor variation in the true narrow observed amplification peakrecorded in these events. This is seen similarly in the AvalonGNS buildings, where the broad amplification peaks capture thisuncertainty and only a minor increase in error is observed. Ifwider peaks are used greater conservatism is given to addressthis uncertainty. This may not, however, reduce the error asthe then-overpredicted range would dominate the measurement.This illustrates the balancing of conservation and accuracy thatthis simplified approach is attempting to find, and which thiserror measurement method penalises the former.

To visualise how these predictions change with different T1 val-ues, Figures 15(b) and 16(b) provide predicted and recorded flooracceleration response spectra using the periods inferred usingthe empirical code method for the same cases as Figures 15(a)and 16(b).

CONCLUSION

A practice-oriented method for the prediction of elastic flooracceleration response spectra and floor displacement responsespectra in buildings has been proposed. The method aims toimprove upon previous methods by accounting for many phys-

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Figure 15: Performance of code and proposed methods using fundamental periods inferred using frequency response functions(FRF) and the NZS1170.5 empirical method for estimating roof level acceleration floor response spectra (FRS) in the longitudinal

direction of the BNZ CentrePort building for the Kaikoura earthquake at 2% and 5% damping.

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Figure 16: Performance of code and proposed methods using fundamental periods inferred using frequency response functions(FRF) and the NZS1170.5 empirical method for estimating roof level acceleration floor response spectra (FRS) in the longitudinal

direction of the MBIE Stout St building for the Kaikoura earthquake at 2% and 5% damping.

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Figure 17: Mean percentage error each event for the case study buildings at the roof level in each orthogonal direction at 2%nonstructural damping, using the T1 determined in each event using NZS1170.5 commentary expression for building period.

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Figure 18: Mean percentage error each event for the case study buildings at the roof level in each orthogonal direction at 5%nonstructural damping, using the T1 determined in each event using NZS1170.5 commentary expression for building period.

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ical factors that influence floor acceleration response spectrawhile aiming for a method that is easy to use. This was built onprevious proposals, where a dynamic amplification factor (DAF)models the dynamic amplification due to resonance between themounted component and the structural modes at varying levelsof damping of the nonstructural component. The shape of theDAF proposed was modified from the simple shape proposedin ASCE 7-16, adopting a decay at long component periods toexplicitly consider the derivation of floor displacement responsespectra from floor acceleration response spectra. Rigid body mo-tion was accounted for by taking final floor acceleration responsespectrum prediction as the maximum of both the combined con-tribution of the modes to the floor acceleration response spectrumand the ground acceleration response spectrum.

A novel approach was used to assess the accuracy of the proposedmethod by comparing recorded floor acceleration spectra fromfive GeoNet Structural Array instrumented buildings to predic-tions computed using the proposed method. This was comparedwith the predictions made using the NZS1170.5, Eurocode 8, andASCE 7-16 code methods. Performance was measured by com-puting the mean percentage errors between the predictions andrecords, computed for roof-level floor acceleration response spec-tra damped at 2% and 5%. For the spectra produced from recordswhere the buildings responded elastically in the 12 investigatedearthquakes, the error measured was on average 28% lower forthe predictions made by the proposed method compared to thebest performing international code method, Eurocode 8. Theobservation that the Eurocode 8 method performed well may be afunction of how the error is quantified, as this in contrast to otherstudies in the literature and likely reflects the low participationof higher modes in the selected case study buildings.

The accuracy of a floor acceleration response spectrum predictedusing the proposed method is heavily dependent on the accuracyof the predicted fundamental period of vibration of the building.Simplified empirical expressions for T1 from the commentaryof NZS1170.5 were trialled and found to be unreliable. It issuggested that modal characteristics of the structure are assessedthrough eigenvalue analysis where possible.

The proposed method currently has been formulated only forthe case in which buildings respond elastically and so may besuitable for serviceability limit state (SLS) intensity levels. Fur-ther work is required to extend the method to intensities wherebuildings and components respond non-linearly, like the ultimatelimit state (ULS) intensity. To account for this and further uncer-tainties yet to be fully investigated, broad period ratios used todefine DAF are recommended.

There is an expectation that the nonstructural components, too,have some ductility capacity. Further research may show thatthe narrow, high spectral acceleration peaks from the modes ofthe building observed in elastic spectra do not present signifi-cant problems provided that components possess some ductilityand thus expressions for inelastic floor spectra should also bedeveloped. However, it is also expected that these narrow peakscan be avoided by bracing a nonstructural element to reduce itsfundamental period away from the periods of the building. In-formation is also limited on the values expected for the dampingof specific types of nonstructural components. Since floor accel-eration response spectra were observed to amplify significantlywith decreasing damping values for nonstructural components,this topic should also be a subject of future research.

ACKNOWLEDGEMENTS

The use of the GeoNet structural array enabled the verificationand refinement of the method presented in this paper. Thanks are

given to GeoNet, the tenants and the owners of these buildingsfor the foresight in instrumenting these structures to provide suchan excellent engineering resource which proved invaluable inthis research.

This project was (partially) supported by QuakeCoRE, a NewZealand Tertiary Education Commission-funded Centre.This isQuakeCoRE publication number 0470.

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2 American Society of Civil Engineers (2017). ASCE/SEI 7-16:Minimum design loads and associated criteria for buildingsand other structures. American Society of Civil Engineers,Reston, Virginia, 834 pp.

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Appendix to

A PRACTICE-ORIENTED METHOD FOR ESTIMATINGELASTIC FLOOR RESPONSE SPECTRA

Kieran Haymes, Timothy J. Sullivan and Reagan Chandramohan

OVERVIEW

This document contains additional tables to assist in enabling theuse of the elastic floor response spectrum method proposed in themain work. Tables A1, A2, and A3 provide mode shapes at eachfloor level for buildings between 1 and 20 storeys tall for modes1, 2 and 3, respectively. Table A4 provides the participationfactors that correspond to these mode shapes.

The values were produced using the method outlined in Mirandaand Taghavi [23]. These were produced using the value given

in Miranda and Taghavi [23] for the dimensionless variableα0 of 3.125, corresponding to a dual shear wall and momentresisting frame lateral force resisting system. For this, interstoreyheights, seismic mass lumped at floor levels, and lateral stiffnessare assumed to be constant throughout the building’s height.The participation factors provided in Table A4 were calculatedusing Equation 10 in the main work, where the mode shapesare taken as discrete points at the floor levels rather than usingthe continuous integration method used in Miranda and Taghavi[23].

Page 20: A PRACTICE-ORIENTED METHOD FOR ESTIMATING ELASTIC … · Kieran Haymes1, Timothy J. Sullivan2 and Reagan Chandramohan3 (Submitted November 2019; Reviewed December 2019; Accepted March

135Ta

ble

1:M

ode

shap

esfo

rmod

e1

forb

uild

ings

with

unifo

rmm

assa

ndα

0=3.

125

acco

rdin

gto

Mir

anda

and

Tagh

avi[

23].

12

34

56

78

910

11

12

13

14

15

16

17

18

19

20

11.0

00

0.4

51

0.2

44

0.1

51

0.1

03

0.0

74

0.0

56

0.0

44

0.0

35

0.0

29

0.0

24

0.0

20

0.0

18

0.0

15

0.0

13

0.0

12

0.0

10

0.0

09

0.0

08

0.0

08

21.0

00

0.6

56

0.4

51

0.3

25

0.2

44

0.1

89

0.1

51

0.1

23

0.1

03

0.0

87

0.0

74

0.0

64

0.0

56

0.0

49

0.0

44

0.0

39

0.0

35

0.0

32

0.0

29

31.0

00

0.7

51

0.5

76

0.4

51

0.3

60

0.2

94

0.2

44

0.2

05

0.1

75

0.1

51

0.1

32

0.1

16

0.1

03

0.0

91

0.0

82

0.0

74

0.0

67

0.0

61

41.0

00

0.8

05

0.6

56

0.5

40

0.4

51

0.3

80

0.3

25

0.2

80

0.2

44

0.2

14

0.1

89

0.1

69

0.1

51

0.1

36

0.1

23

0.1

12

0.1

03

51.0

00

0.8

39

0.7

11

0.6

06

0.5

21

0.4

51

0.3

93

0.3

45

0.3

06

0.2

72

0.2

44

0.2

20

0.1

99

0.1

81

0.1

65

0.1

51

61.0

00

0.8

64

0.7

51

0.6

56

0.5

76

0.5

08

0.4

51

0.4

02

0.3

60

0.3

25

0.2

94

0.2

67

0.2

44

0.2

23

0.2

05

71.0

00

0.8

81

0.7

81

0.6

95

0.6

20

0.5

55

0.4

99

0.4

51

0.4

08

0.3

72

0.3

39

0.3

11

0.2

86

0.2

64

81.0

00

0.8

95

0.8

05

0.7

26

0.6

56

0.5

95

0.5

40

0.4

93

0.4

51

0.4

13

0.3

80

0.3

51

0.3

25

91.0

00

0.9

06

0.8

24

0.7

51

0.6

86

0.6

28

0.5

76

0.5

29

0.4

88

0.4

51

0.4

17

0.3

87

10

1.0

00

0.9

14

0.8

39

0.7

72

0.7

11

0.6

56

0.6

06

0.5

61

0.5

21

0.4

84

0.4

51

11

1.0

00

0.9

22

0.8

52

0.7

90

0.7

33

0.6

80

0.6

33

0.5

89

0.5

50

0.5

14

12

1.0

00

0.9

28

0.8

64

0.8

05

0.7

51

0.7

02

0.6

56

0.6

14

0.5

76

13

1.0

00

0.9

33

0.8

73

0.8

18

0.7

67

0.7

20

0.6

77

0.6

36

14

1.0

00

0.9

38

0.8

81

0.8

29

0.7

81

0.7

37

0.6

95

15

1.0

00

0.9

42

0.8

88

0.8

39

0.7

94

0.7

51

16

1.0

00

0.9

45

0.8

95

0.8

48

0.8

05

17

1.0

00

0.9

48

0.9

01

0.8

56

18

1.0

00

0.9

51

0.9

06

19

1.0

00

0.9

53

20

1.0

00

Floor level

Nu

mber

of

store

ys

Tabl

e2:

Mod

esh

apes

form

ode

2fo

rbui

ldin

gsw

ithun

iform

mas

sand

α0=

3.12

5ac

cord

ing

toM

iran

daan

dTa

ghav

i[23

].

12

34

56

78

910

11

12

13

14

15

16

17

18

19

20

1-0

.674

-0.6

01

-0.4

37

-0.3

21

-0.2

42

-0.1

89

-0.1

50

-0.1

23

-0.1

02

-0.0

86

-0.0

73

-0.0

63

-0.0

55

-0.0

49

-0.0

43

-0.0

39

-0.0

35

-0.0

31

-0.0

28

21.0

00

-0.3

30

-0.6

74

-0.6

79

-0.6

01

-0.5

14

-0.4

37

-0.3

73

-0.3

21

-0.2

78

-0.2

42

-0.2

13

-0.1

89

-0.1

68

-0.1

50

-0.1

36

-0.1

23

-0.1

12

-0.1

02

31.0

00

-0.0

35

-0.5

14

-0.6

74

-0.6

93

-0.6

56

-0.6

01

-0.5

42

-0.4

87

-0.4

37

-0.3

93

-0.3

55

-0.3

21

-0.2

91

-0.2

65

-0.2

42

-0.2

22

-0.2

04

41.0

00

0.1

65

-0.3

30

-0.5

75

-0.6

74

-0.6

96

-0.6

79

-0.6

43

-0.6

01

-0.5

57

-0.5

14

-0.4

74

-0.4

37

-0.4

04

-0.3

73

-0.3

46

-0.3

21

51.0

00

0.3

03

-0.1

68

-0.4

52

-0.6

04

-0.6

74

-0.6

96

-0.6

88

-0.6

66

-0.6

35

-0.6

01

-0.5

66

-0.5

31

-0.4

98

-0.4

67

-0.4

37

61.0

00

0.4

03

-0.0

35

-0.3

30

-0.5

14

-0.6

21

-0.6

74

-0.6

94

-0.6

93

-0.6

79

-0.6

56

-0.6

29

-0.6

01

-0.5

71

-0.5

42

71.0

00

0.4

79

0.0

75

-0.2

19

-0.4

21

-0.5

51

-0.6

31

-0.6

74

-0.6

93

-0.6

95

-0.6

86

-0.6

70

-0.6

49

-0.6

25

81.0

00

0.5

37

0.1

65

-0.1

21

-0.3

30

-0.4

77

-0.5

75

-0.6

38

-0.6

74

-0.6

92

-0.6

96

-0.6

90

-0.6

79

91.0

00

0.5

84

0.2

40

-0.0

35

-0.2

46

-0.4

02

-0.5

14

-0.5

92

-0.6

43

-0.6

74

-0.6

91

-0.6

96

10

1.0

00

0.6

22

0.3

03

0.0

41

-0.1

68

-0.3

30

-0.4

52

-0.5

41

-0.6

04

-0.6

47

-0.6

74

11

1.0

00

0.6

54

0.3

57

0.1

07

-0.0

98

-0.2

62

-0.3

90

-0.4

88

-0.5

61

-0.6

13

12

1.0

00

0.6

81

0.4

03

0.1

65

-0.0

35

-0.1

98

-0.3

30

-0.4

34

-0.5

14

13

1.0

00

0.7

04

0.4

43

0.2

17

0.0

23

-0.1

39

-0.2

73

-0.3

81

14

1.0

00

0.7

24

0.4

79

0.2

62

0.0

75

-0.0

85

-0.2

19

15

1.0

00

0.7

41

0.5

10

0.3

03

0.1

22

-0.0

35

16

1.0

00

0.7

56

0.5

37

0.3

40

0.1

65

17

1.0

00

0.7

70

0.5

62

0.3

73

18

1.0

00

0.7

82

0.5

84

19

1.0

00

0.7

93

20

1.0

00

Nu

mber

of

store

ys

Floor level

Page 21: A PRACTICE-ORIENTED METHOD FOR ESTIMATING ELASTIC … · Kieran Haymes1, Timothy J. Sullivan2 and Reagan Chandramohan3 (Submitted November 2019; Reviewed December 2019; Accepted March

136Ta

ble

3:M

ode

shap

esfo

rmod

e3

forb

uild

ings

with

unifo

rmm

assa

ndα

0=3.

125

acco

rdin

gto

Mir

anda

and

Tagh

avi[

23].

12

34

56

78

910

11

12

13

14

15

16

17

18

19

20

10.6

82

0.7

05

0.5

96

0.4

86

0.3

96

0.3

26

0.2

72

0.2

30

0.1

96

0.1

69

0.1

48

0.1

30

0.1

15

0.1

02

0.0

92

0.0

83

0.0

75

0.0

68

2-0

.649

-0.0

36

0.4

72

0.6

82

0.7

29

0.7

05

0.6

55

0.5

96

0.5

39

0.4

86

0.4

38

0.3

96

0.3

59

0.3

26

0.2

97

0.2

72

0.2

50

0.2

30

31.0

00

-0.5

54

-0.5

05

-0.0

36

0.3

42

0.5

68

0.6

82

0.7

25

0.7

26

0.7

05

0.6

73

0.6

35

0.5

96

0.5

58

0.5

21

0.4

86

0.4

54

0.4

24

41.0

00

-0.3

54

-0.6

49

-0.3

94

-0.0

36

0.2

63

0.4

72

0.6

06

0.6

82

0.7

19

0.7

29

0.7

23

0.7

05

0.6

82

0.6

55

0.6

26

0.5

96

51.0

00

-0.1

73

-0.6

33

-0.5

80

-0.3

23

-0.0

36

0.2

10

0.3

99

0.5

34

0.6

25

0.6

82

0.7

14

0.7

27

0.7

28

0.7

20

0.7

05

61.0

00

-0.0

25

-0.5

54

-0.6

49

-0.5

05

-0.2

74

-0.0

36

0.1

73

0.3

42

0.4

72

0.5

68

0.6

36

0.6

82

0.7

10

0.7

25

71.0

00

0.0

93

-0.4

55

-0.6

48

-0.6

06

-0.4

43

-0.2

39

-0.0

36

0.1

45

0.2

98

0.4

21

0.5

17

0.5

90

0.6

44

81.0

00

0.1

89

-0.3

54

-0.6

11

-0.6

49

-0.5

54

-0.3

94

-0.2

13

-0.0

36

0.1

24

0.2

63

0.3

78

0.4

72

91.0

00

0.2

67

-0.2

59

-0.5

54

-0.6

53

-0.6

18

-0.5

05

-0.3

55

-0.1

93

-0.0

36

0.1

07

0.2

34

10

1.0

00

0.3

32

-0.1

73

-0.4

88

-0.6

33

-0.6

49

-0.5

80

-0.4

63

-0.3

23

-0.1

77

-0.0

36

11

1.0

00

0.3

87

-0.0

95

-0.4

21

-0.5

98

-0.6

54

-0.6

25

-0.5

41

-0.4

26

-0.2

96

12

1.0

00

0.4

33

-0.0

25

-0.3

54

-0.5

54

-0.6

43

-0.6

49

-0.5

96

-0.5

05

13

1.0

00

0.4

74

0.0

37

-0.2

90

-0.5

05

-0.6

20

-0.6

55

-0.6

30

14

1.0

00

0.5

08

0.0

93

-0.2

30

-0.4

55

-0.5

89

-0.6

48

15

1.0

00

0.5

39

0.1

43

-0.1

73

-0.4

04

-0.5

54

16

1.0

00

0.5

66

0.1

89

-0.1

20

-0.3

54

17

1.0

00

0.5

90

0.2

30

-0.0

71

18

1.0

00

0.6

12

0.2

67

19

1.0

00

0.6

31

20

1.0

00

Floor level

Nu

mber

of

store

ys

Tabl

e4:

Part

icip

atio

nfa

ctor

scor

resp

ondi

ngto

the

first

thre

em

odes

shap

esfo

rbui

ldin

gsw

ithun

iform

mas

sand

α0=

3.12

5ac

cord

ing

toM

iran

daan

dTa

ghav

i[23

]asp

rovi

ded

inTa

bles

A1

toA

3.

12

34

56

78

910

11

12

13

14

15

16

17

18

19

20

11.0

00

1.2

06

1.2

75

1.3

14

1.3

40

1.3

58

1.3

72

1.3

82

1.3

91

1.3

98

1.4

03

1.4

08

1.4

12

1.4

16

1.4

19

1.4

22

1.4

24

1.4

26

1.4

28

1.4

30

20.2

24

0.0

47

-0.0

89

-0.1

88

-0.2

62

-0.3

20

-0.3

66

-0.4

03

-0.4

34

-0.4

60

-0.4

82

-0.5

01

-0.5

17

-0.5

32

-0.5

45

-0.5

56

-0.5

66

-0.5

76

-0.5

84

30.5

48

0.6

18

0.6

17

0.6

09

0.5

99

0.5

91

0.5

83

0.5

76

0.5

70

0.5

65

0.5

61

0.5

57

0.5

53

0.5

50

0.5

47

0.5

44

0.5

42

0.5

40

Nu

mber

of

store

ys

Mode