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Miguel A. Diaz , Koichi Kusunoki , and Akira Tasai

Miguel A. Diaz , Koichi Kusunoki , and Akira Tasai

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Table 1 Characteristics of specimens<br />

Specimen<br />

Thickness<br />

1 st F<br />

column<br />

(mm)<br />

Height<br />

1 st F<br />

(mm)<br />

Total<br />

weight<br />

(kN)<br />

Natural<br />

period<br />

(s)<br />

Yield.<br />

Disp.<br />

(mm)<br />

Frame1 a 4.5 805 1.450 1.03 66<br />

Frame2 a, b 4.5 1005 1.464 1.66 101<br />

S-F 01, 02, 03 6.0 1000 1.485 0.93 71<br />

S-S 01, 02 6.0 1000 1.485 0.99 73<br />

S-S 03, 04 6.0 1000 1.485 0.98 73<br />

a) Velocity response spectra<br />

The measurement system was given by accelerometers<br />

at the base <strong>and</strong> beams of each level, <strong>and</strong> displacement<br />

transducers connected at each eastern rigid joint, as shown in<br />

Figure 3.<br />

3.2 Input waveforms<br />

The input motions to conduct this study were one<br />

artificial wave: the WG60, <strong>and</strong> two earthquake records: the<br />

KOBE-NS (Kobe, 1995) <strong>and</strong> the MYG013 (Tohoku, 2011).<br />

The input motions were scaled in order to induce different<br />

performance levels on the specimen within elastic <strong>and</strong><br />

inelastic ranges, both mainshocks <strong>and</strong> aftershocks. Figure 4<br />

shows the WG60, the KOBE-NS <strong>and</strong> the MYG013<br />

waveforms.<br />

b) Displacement <strong>and</strong> acceleration response spectra<br />

Figure 5 Response spectra<br />

3.3 Equivalent SDOF<br />

In order to conduct the residual seismic performance<br />

analysis, it is necessary to transform the capacity curve of<br />

the specimen in terms of S a − S d relations.<br />

The probable value of the maximum response is usually<br />

given by the square root of the sum of square (SRSS) of the<br />

maximum modal response components. Then the maximum<br />

displacement at i-th story <strong>and</strong> the base shear force can be<br />

expressed approximately by Eq. (5) <strong>and</strong> Eq. (6) (Shibata,<br />

2010), respectively; where s S d , s S a is the spectral<br />

displacement <strong>and</strong> spectral acceleration for the s-th mode.<br />

The base shear force of N-DOF is given by Eq. (7).<br />

|δ i | max ≈ √∑<br />

N<br />

| s β ∙ s u i ∙ S d<br />

s | 2<br />

S=1 (5)<br />

Figure 4 Input waveforms<br />

Figure 5 shows their respective a) normalized velocity<br />

response spectra respect to the maximum spectral velocity,<br />

<strong>and</strong> b) normalized response spectra respect to peak ground<br />

acceleration (PGA) <strong>and</strong> maximum spectral displacement.<br />

The maximum spectral response with viscous damping ratio<br />

of 0.05 was obtained at periods of 1.27 seconds, 0.87<br />

seconds <strong>and</strong> 0.67 seconds for the WG60, the KOBE-NS <strong>and</strong><br />

the MYG013 waveforms, respectively (Figure 5a).<br />

N N<br />

S=1 i=1<br />

+ (6)<br />

Q ≈ √∑ *∑ m i ∙ s β ∙ s u i ∙ s S a<br />

N<br />

Q = ∑i=1 m i ∙ (ẍ i + ẍ g) (7)<br />

Particularly, the specimens can be assumed as 3-DOF<br />

systems. Their configuration allows that second <strong>and</strong> third<br />

participation factor can be neglected, <strong>and</strong> the first-mode<br />

distribution can be assumed as the unit { 1 u} ≈ *1+. Then<br />

Eq. (5) is rewritten as Eq. (8) to calculate the spectral<br />

acceleration, <strong>and</strong> Eq. (7) into Eq. (6) is rewritten as Eq. (9) to<br />

calculate the spectral displacement.<br />

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