10.06.2013 Views

Analysis and modelling of the seismic behaviour of high ... - Ingegneria

Analysis and modelling of the seismic behaviour of high ... - Ingegneria

Analysis and modelling of the seismic behaviour of high ... - Ingegneria

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

4. SEISMIC RESPONSE OF PARTIAL-STRENGTH COMPOSITE JOINTS<br />

· <strong>the</strong> maximum rotation <strong>and</strong> local damage in <strong>the</strong> joints;<br />

· <strong>the</strong> local damage in <strong>the</strong> columns;<br />

· <strong>the</strong> value <strong>of</strong> <strong>the</strong> ratio between <strong>the</strong> input energy <strong>and</strong> <strong>the</strong> total hysteretic<br />

energy dissipated.<br />

After <strong>the</strong> elaboration <strong>of</strong> <strong>the</strong> numerical analyses, <strong>the</strong> accelerogram A-14 was<br />

chosen because <strong>of</strong> <strong>the</strong> <strong>high</strong>est level <strong>of</strong> damage induced in <strong>the</strong> joints <strong>and</strong> <strong>the</strong> lower<br />

values <strong>of</strong> damage in <strong>the</strong> columns. This last parameter was taken into account in<br />

order to avoid dangerous global collapse due to <strong>the</strong> loss <strong>of</strong> stability at <strong>the</strong> base<br />

level. The main characteristics <strong>of</strong> <strong>the</strong> accelerogram A-14 are reported in Figure<br />

4.50.<br />

a [m/sec 2 ]<br />

spost. [m]<br />

5.00<br />

4.00<br />

3.00<br />

2.00<br />

1.00<br />

0.00<br />

0.00 2.00 4.00 6.00 8.00 10.00 12.00 14.00 16.00<br />

-1.00<br />

-2.00<br />

-3.00<br />

-4.00<br />

-5.00<br />

0.15<br />

0.10<br />

0.05<br />

time [sec]<br />

0.00<br />

0.00 2.00 4.00 6.00 8.00 10.00 12.00 14.00 16.00<br />

-0.05<br />

-0.10<br />

-0.15<br />

Sa [m/sec 2 ]<br />

12.00<br />

10.00<br />

8.00<br />

6.00<br />

4.00<br />

2.00<br />

0.00<br />

0.00 0.50 1.00 1.50 2.00 2.50 3.00 3.50 4.00<br />

(a) (b)<br />

time [sec]<br />

vel. [m/sec]<br />

0.40<br />

0.30<br />

0.20<br />

0.10<br />

-0.10<br />

-0.20<br />

-0.30<br />

-0.40<br />

T [sec]<br />

0.00<br />

0.00 2.00 4.00 6.00 8.00 10.00 12.00 14.00 16.00<br />

time [sec]<br />

(c) (d)<br />

Figure 4.50. (a) Accelerogram A-14 employed for <strong>the</strong> analyses; (b) Elastic response<br />

spectrum <strong>of</strong> <strong>the</strong> accelerogram A-14 with ξ equal to 5%; (c) Integrated base<br />

displacements after <strong>the</strong> application <strong>of</strong> <strong>the</strong> baseline correction; (d) Integrated base<br />

velocity after <strong>the</strong> application <strong>of</strong> <strong>the</strong> baseline correction<br />

Main results<br />

The pushover <strong>and</strong> <strong>the</strong> incremental dynamic analysis was performed <strong>and</strong> <strong>the</strong>n<br />

compared. Hereinafter <strong>the</strong> main results are reported in Table 4.7, whereas <strong>the</strong><br />

obtained response curves are plotted in Figure 4.51. The uniform <strong>and</strong> triangular<br />

curves <strong>of</strong> <strong>the</strong> pushover analysis represent <strong>the</strong> upper <strong>and</strong> lower limit <strong>of</strong> <strong>the</strong><br />

response curve obtained by <strong>the</strong> IDA (Antoniou et al, 2002). Moreover, in our case,<br />

157

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!