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

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

from <strong>the</strong> linear distribution point <strong>of</strong> view. Moreover, <strong>the</strong> third shape, calculated as<br />

SRSS combinations <strong>of</strong> <strong>the</strong> load distributions is obtained from modal analyses <strong>of</strong><br />

<strong>the</strong> buildings. The choice <strong>of</strong> this load shape is made to take into consideration <strong>the</strong><br />

anticipated effect <strong>of</strong> <strong>high</strong>er modes <strong>of</strong> vibrations for moderate long period <strong>and</strong><br />

irregular structures, as well as for buildings with hybrid lateral resistance systems.<br />

Ano<strong>the</strong>r difference between <strong>the</strong> two approaches, i.e. <strong>the</strong> EC8 procedure <strong>and</strong> <strong>the</strong><br />

FEMA-273 procedure, is <strong>the</strong> evaluation <strong>of</strong> <strong>the</strong> target displacement. Following <strong>the</strong><br />

indication contained in <strong>the</strong> EC8 (2002), <strong>the</strong> capacity curve, which represents <strong>the</strong><br />

relation between base shear force <strong>and</strong> control node displacement, is determined<br />

by pushover analysis for values <strong>of</strong> <strong>the</strong> control displacement ranging between zero<br />

<strong>and</strong> <strong>the</strong> value corresponding to 150% <strong>of</strong> <strong>the</strong> target displacement. The target<br />

displacement is defined as <strong>the</strong> <strong>seismic</strong> dem<strong>and</strong> derived from <strong>the</strong> elastic response<br />

spectrum in terms <strong>of</strong> <strong>the</strong> displacement <strong>of</strong> an equivalent SDoF system. The<br />

procedure presented in <strong>the</strong> Annex B <strong>of</strong> <strong>the</strong> EC8 (2002) is articulated as follows.<br />

i. The MDoF system is firstly converted into an SDoF system. The following<br />

152<br />

relation between normalized lateral forces Fi <strong>and</strong> normalized displacements Φi<br />

is assumed:<br />

Fi = mi<br />

Φ i<br />

( 4.28 )<br />

where mi is <strong>the</strong> mass in <strong>the</strong> i-th storey. Displacements are normalized in such a<br />

way that Φn=1, where n is <strong>the</strong> control node (usually, n denotes <strong>the</strong> ro<strong>of</strong> level),<br />

so that Fn = mn<br />

. The mass <strong>of</strong> an equivalent SDoF system m * is determined as:<br />

*<br />

m = m Φ = F<br />

( 4.29 )<br />

i i i<br />

<strong>and</strong> <strong>the</strong> transformation factor is given by:<br />

Γ =<br />

*<br />

m<br />

m Φ<br />

i<br />

2<br />

i<br />

=<br />

F<br />

i<br />

F<br />

m<br />

2<br />

i<br />

i<br />

( 4.30 )<br />

The force F * <strong>and</strong> <strong>the</strong> displacement d * <strong>of</strong> <strong>the</strong> equivalent SDoF system are <strong>the</strong>n<br />

computed as:<br />

=<br />

Γ<br />

b F<br />

F *<br />

,<br />

=<br />

Γ<br />

n d<br />

d *<br />

( 4.31 )

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