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Earthquake Engineering Research - HKU Libraries - The University ...

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341<br />

DISPLACMENT-BASED NSF<br />

In this paper, a nonlinear static procedure based on displacement is presented. <strong>The</strong> method is a<br />

displacement-based analysis method that adds checking computation of displacement and deformation<br />

of structures. It maintains the simplicity of pushover analysis, and extends pushover analysis to<br />

investigate structural dynamic characteristic, and to account for development of displacement, and to<br />

describe ductility capacity of members set plastic hinge on.<br />

In this method, the acceleration of ground motion is monotonously increased step by step based on<br />

different seismic hazard levels. <strong>The</strong> lateral displacement, instead of base shearing force, is calculated.<br />

Moreover, the distribution of lateral displacement is selected by the mode shapes, which are<br />

considered based on structural dynamic modification considering the residual displacement of inelastic<br />

members, and post yield stiffness etc.<br />

In this method, modal analysis is adopted, because the displacement or force distribution can be<br />

expressed with the modal shapes, and the maximum displacement of each joint or floor of a structure<br />

subjected to the ground motion acceleration can also be expressed with the maximum coordinate using<br />

the displacement response spectrum. Furthermore, the higher modals are taken into consideration via<br />

the SRSS/CQC method. When the displacement is increased to some extend, the structure enters<br />

inelastic range, whose overall stif&iess is modified and whose dynamic characteristics is changed.<br />

<strong>The</strong>n, the structure is anew done modal analysis in order to obtain dynamic characteristics of the<br />

structure in inelastic range.<br />

Modal Analysis<br />

<strong>The</strong> structural motion differential equation is expressed as<br />

(1)<br />

Where M is the mass matrixes, C is the damping matrixes, K is the stiffness matrixes, X is the<br />

displacement vector, x w is the ground acceleration history.<br />

Calculate the eigenvalues and eigenvectors (natural frequencies and modal shapes) of the structure<br />

under undamping free vibration. Assume that X satisfies<br />

where O is the shape matrixes , q is the modal coordinate.<br />

Substitute this expression for X in equation (1):<br />

X=< (2)

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