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Nonlinear Finite Element Analysis of Concrete Structures

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- OD -<br />

where<br />

[B e . D e .,, B^-.dV^K 0 . (4.1-20)<br />

J ija ljkl klB aS<br />

e<br />

v<br />

is the symmetric stiffness tensor <strong>of</strong> the element<br />

j N J a b. dV = Ff (4.1-21)<br />

e<br />

v<br />

is the body force vector. Discrete point forces P. can be treated<br />

by this formulation, but are conveniently treated separately by<br />

use <strong>of</strong> eq. (22) which follows from eq. (21).<br />

7N® P. = F pe (4.1-22)<br />

L ia i ex<br />

is the discrete point force vector. The tensor N.<br />

is evaluated<br />

at the location <strong>of</strong> the point force in question and the summation<br />

is extended over all point forces located within the element.<br />

N e t.dS = F te (4.1-23)<br />

ia i a<br />

is the traction force vector.<br />

B S . D 6 .,, e?, dV = F L ° ,. . ...<br />

j lja ljkl kl a (4.1-24)<br />

e<br />

v<br />

is the force vector due to initial strains.<br />

e<br />

v<br />

B ija °ij dV = F °f<br />

is the force vector due to initial stresses.<br />

(4^- 25)<br />

By means <strong>of</strong> the fundamental equation given by eq. (19) the original<br />

problem has been transformed into a form relating nodal displacements<br />

linearly to forces that can be vizualized as located<br />

at the nodal points. As previously mentioned, an equation completely<br />

analogous to this equation and valid for the whole structure<br />

can be set up; introduction <strong>of</strong> the geometrical boundary<br />

conditions will then establish the final linear equation system

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