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Nonlinear Finite Element Analysis of Concrete Structures

Nonlinear Finite Element Analysis of Concrete Structures

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- 69 -<br />

1^<br />

1 = 2A 4T<br />

b.<br />

i<br />

c.<br />

i<br />

b 5<br />

c .<br />

a. c. z a. c.z a cz<br />

_Ln,.+_L_ o -i + b.+-J- O -^+b +-Sr<br />

i r r i r r m r<br />

b.<br />

i<br />

c.<br />

m<br />

m<br />

m<br />

(4.2-7)<br />

O<br />

b<br />

m<br />

It appears that all strains except the tangential strain are constant<br />

within an element. However, in the present report this<br />

variation <strong>of</strong> the tangential strain is ignored and instead, as an<br />

approximation, the value at the centroid <strong>of</strong> the element is applied.<br />

The stresses are given by the vector.<br />

a =<br />

hi<br />

°R<br />

a e<br />

(4.2-8)<br />

T RZ<br />

with obvious notation. The usual elastic constitutive equation<br />

is assumed to hold, i.e.<br />

a = D (e - e )<br />

o<br />

(4.2-9)<br />

where D is a (4x4) symmetric matrix termed the constitutive or<br />

material matrix and é<br />

o<br />

is a vector containing initial strains<br />

due to temperature. As the strains within an element are constant<br />

the same follows for the stresses. It is here assumed that<br />

the D-matrix may depend on the stress state and time. For an<br />

isotropic material we have<br />

J<br />

D = (1 + v) (1 - 2v)<br />

1-v v v<br />

v 1-v v<br />

V V 1-V<br />

0 0 0<br />

0<br />

0<br />

0<br />

1 - 2v<br />

(4.2-10)<br />

where E and v are Young's modulus and Poisson's ratio, respectively,<br />

that might depend on the stress state and time. The change

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