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Nonlinear Finite Element Analysis of Concrete Structures

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- 84 -<br />

evdn though some features <strong>of</strong> dowel action are indeed reflected,<br />

the approach is in general not preferable.<br />

As concrete and reinforcement is assumed _o follow each other,<br />

the full shear capacity <strong>of</strong> the bars is to be considered. While<br />

this assumption is fair for uncracked regions, it is obvious that<br />

as a result <strong>of</strong> cracking relative deformations parallel to the<br />

crack plane will be localized to the vicinity <strong>of</strong> the crack where<br />

local bending <strong>of</strong> the reinforcement is initiated and where local<br />

crushing <strong>of</strong> the concrete may be present. As a result, the stiffness<br />

<strong>of</strong> the bar parallel to the crack plane is considerably<br />

lower than that given by the original shear stiffness. This effect<br />

can be accounted for in the program by using the term KG<br />

where 0 < K < 1 instead <strong>of</strong> the original shear modulus G <strong>of</strong> the<br />

reinforcement material. Due to simplicity we employ a constant<br />

K-value and as the shear capacity <strong>of</strong> reinforcement bars is insignificant<br />

when no cracking is present a realistic K-value<br />

might be determined by means <strong>of</strong> calibration calculations on a<br />

structure where cracking and dowel action dominate the response.<br />

Such calculations are performed in section 5.1 and, as previously<br />

mentioned, it is found there that neglect <strong>of</strong> dowel shear, i.e.,<br />

K = 0, constitutes in fact the most preferable value. This finding<br />

is supported by the calculations in section 5.3. Consequently,<br />

except for certain sensitivity studies the value K = 0<br />

is always employed in the program.<br />

The objective <strong>of</strong> the following considerations is to determine<br />

the stiffness contributions <strong>of</strong> reinforcement eleme^s to the involved<br />

triangular elements. In section 4.3.1 only linear material<br />

response is considered. Section 4.3.2 then treats the necessary<br />

modifications when plastic strains develop. Moreover, when temperature<br />

stresses are present the contribution from the reinforcement<br />

to the nodal forces <strong>of</strong> the involved triangular elements<br />

are also determined in section 4.3.1.<br />

4.3.1. Elastic deformation <strong>of</strong> reinforcement<br />

Every reinforcement bar is located along an arbitrary straight<br />

line. From the start and end point <strong>of</strong> each bar a special search

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