Nonlinear Finite Element Analysis of Concrete Structures
Nonlinear Finite Element Analysis of Concrete Structures
Nonlinear Finite Element Analysis of Concrete Structures
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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