1. Reference problem#

1.1. Geometry#

This non-regression test case represents a three-point test of a thick beam. The beam is represented by a rectangular element 7.5 meters long and 4.7 meters high. The element contains a square hopper with a side of 1.5 meters located according to Figure 1.1.-a. A fixed support is placed at the left end of the base of the element and a vertical support is considered to be placed at the right end. A vertical load equal to 3 MN is applied in the direction of gravity at 4.7 meters from the left edge. The geometry, boundary conditions, and material definitions were taken directly from the reference [Shlaich et al., 1987].

P=3 MIN

_images/10000000000001FF0000018415022DC70A8F7BD4.png

Image 1.1-1: Sail girder with hopper

1.2. Materials#

The reinforced concrete used for plane modeling corresponds to a linear elastic material with the following characteristics:

Concrete:

Young’s modulus

\(E\)

21 GPa

Poisson’s Ratio

\(\nu\)

0.2

Elastic limit

\({f}_{\mathit{cm}}\)

36 MPa

Table 1.2-1

Reinforcing steel:

Young’s modulus

\(E\)

210 GPa

Elastic limit

\({f}_{y}\)

500 MPa

Table 1.2-2

1.3. Boundary conditions and loading#

The beam is assumed to have a fixed support at the level of the left side and a carriage-type support (locked in the vertical direction) at the level of the level of the right side. The load and boundary conditions are taken as shown in Figure 1.1-1.

1.4. Characteristics of the mesh#

Number of knots: 13504

Number of meshes and types: 13200 meshes QUAD4

1.5. Benchmark solution#

1.5.1. Diagram of the Bielles-Tirants truss#

One of the solutions proposed in reference [Schlaich et al., 1987] is shown in Figure 2.1-a. The author approaches the problem via an ad hoc definition of the Bielles-Tirants model.

_images/100000000000020D0000017E1C570449EE3CD749.png

Figure 1.5-1: BT reference model [Shclaich et al., 1987]

1.5.2. Benchmark results#

The tie rod sections are shown in the following table:

Pulling

Knot i

Knot j

Force [MN]

Length [m] *

As [m2]*

T2

5

6

1.33

1.33

5.6

0.0024

T1

0

5

1.07

1.07

3

0.0027

Table 1.5-1: Tie rod sections [Shclaich et al. 1897]