4. B modeling#

4.1. Characteristics of modeling#

_images/100016B8000069BB00002957D4EF383703BEE0E2.svg

4.2. Characteristics of the mesh#

Number of knots: 169

Number of meshes and type: 36 QUAD9

4.3. Tested values#

Identification

Instants

Reference

Aster

% difference

Limit point no. 1

DZ

1.03

—0.0140

—0.0140

—0.01318

—5.886

Eta_ PILOTAGE

1.03

1.0

0.9724

—2.760

Endpoint No. 2

DZ

—0.0171

—0.01702

—0.462

Eta_ PILOTAGE

0.375 0.250

0.101

—67.69

Endpoint No. 3

DZ

—0.0140

—0.0140

—0.01446

3.269

Eta_ PILOTAGE

—0.400 —0.492

—0.558

25.177

Endpoint No. 4

DZ

—0.0161

—0.0161

—0.007

Eta_ PILOTAGE

—0.633

—0.640

1.120

4.4. notes#

The calculation strategy used is divided into two steps:

  • calculation under imposed load up to \(P=\mathrm{582.N}\) corresponding to 97% of the critical load,

  • imposed displacement calculation: then, an imposed displacement is imposed using the imposed arc-length technique (option LONG_ARC in STAT_NON_LINE).

Using the arc-length technique makes it difficult to define the reference value to be entered in the TEST_RESU command, since these values cannot be imposed. To define the reference values, we looked for the values of \(\mathrm{DZ}\) that were as close as possible to those listed in the table in [§2.2] and we reported the values of the control parameter that we had to obtain for the values of \(\mathrm{DZ}\) in question.