3. Modeling A#

3.1. Characteristics of modeling#

_images/10001E70000069D500002D10A1C295348BA567FD.svg

3.2. Characteristics of the mesh#

Number of knots: 241

Number of meshes and type: 72 TRIA7

3.3. Tested values#

Identification

Instants

Reference

Aster

% difference

Limit point no. 1

DZ

1.03

—0.0140

—0.0140

—0.01322

—5.573

Eta_ PILOTAGE

1.03

1.0

0.9729

—2.471

Endpoint No. 2

DZ

1.78

—0.0171

—0.0171

—0.01696

—0.847

Eta_ PILOTAGE

1.78

0.375 0.250

0.07513

—75.96

Endpoint No. 3

DZ

2.3

—0.0140

—0.0140

—0.01458

4.176

Eta_ PILOTAGE

2.3

—0.400 —0.492

—0.533

19.67

Endpoint No. 4

DZ

2.48

—0.0161

—0.01617

0.452

Eta_ PILOTAGE

2.48

—0.633

—0.6442

1.717

3.4. notes#

The calculation strategy used is divided into two steps:

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

  • « imposed displacement » calculation: then, an imposed displacement is imposed using the technique of the arc length imposed on the entire structure (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 \(\mathit{DZ}\) 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 \(\mathit{DZ}\) in question.