8. F modeling#

8.1. Characteristics of modeling#

We use a MEMBRANE modeling in large deformations (DEFORMATION =” GROT_GDEP “) with the Neo-Hookian law of behavior (RELATION =” ELAS_MEMBRANE_NH”). Bi-quadratic elements are used.

8.2. Characteristics of the mesh#

The mesh is the same as for C modeling.

8.3. Tested sizes and results#

The pressure applied during loading is tested.

Identification

Reference type

Reference value

Precision

Instant 0.1 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

109.55 \(N/{m}^{2}\)

8%

Instant 0.2 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

531.73 \(N/{m}^{2}\)

2%

Instant 0.3 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

995.8 \(N/{m}^{2}\)

2%

Instant 0.4 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

1276.2 \(N/{m}^{2}\)

2%

Instant 0.5 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

1366.9 \(N/{m}^{2}\)

0.7%

Instant 0.6 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

1344.7 \(N/{m}^{2}\)

0.6%

Instant 0.7 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

1280.6 \(N/{m}^{2}\)

0.4%

Instant 0.8 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

1203.0 \(N/{m}^{2}\)

0.3%

Instant 0.9 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

1124.4 \(N/{m}^{2}\)

0.1%

Instant 1.0 - \(\mathit{ETA}\text{\_}\mathit{PILO}\)

“SOURCE_EXTERNE”

1049.0 \(N/{m}^{2}\)

0.1%

_images/10000201000006CF00000512F0DBC90C32B5E7E4.png

Figure 6.2-a: Results of the D modeling vs numerical reference in figure 2.1 -a.

8.4. notes#

We used on-the-go piloting (SUIV_PILO) as for the D modeling.

With bi-quadratic cells, therefore of a higher order than the reference solution, the results remain as satisfactory as with the quadratic cells of the E modeling.