3. Modeling A#

3.1. Characteristics of modeling#

439 POU_D_T

3.2. Characteristics of the mesh#

Number of knots: 440

Number of meshes and type: 339 SEG2 and 6 SEG2 (DIS_T)

Note:

Care must be taken to correctly order the groups of nodes on which temperature measurements and average calculations are carried out.

3.3. Tested sizes and results#

In order to correctly validate the fatigue calculation, it is ensured that the results of the mechanical calculations are sufficiently close to the reference.

Natural frequencies of the empty line:

Mode Number

Reference

Aster

\(\text{\%}\) difference

1

5.059

5.05799

0.02

2

6.023

5.98255

0.67

3

6.866

6.86007

0.09

4

8,204

8,20337

0,01

5

9.733

9.73339

0.00

6

9.987

9.95736

0.30

7

16.535

16.4647

0.43

8

17,329

17,326

0.02

9

18.282

18.2823

0.00

10

19.004

18.996

0.04

11

20,271

20,2708

0,00

Efforts (moments) at node N1

NO. 1

Reference

Aster

\(\text{\%}\) difference

Charging case

\(\mathit{Mx}\) (\(\mathit{N.m}\))

\(\mathit{My}\) (\(\mathit{N.m}\))

\(\mathit{Mz}\) (\(\mathit{N.m}\))

\(\mathit{Mx}\) (\(\mathit{N.m}\))

\(\mathit{My}\) (\(\mathit{N.m}\))

\(\mathit{Mz}\) (\(\mathit{N.m}\))

\(\mathit{Mx}\)

\(\mathit{My}\)

\(\mathit{Mz}\)

1

5947

4412.5

—5526

5985.5

4440.76

—5561.92

—0.65

—0.64

—0.65

2

—41084

—25691

91767.3

—41041.6

—25659.6

91727.2

0.10

0.12

0.04

3

—34253

—20695.4

83346.2

—34212.8

—20665.9

83307.7

0.12

0.14

0.05

5

—32752

—19577

81995.4

—32802.8

—19615.8

82041.5

—0.16

—0.20

—0.06

5

—40330

—25129

91089.6

—40335.5

—25133.6

91094.1

—0.01

—0.02

0,00

6

—34565

—20927.8

83624.6

—34565.3

—20928.5

83624.3

0,00

0,00

0,00

7

—42718

—26884

93803.2

—42664.3

—26845.2

93752.5

0.13

0.14

0.05

8

—38457

—23711

89984.4

—38426.1

—23688.3

89954

0.08

0.10

0.03

10

—43556

—28408.2

86848.7

—43537.4

—28394.9

86830

0.04

0.05

0.02

12

—44175

—28868.5

87403.1

—44232.3

—28912.1

87456.1

—0.13

—0.15

—0.06

14

1381

5671

—3179

1370

5700

—3320

0.59

—0.54

—4.45

Reference

N 1

Aster

\(\text{\%}\) difference

\(\mathit{Mx}\) (\(\mathit{N.m}\))

\(\mathrm{\mid }\mathrm{\mid }{\mathit{Mx}}^{2}+{\mathit{My}}^{2}\mathrm{\mid }\mathrm{\mid }\)

Charging case

\(\mathit{Mx}\) (\(\mathit{N.m}\))

\(\mathrm{\mid }\mathrm{\mid }{\mathit{Mx}}^{2}+{\mathit{My}}^{2}\mathrm{\mid }\mathrm{\mid }\)

Diff \(\mathit{Mx}\)

Diff \(\mathrm{\mid }\mathrm{\mid }{\mathit{Mx}}^{2}+{\mathit{My}}^{2}\mathrm{\mid }\mathrm{\mid }\)

240269

108501

Earthquake

239009

108167

0.52

0.31

Thermal calculations:

Reference

Aster

\(\text{\%}\) difference

Thermal transient

_images/Object_8.svg

\(°C\)

_images/Object_9.svg

\(°C\) right side

2

0.741

0.719

3

6

15.48

15.38

3

Reference

Aster

\(\text{\%}\) difference

Thermal transient

_images/Object_10.svg

right side

_images/Object_11.svg

right side

2

1.043

1.8

73

6

5.99

9.34

56

Reference

Aster

\(\text{\%}\) difference

Thermal transient

_images/Object_12.svg

elbow side

_images/Object_13.svg

elbow side

2

1.445

2.4

65

6

5.69

8.8

54

Note:

Average temperatures are relatively different from the reference. This may be due to modeling (here axisymmetric, and \(\mathrm{3D}\) in [bib2]). In practice, only the mean temperature difference between the elbow and the straight pipe is used in the stress calculations.

Finally, the total cumulative use factor is equal to:

Reference

Aster

\(\text{\%}\) difference

Knot/Knit

Use Factor

Use Factor

\(\mathit{N80}\), \(\mathit{M1}\)

0.00648

0.00648

0.0079

22