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Investigating the Effects of Crack Orientation and Defects on Pipeline Fatigue Life Through Finite Element Analysis Cover

Investigating the Effects of Crack Orientation and Defects on Pipeline Fatigue Life Through Finite Element Analysis

Open Access
|Apr 2024

Figures & Tables

Figure 1.

Mesh of the pipe.
Mesh of the pipe.

Figure 2.

Stress distribution Syy in the case of a) longitudinal (axial) crack, b) circumferential (transversal) crack.
Stress distribution Syy in the case of a) longitudinal (axial) crack, b) circumferential (transversal) crack.

Figure 3.

J-integral versus crack length.
J-integral versus crack length.

Figure 4.

Stress intensity factor KI versus crack length.
Stress intensity factor KI versus crack length.

Figure 5.

Stress intensity factor KII versus crack length.
Stress intensity factor KII versus crack length.

Figure 6.

An organogram of fatigue life prediction in AFGROW.
An organogram of fatigue life prediction in AFGROW.

Figure 7.

Geometrical parameters of semi-elliptic crack and pipe.
Geometrical parameters of semi-elliptic crack and pipe.

Figure 8.

Evolution of the crack depth a and crack length c according to the number of cycles N (t = 3 mm).
Evolution of the crack depth a and crack length c according to the number of cycles N (t = 3 mm).

Figure 9.

Evolution of the crack depth a and crack length c according to the number of cycles N (t = 4 mm).
Evolution of the crack depth a and crack length c according to the number of cycles N (t = 4 mm).

Figure 10.

Evolution of the crack depth a and crack length c according to the number of cycles N (t = 5 mm).
Evolution of the crack depth a and crack length c according to the number of cycles N (t = 5 mm).

Figure 11.

Evolution of the crack depth a and crack length c according to the number of cycles N (t = 6 mm).
Evolution of the crack depth a and crack length c according to the number of cycles N (t = 6 mm).

Figure 12.

Evolution of the crack length c according to the number of cycles N for different ratios a/t.
Evolution of the crack length c according to the number of cycles N for different ratios a/t.

Figure 13.

Evolution of the relative crack depth a/t according to the number of cycles N.
Evolution of the relative crack depth a/t according to the number of cycles N.

Figure 14.

Evolutionof the aspect ratio a/c according to the number of cycles N.
Evolutionof the aspect ratio a/c according to the number of cycles N.

Figure 15.

Evolution of the crack depth and length crack (a and c) according to the number of cycles N(Do = 350 mm)
Evolution of the crack depth and length crack (a and c) according to the number of cycles N(Do = 350 mm)

Figure 16.

Evolution of the crack depth and length crack (a and c) according to the number of cycles N (Do = 345 mm)
Evolution of the crack depth and length crack (a and c) according to the number of cycles N (Do = 345 mm)

Figure 17.

Evolution of the crack depth and length crack (a and c) according to the number of cycles N (Do = 340 mm)
Evolution of the crack depth and length crack (a and c) according to the number of cycles N (Do = 340 mm)

Figure 18.

Evolution of the crack depth and length crack (a and c) according to the number of cycles N (Do = 335 mm)
Evolution of the crack depth and length crack (a and c) according to the number of cycles N (Do = 335 mm)

Figure 19.

Evolution of outside diameter of pipe Do as a function of number of cycles N.
Evolution of outside diameter of pipe Do as a function of number of cycles N.

Figure 20.

Evolution of the crack depth and length (a and c) according to the number of cycles N for different values of internal pressure.
Evolution of the crack depth and length (a and c) according to the number of cycles N for different values of internal pressure.

Figure 21.

Internal pressure versus number of cycles N.
Internal pressure versus number of cycles N.

Test simulation conditions with different values of relative depth a/t_

TestDo mmDi mmt mma/t
135034430.30
235034240.25
335034050.20
435033960.16

Mechanical properties of X52 steel_ (Harter, 2002; NASA, 2001)

Young’s modulus E (MPa)200
Poisson’s ratio υ0.30
Yield stress σY (MPa)410
Ultimate tensile stress σUTS (MPa)498
Elongation εf (%)35
Toughness fracture (Mpa.mm1/2)95
Threshold (MPa.mm1/2)7

Tests simulation conditions with different values of outer diameter Do_

TestDo mmDi mmt mma/t
135034050.2
234533550.2
334033050.2
433532550.2

Tests simulation conditions with different values of aspect ratio a/c_

TestDepthLengthAspect ratio
a mmc mma/c
1111
211.20.83
311.40.71
411.60.62
511.80.55
6120.50

Mechanical properties of X52 steel for NASGROW model_ (Harter, 2002; NASA, 2001)

Young’s modulus E (MPa)200
Poisson’s ratio υ0.30
Yield stress σY(MPa)410
Ultimate tensile stress σUTS(MPa)498
Elongation εf (%)35
Toughness fracture Kc (Mpa.mm1/2)95
Threshold Kth (Mpa.mm1/2)200
p0.65
q0.001
C1.15e-10
n2.41
DOI: https://doi.org/10.2478/fas-2023-0001 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 1 - 21
Published on: Apr 29, 2024
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2024 Tayeb Kebir, Mohamed Belhamiani, Ahmed Amine Daikh, Mohamed Benguediab, Mustapha Benachour, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.