2015
DOI: 10.1016/j.marstruc.2015.10.001
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Theoretical and numerical analysis of bending behavior of unbonded flexible risers

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Cited by 27 publications
(8 citation statements)
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“…The stress at critical point of helical wire is highly concerned in the fatigue assessment of flexible riser. Figure 7 demonstrates the comparison of the axial stress calculated from the present model and the detailed finite element model under initial contact pressure [23]. It can be seen that under the bending moment of 140 NÁm, the helical wires keep full-sticking, and the result shows good agreement.…”
Section: Riser-seabed Interaction Modelmentioning
confidence: 86%
“…The stress at critical point of helical wire is highly concerned in the fatigue assessment of flexible riser. Figure 7 demonstrates the comparison of the axial stress calculated from the present model and the detailed finite element model under initial contact pressure [23]. It can be seen that under the bending moment of 140 NÁm, the helical wires keep full-sticking, and the result shows good agreement.…”
Section: Riser-seabed Interaction Modelmentioning
confidence: 86%
“…Since the geometric nonlinearity is strong within the riser model, the explicit solution method is applied to avoid non-convergence in the numerical simulation. Since it is difficult to define the accurate contact between and within interlayers, general contact is thus applied to define the nonlinear contact, where the tangential behavior is simulated by using the Coulomb friction model [25] and the corresponding frictional coefficient is 0.1 [37], while the normal contact is set to hard contact. Two reference points, RP1 and RP2 (see Figure 4), are set at the geometric center of the top and end cross-section and all the layer's nodes at the edge of the cross-section are kinematically and rigidly bounded onto the two reference points, thus applying the boundary conditions and external loads.…”
Section: Model Verificationmentioning
confidence: 99%
“…The proposed numerical can effectively simulate the inter-layer and intra-layer contact and friction, and therefore can be used to calculate the cross-sectional mechanical properties of an unbonded flexible riser under axisymmetric and bending loads. Zhang et al [25] also developed a numerical model containing detailed geometries, and all layers of the structure were also simulated using body cells to analyze the structural response under the combined effects of external pressure and bending moments. Yoo et al [26,27] established a carcass layer with detailed geometrical characteristics through ANSYS software (https://www.ansys.com/, accessed on 7 May 2024), and simplified it into an equivalent cylindrical shell layer by analyzing the mechanical failure characteristics of the carcass layer under the action of axial force, and established an equivalent simplified eight-layer numerical model and a five-layer numerical model; at the same time, they considered the effect of the shell unit or the body unit in simulating the cylindrical shell layer, and investigated the axial load-bearing capacity of the unbonded flexible riser.…”
Section: Introductionmentioning
confidence: 99%
“…Few studies have carried out research on the cross-sectional mechanical properties of unbonded flexible risers under bending loads using this method. Among them, Zhang et al [ 121 ] took a class of eight-layer 2.5-inch unbonded flexible risers as the object of study, and simplified the cross-sectional mechanical structure of the carcass layer and the pressure armor layer to some extent (shown in Figure 19 ). The mesh of the regular cylindrical shell layers was divided into large elements.…”
Section: Development Of Cross-sectional Properties Of An Unbonded Fle...mentioning
confidence: 99%