Global Strenght Analysis in Head Waves, for an Offshore...
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Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
Asian Business Consortium | AJASE ● Aug 2014 ● Vol 3 ● Issue 8 Page 73
Global Strenght Analysis in Head Waves, for
an Offshore Support Vessel
Mihaela Costache, & George Jagite
Naval Architecture Faculty, University "Dunarea de Jos" of Galati, Romania
ARTICLE INFO ABSTRACT Volume 3 Number 4/2014 Issue 8 DOI: 10.15590/ajase/ Received: Sep 14, 2014 Accepted: Sep 19, 2014 Revised: Sep 24, 2014 Published: Sep 26, 2014 E-mail for correspondence: [email protected]
The main topic of this paper is the 3D-FEM global strength analysis of a offshore supply vessel (OSV) under the following loads: still water and equivalent quasi-static head waves pressure, eigen ship and cargo weight. Two loading cases are selected for this analysis: full loading condition and ballast condition. The 3D-FEM (Finite Element Method) model extends over the whole ship length, the floating and trim equilibrium condition, in vertical plane, are obtained using eigen iterative numerical procedures. The buckling and yielding criteria are used to compare the numerical results with the allowable values according to classification societies. Key words: global ship strength, 3D-FEM, equivalent quasi-static head waves
Source of Support: European Union (“POSDRU/159/1.5/S/132397-ExcelDOC”),
Conflict of Interest: Declared.
How to Cite: Costache M and Jagite G. 2014. Global Strenght Analysis in Head Waves, for an Offshore Support Vessel Asian Journal of Applied Science and Engineering, 3, 73-88.
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INTRODUCTION
n order to increase the accuracy of the global strength analysis of ship structure, a major
step is to use the 3D-FEM full ship length models (Lehmann 1998, Rozbicki et al. 2001, Domnisoru 2006), instead of models extended only over several cargo holds (Hughes 1988,
Domnisoru 2001, Servis et al. 2003). In this study, the global strength analysis is carried on a offshore supply vessel, that operates in Black Sea. Two main loading cases are selected for this analysis (full loading condition and ballast condition) under equivalent quasi-static head waves. To obtain the equilibrium parameters eigen program codes (Jagite et Domnisoru 2014) are used. Siemens PLM - FEMAP software is used for preprocessing and post-processing and NX Nastran software is used to carry out the analysis.
I
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
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THE THEORETICAL MODELS FOR THE ANALYSIS OF SHIP STRENGTH
The main advantages of the 3D-FEM analysis compared as to the classical method based on 1D-girder models are:
the floating and trim equilibrium position is obtained at still water and equivalent quasi-static head waves, with no restrictions due to the ship hull form;
the 3D stress and deformation distributions are obtained, predicting the domains with higher risk;
compared as to the models developed on several cargo holds a reduced number of boundary conditions are used;
the real ship 3D structure is taken into account;
compared as to the 1D models, the 3D-FEM models include also the transversal structures which cannot be considered in 1D girder models, these are based only on longitudinal structures.
In the following are presented the main steps for the global strength analysis, based on 3D-FEM ship model, extended over whole length. The 3D-FEM mesh of the ship hull structure
The first step of the ship strength analysis includes the generation of the 3D-FEM-hull model. The mesh can be generated automatically, using auto-mesh options that are usual included in the FEM programs or it can be done manually. In the 3D-FEM models, all structural members have been modeled according to their original shape using the following types of elements:
plate element defined by four nodes each with six degrees of freedom;
bar elements defined by two nodes, six degrees of freedom per node;
mass elements defined by one node. The boundary conditions of the 3D-FEM model The next step of analysis includes the generation of the boundary conditions for the 3D-FEM hull model, Full extend over the ship length, that are of two types:
the vertical support condition at two nodes disposed at the ship hull structure extremities (on the central line), noted NDaft at aft end and NDfore at fore end;
due to the symmetry of the ship structure and the symmetry of the loads the model was developed only on one side and symmetry boundary conditions are applied at the nodes located on the central line of the ship;
The two nodes NDaft and NDfore are used as objective function at the veritical equilibrium conditions, at still water or equivalent quasi-static head waves, the vertical reaction force have to become zero. The loading conditions: The numerical analysis based on 3D-FEM model
This third step of the global strength analysis contains the modeling of the load conditions and the effective numerical structure analysis of the 3D-FEM model. The next type of loads acts over the ship hull structure:
the gravity load from the eigen hull structure weight and other mass components of the displacement (these masses are modeled with concentrated mass elements), except the cargo weight;
the cargo load, considered as local hydrostatic pressure over the ship structure;
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
Asian Business Consortium | AJASE ● Aug 2014 ● Vol 3 ● Issue 8 Page 75
the equivalent quasi-static wave pressure load for the following cases: hw=0 (still water) and hw≠0, according the statistical values from classifications societies (Bureau Veritas 2014), using an iterative procedure for the free floating and trim condition equilibrium, implemented with eigen program code (Jagite et Domnisoru 2014) developed in API (Femap programming interface). Figure 1 contains the flow chart of the eigen API program code.
The height of the equivalent wave is calculated according to Bureau Veritas Rules:
4.125
w Rw
Lh c
[m] for L<90m;
3/ 2300
10.75100
w Rw
Lh c
[m] for 90≤L≤300;
where Rwc = {1.00 9.00 0.75 0.66 0.60} is navigation coefficient.
Figure 1. Flow chart of eigen API program file
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
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The iterative procedure contains two main steps:
the free floating condition, having as objective numerical function the sum of vertical reaction forces at the two nodes, from the ship extremities,
3 3 3 0RT eq RT aft RT fore ;
the free trim and floating condition having as objective numerical function the vertical reaction forces at each two nodes, from the ship extremities,
3 0RT aft , 3 0RT fore ;
The numerical results evaluation This step of the global ship strength analysis based on 3D-FEM models is obtained the following numerical results:
the free floating and trim equilibrium parameters, draughts (average, aft draught and fore draught) and trim angle;
the stress and deformations over the whole ship hull length, and also the prediction of the higher risk domains.
Shear force and bending moment distribution along whole ship length is calculated with the following relation:
1.i i
t A R M
x nod x x
F i F nod F nod F nod
;
1.
.
.
i i
i Az Rz Mz
x nod x x
Ax Rx Mx Ay Ry My
M i nod x x F nod F nod F nod
nod z Z F nod F nod F nod M nod M nod M nod
;
where: FA - applied force; FR - force reaction; FM - multi force; MA - applied moment; MR - moment reaction; MM - multi moment; Z - elevation of reference plane to calculate the moment. The yielding ratio and buckling ratio were used as checking criteria. The yielding ratio is calculated according to Bureau Veritas Rules using eigen program codes.
VM
Master
YR
;
y
Master
R M
R
;
235yR
k ;
1/ 22 2 23VM x y x y ;
where k is the material coefficient (for grade A steel, Reh =235 N/mm2, k=1) and ,R M
are partial safety factors. The buckling ratio is calculated using SDC Verifier ver.3.6 software (www.sdcverifier.com). The buckling per panel is verified according to Det Norske Veritas rules for:
longitudinally uniform compression;
transverse compression;
shear forces;
biaxially loaded plates with shear.
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
Asian Business Consortium | AJASE ● Aug 2014 ● Vol 3 ● Issue 8 Page 77
THE OSV SHIP 3D-FEM MODEL
In this study is considered a offshore supply vessel (OSV) ship. The main dimensions of the ship are presented in Table I.
Table I. The OSV ship main characteristics Length overall LOA 62.20 m
Length between perpendiculars LBP 59.80 m
Breadth B 13.60 m
Draught T 4.50 m
Depth D 5.40 m
Service speed vs 11.00 knots
The two loading conditions selected for this study are: full loading condition and ballast condition. Hereafter are presented the mass distribution for each case and also the lightship distribution.
Figure 2. Lightship distribution
Figure 3. Full loading condition. Mass distribution
Figure 4. Ballast condition. Mass distribution
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
Asian Business Consortium | AJASE ● Aug 2014 ● Vol 3 ● Issue 8 Page 78
The 3D-FEM model was built according to classification societies rules, global coarse mesh with mesh dimension around 600 mm, one element between stiffeners. Three type of elements were used: plate elements, bar elements and mass elements.
Table II. The 3D-FEM model characteristic
Nodes 8435
Elements 17092
Properties 46
Materials 1
Figure 5. 3D-FEM model extending over whole ship length
Figure 6. 3D-FEM model - side shell
Figure 7. 3D-FEM model - main deck
Figure 8. 3D-FEM model - double bottom
Figure 9. 3D-FEM model - longitudinal bulkhead
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Figure 10. 3D-FEM model - transverse bulkhead and web frames
In the table III are presented the characteristics of the material used for 3D-FEM model, mild steel (grade A).
Table III. Material characteristics Young modulus 206000 N/mm2
Poison coefficient 0.3
Transversal modulus 79231 N/mm2
Density 7850 Kg/m3
Yield limit 235 N/mm2
The boundary conditions applied to the 3D-FEM model are presented in the Table IV. The TX, TY and TZ are the translation along X, Y and Z axis and the RX, RY and RZ are the rotations around X, Y and Z axis.
Table IV. Boundary conditions applied to 3D-FEM model Boundary condition TX TY TZ RX RY RZ
Center line symmetry PD X X
Aft node NDaft X X
Fore node NDfore X
Figure 11. Boundary conditions on 3D-FEM model
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
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Figure 12. Boundary conditions on extremities of the ship (aft - left, fore - right)
Numerical Analysis of the Global Strength of the Ship Hull The numerical analysis is focused on the global ship hull structure strength. The external equivalent quasi-static head waves pressure, with height hw=0-6m, 1m step is applied on the 3D-FEM model, using an iterative procedure for the vertical plane equilibrium condition. Based on Bureau Veritas Rules the equivalent quasi-static wave height for this ship is hw = 5.84 m. The 3D-FEM model is analyzed under equivalent wave loads both for wave crest and wave through. For each loading condition 15 load cases were analyzed, here after are presented the equilibrium parameters for full loading condition. Taft represents the aft draught and Tfore represents the fore draught.
Table V. Equilibrium parameters for full loading condition
Wave crest Wave through
Hw [m] Taft [m] Tfore [m] Taft [m] Tfore [m]
0.00 4.500 4.500 4.500 4.500
1.00 4.500 4.500 4.380 4.620
2.00 4.500 4.500 4.269 4.729
3.00 4.500 4.500 4.170 4.830
4.00 4.500 4.500 4.079 4.919
5.00 4.500 4.500 3.990 5.010
5.84 4.500 4.500 3.930 5.067
6.00 4.500 4.500 3.919 5.079
In the figures Figure 13 - Figure 16 are presented the shear force and the bending moment distribution along whole ship length for full loading condition (FL) for both wave crest and though. In the figures Figure 17 - Figure 28 are presented the yielding ratio and buckling ratio distribution along whole ship length for full loading condition(FL) for both wave crest and though.
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
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Figure 13. FL, shear force distribution, wave crest Figure 14. FL, shear force distribution, wave through
Figure 15. FL, bending moment distribution, wave crest Figure 16. FL, bending moment distribution, wave through
Figure 17. FL, Yielding ratio distribution on side shell, wave crest
Figure 18. FL, Yielding ratio distribution on side shell, wave through
Figure 19. FL, Yielding ratio distribution on main deck, wave crest
Figure 20. FL, Yielding ratio distribution on main deck, wave through
Figure 21. FL, Yielding ratio distribution on double bottom, wave crest
Figure 22. FL, Yielding ratio distribution on double bottom, wave through
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Figure 23. FL, Buckling ratio distribution on side shell, wave crest
Figure 24. FL, Buckling ratio distribution on side shell, wave through
Figure 25. FL, Buckling ratio distribution on main deck, wave crest
Figure 26. FL, Buckling ratio distribution on main deck, wave through
Figure 27. FL, Buckling ratio distribution on double bottom, wave crest
Figure 28. FL, Buckling ratio distribution on double bottom, wave through
Hereafter are presented the results obtained for ballast load condition. Table VI. Equilibrium parameters for ballast condition
Wave crest Wave through
Hw [m] Taft [m] Tfore [m] Taft [m] Tfore [m]
0.00 2.600 2.480 2.600 2.480
1.00 2.415 2.473 2.550 2.690
2.00 2.210 2.426 2.480 2.860
3.00 1.950 2.350 2.365 3.000
4.00 1.740 2.212 2.280 3.080
5.00 1.475 2.045 2.150 3.130
5.84 1.118 1.906 1.960 3.167
6.00 1.050 1.880 1.900 3.175
In the figures Figure 29 - Figure 32 are presented the shear force and the bending moment distribution along whole ship length for ballast loading condition (B) for both wave crest and though. In the figures Figure 33 - Figure 44 are presented the yielding ratio and buckling ratio distribution along whole ship length for ballast loading condition(B) for both wave crest and though.
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Figure 29. B, shear force distribution, wave crest Figure 30. B, shear force distribution, wave through
Figure 31. B, bending moment distribution, wave crest Figure 32. B, bending moment distribution, wave through
Figure 33. B, Yielding ratio distribution on side shell, wave crest Figure 34. B, Yielding ratio distribution on side shell, wave through
Figure 35. B, Yielding ratio distribution on main deck, wave crest Figure 36. B, Yielding ratio distribution on main deck, wave through
Figure 37. B, Yielding ratio distribution on double bottom, wave crest
Figure 38. B, Yielding ratio distribution on double bottom, wave through
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Figure 39. B, Buckling ratio distribution on side shell, wave crest Figure 40. B, Buckling ratio distribution on side shell, wave through
Figure 41. B, Buckling ratio distribution on main deck, wave crest Figure 42. B, Buckling ratio distribution on main deck, wave through
Figure 43. B, Buckling ratio distribution on double bottom, wave crest
Figure 44. B, Buckling ratio distribution on double bottom, wave through
For the equivalent quasi-static wave height hw = 5.84 m the yielding ratio and buckling ratio distribution is presented, for wave crest and through, both for full loading and ballast condition.
Figures 45 - 52, Full loading condition, wave crest;
Figures 53 - 60, Full loading condition, wave through;
Figures 61 - 68, Ballast condition, wave crest;
Figures 69 - 76, Ballast condition, wave through;
Full loading condition, wave crest, hw = 5.84 m
Figure 45. FL, wave pressure Figure 46. FL, vertical deflection [mm]
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Figure 47. FL, side shell - yielding ratio Figure 48. FL, side shell - buckling ratio
Figure 49. FL, main deck - yielding ratio Figure 50. FL, main deck - buckling ratio
Figure 51. FL, double bottom - yielding ratio Figure 52. FL, double bottom - buckling ratio
Full loading condition, wave through, hw = 5.84 m
Figure 53. FL, wave pressure Figure 54. FL, vertical deflection [mm]
Figure 55. FL, side shell - yielding ratio Figure 56. FL, side shell - buckling ratio
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Figure 57. FL, main deck - yielding ratio Figure 58. FL, main deck - buckling ratio
Figure 59. FL, double bottom - yielding ratio Figure 60. FL, double bottom - buckling ratio
Ballast condition, wave crest, hw = 5.84 m
Figure 61. B, wave pressure Figure 62. B, vertical deflection [mm]
Figure 63. B, side shell - yielding ratio Figure 64. B, side shell - buckling ratio
Figure 65. B, main deck - yielding ratio Figure 66. B, main deck - buckling ratio
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Figure 67. B, double bottom - yielding ratio Figure 68. B, double bottom - buckling ratio
Ballast condition, wave trough, hw = 5.84 m
Figure 69. B, wave pressure Figure 70. B, vertical deflection [mm]
Figure 71. B, side shell - yielding ratio Figure 72. B, side shell - buckling ratio
Figure 73. B, main deck - yielding ratio Figure 74. B, main deck - buckling ratio
Figure 75. B, double bottom - yielding ratio Figure 76. B, double bottom - buckling ratio
Asian Journal of Applied Science and Engineering ISSN 2305-915X(p); 2307-9584(e)
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CONCLUSIONS
Based on the numerical results, from the global strength analysis for the offshore supply vessel, it results the following conclusions:
the maximum vertical deflections are smaller as the admissible value for both loading cases (maximum vertical deflection is wmax = 65.95 mm < wadm = L/500 =119.6 mm);
the maximum value for yielding criteria, for full loading condition, 0.897 located on side shell, is lower than the admissible value, considering the maximum wave height hw =6m;
the maximum value for buckling criteria, for full loading condition, 0.827 located on side shell, is lower than the admissible value, considering the maximum wave height hw =6m;
the maximum value for yielding criteria, for ballast condition, 0.409 located on side shell, is lower than the admissible value, considering the maximum wave height hw =6m;
the maximum value for buckling criteria, for ballast condition, 0.551 located on main deck, is lower than the admissible value, considering the maximum wave height hw =6m;
using the 3D-FEM models, it makes possible to obtain the global stress distribution over the structure, predicting also the domains with higher risk.
ACKNOWLEDGEMENTS
The authors appreciated the support provided by the Prof. Dr. Leonard Domnisoru.
This work has been accomplished using NX Nastran FEMAP software, and has been funded by European Union under the project “POSDRU/159/1.5/S/132397-ExcelDOC”.
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Siemens PLM - FEMAP
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