Brazil 2014ugm Imperfections in Structural Resistance of Submarines

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    Imperfections’ influence in the structural

    resistance of submarines

    Fabíola Tomasin

    Thiago Pontin Tancredi

    Departamento de Eng. Naval e Oceânica  –  PNV2512  –  05/12/2013

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    PRESENTATION TOPICS

    • Introduction and objectives

    • Shell buckling

     –  Analytical model;

     – Element finite model;

    • Shell with imperfections

     – Imperfections: shell not concentric;

     – Imperfections: oval conformation;

    • Conclusions

    Departamento de Eng. Naval e Oceânica

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    INTRODUCTION

    Departamento de Eng. Naval e Oceânica

    The objective of this work is to determine the influenceof the design parameters and defects (imperfections) in

    the collapse pressure of structure of submarine.

    ‘Submarine Design and development’ 

     Numerical evaluation of the buckling pressure of a

    submarine with imperfections in the structure.

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    CYLINDRICAL SHELL

    • External pressure

    • Buckling pressure is

    proportional to square of

    length

    Allen, H.G; Bulson, P.S. (1980)

    Analytical model

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    CYLINDRICAL SHELL WITH STIFFENERS

    • External pressure with rigidstiffeners

    • Buckling pressure is proportionalto square of distance betweenrings

    • The buckling is localized betweenthe rings with no deformation ofthem

    Allen, H.G; Bulson, P.S. (1980)

    Analytical model

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    CYLINDRICAL SHELL WITH STIFFENERS

    • External pressure with

    flexible stiffeners

    • Global buckling of the structure

    with deformation and rotation ofthe rings

    Allen, H.G; Bulson, P.S. (1980)

    Analytical model

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    RESULT COMPARISON: Buckling first mode

    • t = 0,021m;

    • l = 87,6m;

    • d = 5,4m;• E = 210 GPa;

    • ν =0,3

    Buckling pressure

    Departamento de Eng. Naval e Oceânica

    Cylindrical shell with axial pressure. Benchmark case

    Ansys Analytical

    7,8 * 108 Pa 9,9 * 108 Pa

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    RESULT COMPARISON: Buckling third mode

    • t = 0,021m;

    • l = 87,6m;

    • d = 5,4m;• E = 210 GPa;

    • ν =0,3

    Buckling pressure

    Departamento de Eng. Naval e Oceânica

    Cylindrical shell with external pressure. Benchmark case

    Ansys Analytical

    2,9 * 104 Pa 3,0 * 104 Pa

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    CASE OF STUDY: Sreelatha P. R. (2013)

    Departamento de Eng. Naval e Oceânica

    Stiffeners height 336 mm

    Stiffeners section area 12558 mm2 

    Web thickness 18 mmFlange thickness 28 mm

    Material Steel

    Coefficient of Poisson 0,3

    Benchmark case

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    RESULT COMPARISON: Global buckling 

    Simulation results Original results

    Departamento de Eng. Naval e Oceânica

    (SREELATHA P.R , 2013)

    Benchmark case

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    RESULT COMPARISON: Between stiffeners 

    Departamento de Eng. Naval e Oceânica

    (SREELATHA P.R , 2013)

    Benchmark case

    Simulation results Original results

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    ANALYSIS OF RESULTS

    The simulation results were close to the

    analytical results

    The simulation results were close to the

    benchmark case published in the literature

    Departamento de Eng. Naval e Oceânica

    Benchmark case

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    What are the motives for the differencesbetween the theoretical buckling pressureand the practical buckling pressure?

    Departamento de Eng. Naval e Oceânica

    • Initial deformation before the buckling;

    • Variation in constraints;

    • Imperfections in initial geometry;

    • Imperfections in material;

    • Imperfections resulted of the fabrication process.

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    IMPERFECTION: SHELL NOT CONCENTRIC

    Imperfections

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    IMPERFECTION: SHELL NOT CONCENTRIC

    Imperfections

    Buckling pressure (Mpa)  Distance between centers (mm) Distance between centers /

    original thickness Reduction % 

    27,9  0  0%  0 

    22,50  1,36  4%  19% 

    20,49 

    2,72  8%  26% 

    18,57  4,08  12%  33% 

    14,99  6,8  20%  46% 

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    14

    16

    18

    20

    22

    24

    26

    28

    30

    0% 5% 10% 15% 20% 25%

       B

       u   c    k    l   i   n   g   P   r   e   s   s   u   r   e    (   M   p   a    )

    Distance between centers / original thickness

    Buckling Pressure

    Buckling pressure (Mpa)  Distance between centers (mm) Distance between centers /

    original thickness Reduction % 

    27,9  0  0%  0 

    22,50  1,36  4%  19% 

    20,49 

    2,72  8%  26% 

    18,57  4,08  12%  33% 

    14,99  6,8  20%  46% 

    Imperfections

    IMPERFECTION: SHELL NOT CONCENTRIC

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    RESULTS: Oval conformation

    a (m)  % R  b (m)  a/b Buckling pressure

    (105 Pa) 

    Reduction % 

    4  0,0%  4,00  1,00  7,09  0% 

    4,04  1,0%  3,96  1,02  6,94  2% 

    4,08 

    2,0%  3,92  1,04  6,76  5% 

    4,12  3,0%  3,88  1,06  6,56  7% 

    4,16 

    4,0%  3,84  1,08  6,34  11% 

    4,32 

    8,0%  3,68  1,17  5,42  24% 

    5

    5,5

    6

    6,5

    7

    7,5

    0,95 1 1,05 1,1 1,15 1,2

       B   u   c    k    l   i   n   g   p   r   e   s   s   u   r   e    (   1   0   5   P   a    )

     a/b

    Buckling pressure

    Imperfections

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    Shell with stiffeners and oval deformation

    Stiffener buckling

    Buckling between stiffeners Global buckling

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    Shell With Stiffeners And Oval Deformation

    a (m) 

    b (m) 

    a/b 

    Buckling Pressure (107Pa) 

    Reduction %

    4,00  0,0%  4  1,00  2,634  0% 

    4,02  0,5%  3,98  1,02  2,558  3% 

    4,12 

    3,0%  3,88  1,04  2,308  12% 

    4,32 

    8,0%  3,68  1,06  1,718  35% 

    0

    0,5

    1

    1,5

    2

    2,5

    3

    0,95 1,00 1,05 1,10 1,15 1,20

       B   u   c    k    l   i   n   g   P   r   e   s   s   u   r   e    (   1   0   M   p   a    )

    a/b

    Shell with stiffeners and oval

    deformation

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    CONCLUSIONS

    There is a great sensitivity in buckling in function of the initialimperfections.

    With small reductions in thickness, the buckling pressure can

    decrease significantly.

    In the oval conformation, the thickness was kept constant so

    the influence of the a / b ratio was not so expressive.

    In fact, with the oval conformation, the thickness is variable

    and the influence is even bigger.

    Departamento de Eng. Naval e Oceânica

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    Thank you!Questions?

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    References

    • [1] A. GODOY, Thin Walled Structures with Structural Imperfections: Analysis and Behavior,L. Pergamon. Press, Oxford, U.K., 1996.

    • [2] BUCHER, Roy; RYDILL, Louis. Concepts in submarine design. Cambridge.New York:Cambridge University Press, 1994. Tese (de livre docência) em Engenharia Naval eOceânica. Escola Politécnica da Universidade de São Paulo. São Paulo.

    • [3] BUELTA, Miguel A. M.. Projeto do casco resistente de submersíveis. 1. ed.. São Paulo,1987.

    •  [4] GABLER, Ulrich. Projeto de submarinos. 1 ed.. Rio de Janeiro: Arsenal de Marinha,1991.

    • [5] ALLEN, H.G; BULSON, P.S. Background to Buckling. London New York : McGraw-HillBook Co. ,1980.

    •  [6] LEWIS, Edward V. Principles of Naval Architecture. 3. ed.. Jersey City: The Society ofNaval Architects and Marine Engineers, 1988.

    • [7] O Primeiro Humaita. Site utilizado: Visitado em 20/04/2013.

    • [8] SIMITSES, G. J., "Buckling and Post buckling of Imperfect Cylindrical Shells: a Review," Applied Mechanics Reviews, 39, 1517-1524 (1986).

    • [9] SREELATHA P.R et al. International Journal of Engineering Science and Technology(IJEST), 2010.

    Departamento de Eng. Naval e Oceânica

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