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    Optimization of Cable Tensioning in Cable-Stayed Bridges

    Le Hong Lam1Nguyen Huy Cung2Vu Hong Nghiep2

    1 Hohai UniversityNanjing210098

    2 Ho Chi Minh City University of TransportVietnam.

    [email protected]@yahoo.com

    AbstractDuring the structural analysis of cable-stayed bridges, some specific problems arise that are notcommon in other types of bridges. One of these problems is the derivation of an optimal sequence forthe tensioning of the stay cables. This paper describes a novel solution to this problem. Finite elementsare used for modeling the bridge structure. Numerical examples are presented, which illustrate the highobtainable accuracy of the method.

    Keywordscable-stayed bridgesoptimizationfinite elementcatenary cable element

    1. Introduction

    In the design cable-stayed bridge, an important step is determining the tensioning forces of stay

    cables to achieve a desired geometry of the bridge after construction, especially under the reaction of

    dead load. Many structural analysis techniques were proposed to solve this problem. The different

    models of cable have been investigated.

    The elastic cable is assumed to be perfectly flexible and possesses only tension stiffness; it is

    incapable of resisting compression, shear and bending forces. When the weight of the cable is neglected,

    the cable element can be considered as a straight member. But under action of its own dead load and

    axial tensile force, a cable supported at its end will sag into a catenary shape. The axial stiffness of a

    cable will change with changing sag. When a straight cable element for a whole inclined cable stay is

    used in the analysis, the sag effect has to be taken into account. On the consideration of the sag

    nonlinearity in the inclined cable stays, it is convenient to use an equivalent straight cable element with

    an equivalent modulus of elasticity, which can well describe the catenary action of the cable. The

    concept of a cable equivalent modulus of elasticity was first introduced by Ernst [1],[2],[5],[6]. This

    cable element has been used popularly in cable stayed bridge design.

    More accurate than cable element with an equivalent modulus of elasticity, some cable elements

    have been proposed such as nonlinear geometry cable element [4] proposed by the last of authors,

    nonlinear cable element [13] proposed by R.Karoumi, elastic catenary cable element with an unknown

    initial length [9].

    In this paper, the other model of cable is used for modeling cable in cable stayed bridge. When

    adjusting the cable, the length of cable changes, lead to the changing of sag. The horizontal component

    of cable tension is determined by using the built equations of the length of cable. From then on,determining the tensioning forces of stay cables under dead load to achieve a desired geometry of the

    bridge after construction.

    2. Proposed cable

    Consider the inclined cable AB of span l subjected to its own weight, having projection equal to w

    (Figure 1). Now, we build the equations of the length of cable. For the below expressions it is assumed

    that the cable is perfectly flexible and Hookes law is applicable to the cable material.

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    Figure 1: Geometry of the inclined cable

    The length of cable [1], [2]:

    3

    0 2

    0

    cos

    cos 2

    l DL

    H

    = + (1)

    Where

    2 32

    0

    012

    lw l

    D Q dz= = , Q is the simple beam shear force for given span l and H0 the

    horizontal component of cable tension.

    Let 0 be the elastic strain, we have [1]:

    ( )20 000 0

    1cos .

    l lH Hds tg ds

    EF EF

    = = +

    Where

    E : Youngs modulus of cable.

    F : Cross section area.

    : The inclination of the cable to the horizontal at any point.

    On the other hand,

    0

    Qtg tg

    H = +

    Hence

    ( )

    ( )

    2

    20 00

    00 0

    220

    2

    0 00

    2 20 0 0

    2

    0 00 0 0

    1 1

    1 2

    1 1. 1 . .2

    = + = + +

    = + + +

    = + + +

    l l

    l

    l l l

    H H Qtg ds tg ds

    EF EF H

    H Q Qtg tg ds

    EF H H

    H H Htg ds tg Qds Q ds

    EF EF H EF H

    (2)

    Because of

    0

    0l

    Qds= , (2) can be express:

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    0 00 2

    0

    .

    cos

    H l D

    EF EFH

    = + (3)

    If we skip the elastic strain of cable, the length of cable is:

    3' 0 0

    0 0 0 2 20 0

    .cos

    cos 2 cos

    H l Dl DL L

    H EF EFH

    = = + (4)

    When adjusting the cable, the position A changes to A due to the displacement of pylon Figure 2.

    Also, the original sag f0increase to f, the horizontal component of cable tension H0change to H. The

    expression of the length of cable can be written:

    '

    1 1 1L L = (5)

    Where

    L1: Length of cable.

    1 : The elastic strain.

    Figure 2: The inclined cable in working state.

    From the Fig.2-2, we see:

    3 31 1

    1 2 2

    1 0 0

    cos cos'

    cos 2 2

    D Dl uL A B

    H H

    = + = + (6)

    ( ) ( )2 2 2 2

    1

    2

    2 2

    ' 2 2 2 2

    1 2 1

    sin coscos

    = + = + =

    + + = =

    =

    A B d v l u d l vd ul AB vd ul

    vd ul vd ul vd ulAB AB AB

    AB AB AB AB

    lv u

    (7)

    And

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    1

    1 2 2

    22

    cos 1 1 1 1'

    cos 1 cos 1

    cos

    cos . 1 sin .cos cos .cos

    cos . 1 sin .co

    + +

    = = +

    + + + = +

    = + +

    = +

    l u u vd ul l u vd ull AB

    A B l AB AB l AB

    vd ul u vd ul u

    AB l ll

    v u u

    l l l

    v

    l

    ( )2

    2

    s cos 1

    cos . 1 sin .cos sin

    +

    = +

    u

    l

    v u

    l l

    (8)

    By substituting (7) and (9) into (6), we have:

    ( )3 3

    1 2 2

    cos . 3 cos .sin cos sin cos sin

    cos 2 2= + +

    l D DL v u v u

    H H l

    (10)

    The elastic strain:

    ( ) 20 12

    1

    2

    2

    2

    2

    2

    2

    .1 cos

    cos

    1 cos . 1 sin .cos sin

    2 21 1 sin .cos sin

    cos

    2 21 sin .cos sin

    cos

    = + = +

    = + +

    + +

    +

    H l u D H u Dl

    EF EFH EF l EFH

    H u v u Dl

    EF l l l EFH

    Hl u v u D

    EF l l l EFH

    Hl v u u

    EF l l l

    ( )2

    2

    1 sin 2 1 cos 2cos

    1 sin 2 cos 2cos

    +

    = + +

    = +

    D

    EFH

    Hl v u u D

    EF l l l EFH

    Hl v u D

    EF l l EFH

    (11)

    By substituting (10) and (11) into (5), we have:

    ( )3 3

    '

    1 2 2

    2

    cos . 3 cos .sin cos sin cos sin

    cos 2 2

    1 sin 2 cos 2cos

    = + +

    l D DL v u v u

    H H l

    Hl v u D

    EF l l EFH

    (12)

    Suppose that the cable doesnt elongate, then

    ' 1

    1 0L L= (13)

    By substituting (4) and (12) into (13), then transforming and reducing, we have:

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    ( )5 2

    3 2 3 20 002

    0 0

    22 5

    . . .cos .cos .1 sin 2 cos 2 .sin .cos .cos

    2. . .

    .cos .

    1 3 sin .cos 3 sin cos 02

    + + + +

    + + =

    E F D Dv u E F H H v u H

    l l l H l H l

    D E F v u

    H Dl l l l

    (14)

    By solving eq.(14) we can determine the horizontal component of cable tension H.

    3. Optimization cable tension under dead load

    The purpose is determined the tension of cable that satisfy two following conditions:

    i) The displacement of beam is zero.

    ii) The displacement of pylon is minimum.

    To analyze the cable stayed bridge, the pylon and girder are modeled using beam column

    element. The stay cables are replaced by nodal forces as shown in Figure 3.

    Figure 3: The stay cables are replaced by nodal forces.

    The nodal forces of stay cable are determined by the following formulas:

    1 3= =P P H (15)

    2

    2 tan2 8

    = +wl wl

    Pf

    (16)

    2

    4 tan2 8

    = wl wl

    Pf

    (17)

    P1

    P3

    P4

    P2

    Y

    Figure 4: The nodal force of cable.

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    The general form of the equilibrium equations are:

    [ ]{ } { }K u F= (18)

    Where

    [K]: The stiffness matrix of system.

    {u}: The nodal displacement vector.

    {F}: The force vector.

    `

    Figure 5: Procedure to optimize the tension of cables force:

    Begin

    Input the properties of cable stayed bridge

    Calculate [K], {F} with the

    beginning sag f0

    Solve the eq (18) to calculatevector {u}

    Solve the eq (14) to calculate H, then

    calculate vector {F} from (15),(16),(17)

    Solve the eq (18) to calculatevector {u}

    Check the condition:

    Max {u} [u]

    NO

    YES

    Calculate the initial cables force

    Export results.END

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    4. Numerical example

    In order to estimating the accuracy of this method, let us analyze the same problem which

    introduced in [7] and [9].

    4.1 Problem

    Consider a cable stayed bridge which the detailed geometry and the finite element model are

    shown in Figure 6. The material and sectional properties of stay cables, deck and pylons are shown in

    Table 1.

    Figure 6: Geometry of the cable-stayed bridge studied in example.

    Table 1. The material and sectional properties of stay cables, deck and pylons

    Member E(GPa) A(m2) I(m4) w(KN/m)

    Exterior cable 207 0.042 - 3.2

    Interior cable 207 0.016 - 1.2

    Girder 207 0.32 1.131 87.5

    Pylon (0.0-20.3m) 207 0.269 0.432 -

    Pylon (20.3-40.6m) 207 0.228 0.345 -

    Pylon (40.6-61.0m) 207 0.203 0.211 -

    The display of cable stayed bridge model using Matlab is shown in Figure 7.

    Figure 7: Calculating modeling of the system.

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    4.2 Numerical results

    4.2.1. Displacement of nodes

    Node Ux Uy Rz

    1 0.033200 0.000000 -0.000877

    2 0.025973 -0.000371 0.0002383 0.014000 0.000225 -0.000060

    4 0.000000 0.000000 0.000025

    5 -0.014000 0.000180 -0.000042

    6 -0.025867 -0.000322 0.000123

    7 -0.033842 0.000093 -0.000457

    8 -0.033842 0.000093 0.000457

    9 -0.041818 -0.000322 -0.000123

    10 -0.053685 0.000180 0.000042

    11 -0.067685 0.000000 -0.000025

    12 -0.081685 0.000225 0.000060

    13 -0.093658 -0.000371 -0.000238

    14 -0.100885 0.000000 0.000877

    15 0.000000 0.000000 0.000000

    16 0.000000 -0.022732 0.000000

    17 0.000000 -0.034466 0.000000

    18 0.000000 -0.047544 0.000000

    19 0.000000 0.000000 0.000000

    20 0.000000 -0.022732 0.000000

    21 0.000000 -0.034466 0.000000

    22 0.000000 -0.047544 0.000000

    4.2.2. Initial force components of elements

    Element Pi Pj Mi Mij Mj

    1 -1046.4336 -1046.4336 0.0000 570.2548 -

    1911.8732

    2 -1733.5221 -1733.5221 -1911.8732 -152.1121 -

    1444.7338

    3 -2026.9961 -2026.9961 -1444.7338 43.1139 -

    1521.42124 -2026.9961 -2026.9961 -1521.4212 -34.2901 -

    1599.5417

    5 -1718.1429 -1718.1429 -1599.5417 84.7407 -

    1283.3597

    6 -1154.8083 -1154.8083 -1283.3597 -296.8176 -

    2362.6583

    7 -0.0000 -0.0000 -2362.6583 350.5709 -

    2362.6583

    8 -1154.8083 -1154.8083 -2362.6583 -296.8176 -

    1283.3597

    9 -1718.1429 -1718.1429 -1283.3597 84.7407 -

    1599.5417

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    10 -2026.9961 -2026.9961 -1599.5417 -34.2901 -

    1521.4212

    11 -2026.9961 -2026.9961 -1521.4212 43.1139 -

    1444.7338

    12 -1733.5221 -1733.5221 -1444.7338 -152.1121 -

    1911.873213 -1046.4336 -1046.4336 -1911.8732 570.2548

    0.0000

    14 -2842.0370 -2746.3793 0.0000 0.0000

    0.0000

    15 -2746.3793 -2710.0464 0.0000 0.0000

    0.0000

    16 -2710.0464 -2677.5379 0.0000 0.0000

    0.0000

    17 -2842.0370 -2746.3793 0.0000 0.0000

    0.000018 -2746.3793 -2710.0464 0.0000 0.0000

    0.0000

    19 -2710.0464 -2677.5379 0.0000 0.0000

    0.0000

    20 1136.1296 1154.5049 0.0000 0.0000

    0.0000

    21 822.6040 828.9788 0.0000 0.0000

    0.0000

    22 486.8279 491.4248 0.0000 0.0000

    0.0000

    23 512.4597 517.0566 0.0000 0.0000

    0.0000

    24 673.8735 680.2481 0.0000 0.0000

    0.0000

    25 1254.7082 1273.0840 0.0000 0.0000

    0.0000

    26 1254.7082 1273.0840 0.0000 0.0000

    0.0000

    27 673.8735 680.2481 0.0000 0.0000

    0.0000

    28 512.4597 517.0566 0.0000 0.00000.0000

    29 486.8279 491.4248 0.0000 0.0000

    0.0000

    30 822.6040 828.9788 0.0000 0.0000

    0.0000

    31 1136.1296 1154.5049 0.0000 0.0000

    0.0000

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    4.2.3. Diagrams

    Figure 8: Displacement diagram.

    Figure 9: Axial force diagram.

    Figure10: Moment diagram.

    4.2.4. Remarks

    Displacement of deck is very small. The maximum displacement is 0.000371m (at node2 and node 13). Therefore, under dead load, the designed geometry of deck seems

    invariable.

    Due to the equilibrium condition of forces, displacements of pylons are almost equal zero. The present study and the study of Ki - Hae [9] exactly reproduce the target profile of the

    deck, while Wangs study [7] yields an inaccurate profile. The tensions of the stay cables

    in present study and the study of Kim-Lee are not considerably different but considerably

    different in Wangs study. This comparison is shown in Table 2 and Figure 11.

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    Table 2 The comparison

    Cable no.Present

    study

    Ki Haes

    study

    Wangs

    study

    Relative error

    between Present &

    Ki Hae

    Relative error

    between Present &

    Wang

    Relative error

    between Ki -

    Hae & Wang

    20 11.45 11.38 10.73 0.61% 5.71% 6.29%

    21 8.25 8.26 8.26 0.12% 0.00% 0.12%

    22 4.89 4.85 4.79 0.82% 1.24% 2.04%

    23 5.14 5.11 4.55 0.58% 10.96% 11.48%

    24 6.77 6.79 7.81 0.30% 15.02% 15.36%

    25 12.63 12.55 11.3 0.63% 9.96% 10.53%

    Force Unit: MN

    Figure 11: The comparison of three methods.

    5. Conclusion

    This paper presents the cable element to model the stay cables and procedure to solve an important

    problem in cable stayed bridge analysis. The numerical example is presented for demonstrating the

    validity and effectiveness of the proposed method in comparison to other methods in [7], [9]. Although

    this paper only presents the formulations and numerical example in the two-dimensional problem, the

    proposed method can easily extended to the three-dimensional problems.Its believed that this method

    provides the powerful tool for engineers in design of cable stayed bridge.

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    Reference

    [1]. MS Troitsky. Cable-stayed bridge theory and design. BSP Professional Books-1998.[2]. Le Dinh Tam, Pham Duy Hoa. Cable-stayed bridge. Science & engineering Press, 2001. (in Vietnamese).[3].Nguyen Viet Trung. Cable supported bridge. Construction Press, Hanoi 2004. (in Vietnamese).[4].Nguyen Huy Cung. Cable stayed bridge design. Engineering graduate thesis. University of Transportation2007. (in Vietnamese).

    [5]. Cable-Stayed Bridges-Developments Recent and Their Future. Developments in Civil Engineering-Vol.40.Elsevier[6]. Wang PH, Tseng TC, Yang CG.Initial shape of cable-stayed bridges. Computers & Structures Vols. 46. No.6. pp. 1095-I 106. 1993[7]. Pao-Hsii Wang, Hung-Ta Lin, Tzu-Yang Tang. Study on nonlinear analysis of a highly redundant cable-stayed bridge. Computers & Structures 80 (2002) 165182[8]. H. M. Alit and A. M. Abdel-Ghaffarf.Modeling the nonlinear seismic behavior of cable-stayed bridges withpassive control bearings.Computers & Structures Vol. 54. No. 3. pp. 461492, 1995[9]. Ki Seok Kim, Hae Sung Lee. Analysis of target configuration under dead load for cable stayed bridges.Computers and Structures 79 (2001).[10].D.W.Chen, F.T.K.Au, L.G.Tham, P.K.K.Lee. Determination of initial cable forces in prestressed concretecable stayed bridges for given design deck profiles using the force equilibrium method. Computers andStructures74. 2000.[11].J.H.O. Negrao, L.M.C Simoes. Optimization of cable stayed bridges with three dimensional modeling.Computers and Structures 64 (1997).[12].J.F. Debongnie. Fundamentals of finite elements.Les Editions de lUniversit de Lige, Lige, 2003, ISBN 2-93032254-3[13].Nguyen Hoai Son. FEM with Matlab. Ho Chi Minh National university publishing house, 2001. (inVietnamese).[14].Raid Karoumi.Response of Cable-Stayed and Suspension Bridges to Moving Vehicles-Analysis methods andpractical modeling techniques. Ph.D Thesis.[15].Zienkiewicz, O. C. and Taylor, R. L., The Finite Element Method, 5th edition, Butterworth-Heinemann, 2000.