investigasi tentang perilaku dinamik alami dari struktur kurva akibat perubahan bentuk...

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  • 8/3/2019 Investigasi Tentang Perilaku Dinamik Alami Dari Struktur Kurva Akibat Perubahan Bentuk Kurva_Transportasi Mariti

    1/1

    The governing equations of dynamic behaviour of a curved beam is derived as follows:

    The solutions of eigenvalue are formulated as follows:

    The simplified perturbation equation is finally derived as follows:

    Considering the boundary conditions, the eigenvalue problem can be solved based on alat beam solution, where the transverse displacement is expressed as follows:

    where w h is the homogeneous solution of a flat beam and w p is the particular solutionontaining the curvature term

    Numerical Models

    B. HU

    School of Engineering Sciences, University of Southampton, UK

    An Investigation on the natural dynamic behaviours of curved structures affected bychanges in curvatures

    Fig, 1: FEM model of circular beam and s-shaped strip

    Various curved strips can be modelled based on a flat one if the curvature is a linear function of k = f ( s )

    Curved StructuresBackground

    Proposition

    Perturbation Approach

    SupervisorProf. J T Xing

    Prof. R A Shenoi

    Natural Vibration Numerical results agree with theoretical

    ones The curvature affects the natural

    frequency significantly The mode shape transition occurs when

    the curvature increases to a certainlarge degree

    The lower natural frequencies areaffected by the curvature much morethan the higher ones

    Fig. 2: Effect of the curvature on the natural frequency of a circular curved beam

    Fig. 3: Mode shape transi tions for the circular curved beam

    Applications

    Fig. 4: Effects of the curvature on the natural frequency of the composite laminat ed curved beams (a) circular beam (b) s-shaped strip

    Fig. 5: Lateral vibra tion mode shapes of (a) curved circular beam, (b) s-shaped strip

    Composite laminated curved beams S-glass/proxy [0/90]s, [0/90/90/0], [45/-45/-45/45]

    Mode shapes performing transition characteristics with the curvature increasing Curvature produces different effects on symmetric and anti-symmetric modes The ratio between the axial and bending stiffness decides the dynamic behaviour of

    the curved structure

    The curvature adjusts the spatial status, stiffness, stability and capacity of loading of curved structuresComplex curved structures are analyzed only by numerical approachesMore characteristics of dynamic behaviours need to be revealed and explained

    The perturbation approach is further developed to analyze curved beamsNovel applications for various curved beams and shells are suggestedCurved beams with different curvatures are modelled by the numerical method

    Conclusions

    Fluid Structure InteractionsResearch Group,

    School of EngineeringSciences

    ( ) ( )susun

    nn

    ==

    0

    ,

    ( ) ( )swswn

    nn

    ==

    0

    ,

    ( ) ( )ssn

    nn

    ==

    0

    ,

    = 1

    02

    4 sd wk k w

    sw

    ph www +=

    0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 0.50

    0.005

    0.01

    0.015

    0.02

    0.025

    Curvature parameter b( 1 /2)

    N o n - d

    i m e n s i o n a l f r e q u

    e n c y

    FEM symmetric modesAsymptotic curvesAnalytical result

    3rd symmetric mode

    2nd symmetric mode

    1st symmetric mode

    anti-symmetric modes

    Asymptoticcurves

    Subtended angle (degree)

    1.71

    7.64

    29.1

    0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.10

    2

    4

    6x 10

    -4 First symmetric mode

    Curvatureparameterb( 1 /2)

    N o n - d

    i m e n s

    i o n a

    l f r e q u e n c y

    [0/90/90/0][0/90/0/90][45/-45/-45/45]

    0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.90

    0.5

    1

    1.5

    2

    2.5x 10

    -3 First anti-symmetric mode

    Curvatureparameterb( 1 /2)

    N o n - d

    i m e n s

    i o n a

    l f r e q u e n c y

    [0/90/90/0][0/90][45/-45/-45/45]

    k =small parameter

    usw

    k wsk

    us

    k k wsu

    s

    2

    22 =

    ++

    +

    wsw

    k wsk

    us

    k wsu

    k =

    ++

    2

    22

    2

    2

    Curved beams with discontinued varying curvatures Based on the perturbation solution, a curved beam with various curvatures can be solved

    analytically

    Dynamic behaviour of two dimensional thin shell structures The energy method is adopted to obtain the analytical solution of the lateral vibration

    Fig. 6: Effects of the curvature on the natural frequency of a circular curved

    beam

    The lateral vibration The numerical study shows the natural

    frequencies of the lateral vibration changesfollowing the different curvatures

    It also shows the difference in mode shapesbetween the circular curved strip and the s-shaped strip