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    Vol.49 No.4 199714) SEISAN KENKYU 239

    l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l

    Application of Biological-Growth Strain Method on

    TaketO UO 10TO*

    Ef ct e Strcss Poillt

    M a x M i l l l i l i D n n

    Fig. 1 Illustration for curvature

    based Baud's postulation

    Design 'rotlle

    - optilnai- : Intemrediate- Initial

    variation on the design profile

    demonstration3). ased on this validated Baud's postula-

    ulated by Baud showed ts practical validation by analytical

    demonstration3). ased on this validated Baud's postula-

    tion, the stress optimal design can be achieved y varying

    the outer-surface hape i.e. curvature of the design points

    along the design profile) of the design structure. By

    iteratively repeating he above process, he outer-surface

    shape can be considered o be optimized once if the'

    condition Eq. (1) is satisfied. The iterative optimization

    process an be illustrated by Fig. 1. On the other hand, by

    looking at the load carriers n animals r plants ike bones or

    brunches, t is undoubtedly convinced hat the load carriers

    develop heir optimum by well adapting hemselves o their

    environment at a certain loading conditions4). With the

    further inspect on those biological adaptation process'

    several interesting aspects can be summarized n the

    following points; (1) the state of constant stress can be

    found on the surface of those well-adapted biological

    structures nd (2) the adaptation process f these biological

    tissues s carried out by growth or atrophy of their live

    tissues ear the stress-concentrated urface. By comparing

    these observed acts on the biological adaptation process

    with stress optimal design process, t is not difficult to find

    out the high simitarity between them on the optimality

    Optimal Shape Design of Mechanical Components

    Kai Lin HSU*and

    1 . INTRODUCTION

    By the notch stress heory developed by Baudl) and

    Schack2), tc., the shape optimization problem of minimiz-

    ing stress concentration n the continuous structures also

    termed as stress optimal design) can be focused on the

    adjacent area where stress oncentration ccurs n stead of

    dealing with the whole design tructure. On the other hand,

    from the comparative viewpoint on the mechanism of

    minimizing stress ioncentration, it is found that the

    adaptation rocess f biological issues y shape ariation o

    their environment is very effective in reducing stress

    concentration n the biotogical structures. The high simi-

    larity between the biological adaptation process and the

    stress ptimal design n the continuous tructures motivated

    us to present one new optimal shape design method based

    called biological-growth train method (BGS) by simulat-

    ing biological adaptation process.

    In the following, the characterjstics f BGS will be given

    in section ; then, he numerical erification of the proposed

    method and application n various ields of structural design

    are llustrated n section 3. Finally, the concluding emarks

    is included in section 4.

    2. CHARACTERISTICS F BIOLOGICAL.GROWTH

    STRAIN METHOD

    (1) Similarity etween stress optimal design and biolo-

    gical adaptation process

    Through years of researches, uniform stress istribution

    design (or equi-strength design) -the hypothesis post-* 5th Deputtment, Institute of Industrial Science, University of

    Tokyo

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    240 V01.49 No.4 1997.4) SEISAN KENKYU

    condition and the optimization process. Here, it is worthmentioning hat the gradients or objective unction and heconstraint conditions s usually necessary or the conven-tional stress ptimal design while the biological optimizationprocess eeds no gradient nformation. As a result, it wasmotivated o propose one gradientless tress ptimal designmethod by simulating he biological adaptation process oupdate the design variables nstead of using the gradientoptimization techniques.

    In fact, the derivation of BGS is similar to ,,initial stressmethod , i.e. the shape updating of the design structure san iterative process which consists of two stages: (i)generation of fictitious strain by some built-in rules (e.g.nonlinear constitutive elationship or the biological growthrules) and (ii) production of fictitious external oads by thegiven fictitious strain. In stage i), due to the definition ofthe fictious strain derived rom the simulation on biologicaladaptation, t is termed as the biological-growth train. Inthe followings, irst of all, the concept and the definition ofthe biological-growth train s given; hen, the algorithm orthe production of the fictious external loads termed as biological-growth strain analysis s derived.

    (2) Brief Description on Biological-Growth train MethodIn order to optimally design he shape of the structure,

    one optimal shape design method proposed y the authorss)was utilized to design he structures. Compared o otherconventional tructural optimization echnique, he featureof this proposed method was its ignorance on gradientcalculation, which could be regarded as he dominant actoron increasing he computational ost of structural optimiza-tion. The design objective of this rnethod s to minimize thestress oncentration within the design structure; which canbe expressed as

    called biological growth strain was defined as follow

    i0) , if element f *

    _ 21

    dghal ,hap0

    3

    { Ph PL for dectile material:

    #+

    yh, if element e I*

    Here, the design variables are the coordinates x1, 1)ofthe design oints selected long he design rofile -, where: 1..n. The reference tress s &; s nd the equivalent tressalong -is q. The algorithm of this method was proposed ysimulating the biological adaptation to their loadingenvironment like trees or bones; i.e. they change heirshapes y the growth or trophy of the living tissue near thehigh stressed rea. Based on this concept, one pararneter

    Calcula

    8Fig.2 COmputatiO,al low Of BGS

    br b e matc 1 7h,r demcd jc121

    Here j: jth design element within design domain f *; oi :

    equivalent stress within jth design element; omear,t mean ofequivalent stress of all the design elements; o1: kth principal

    stress, k:1..2; fr: uniaxial compressive or tensile strength;Vh: constant for search step. With the introduction of this

    parameter, the shape of the design structure can be changed

    by means of updating vectors of nodes coordinates (i.e. th e

    shrinking or swelling of the design elements), which is

    formulated as

    [r]{ }: {4e} (3)

    Here [K]: global stiffness matrix and {rr}, nodalcoordinate updating vectors. The equivalent nodal forcevector {dg} is

    {ae} :/o

    [B]' [D]{#}a O@)

    That'is, he nodal coordinate updating vectors u} can beattained by solving he global governing equation superim-posed by Eq. (3) without figuring out the gradient of theobjective unction or constraint conditions. Therefore, he

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    SEISAN KENKYUVol.49 No.4 1997.4)

    new shape of the structure s obtained by adding he nodal

    coordinate updating ectors o the old coordinates f nodes.

    For brevity, the computational low of BGS is llustrated n

    Fig.2. The termination of this terative computation an be

    recognized when Eq. (1) is satisfied.

    3. NUMERICAL ERIFICATION ON CORRECTNESS

    OF BGS

    After explaining haracteristics f BGS, the availability of

    this method s necessary o be verified before applying his

    method to general structures. To verify the availability of

    this method, the design problem to find out the optimal

    shape of the hole in a plate under biaxial stress was

    considered. According to the elasticity theory6), the

    tangential stress or the elliptical hole in an infinite plate

    under biaxial stress s siven as

    oe : o l

    Here, k:

    transversalintroduction

    rewritten as

    axis ratio (:bia; b: vertical axis and a:

    axis) and 0: directional angle. With the

    of the assumption 2/o1:k, Eq. (5) can be

    follow

    n, rigraF4

    J

    =2

    J=

    ,

    (b) rectangle hole

    Fig.3 Sketch of FEM model for the hole in an infinite plate

    under biaxial stress with different initial shapes

    b)CaSe Bl

    Fig.4 0ptimalshapes and EQS designed by BGS P/Q=1)

    Table 2 Loading conditionand case abel

    PiQ A B1 Al Bl

    1:2 Z B2

    = l 1+k)2 sin2 k 1+k)2 cos2

    _k2_k

    sin2 +k2cos2

    : (1+k)o1

    Thus, provided oz./or:b/a: k, the tangential tress

    will be constant along the edge. According to Baud's

    postulation, he shape with uniform strength distribution s

    considered as optimum. Furthermore, to verify the

    availability of BGS , different initial shapes of holes

    including (u) square and (b) rectangle were used as

    numerical examples as shown n Fig.3. Due to symmetry,

    only one quarter of these structural models were analyzed.

    The material property and oading condition with case abel

    were given in Table.l. and 2 respectively. Due to ductile

    material used n these ases, on Mises stress was selected s

    the equivalent stress(abbr. s EQS). By applying BGS, the

    optimized shape or different initial shapes under the equal

    case 81

    T: Dcsign Profilt

    J

    2

    (a) square hole

    Table 1 Material property

    c* E*

    1000 1000 7.00E+04x : urut kgul'cnr:)

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