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Determine Mode

Apr 06, 2018

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Hairil Mohd
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  • 8/3/2019 Determine Mode

    1/20

  • 8/3/2019 Determine Mode

    2/20

    X

    YZ

    a=L 2550mm

    b 850mm

    B 3400mm

    tp 16mm

    hw 235mm

    tw 10mm

    bf 90mm

    tf 15mm

    E 205800MPa

    Y 313.6Mpa

    p 0.1MPa

    0.3

    D

    wopl 0.12t

    3

    212(1 )

    Et

    Y

    E

    b

    t

    Three longitudinal stiffeners

    Only applied on longitudinal compressive loads

    Lateral pressure loadNeglect(=0)

  • 8/3/2019 Determine Mode

    3/20

    Overall Collapse (Mode I)

    Collapse of plating together with stiffener as a unit

  • 8/3/2019 Determine Mode

    4/20

    Overall Collapse (Mode I)

    Collapse of plating together with stiffener as a unit

    1 sx sxx

    n AE E

    Bt

    1

    sy sy

    y

    n A

    E E Lt

    (1 2 )

    x y

    xy

    x x y y

    E EG

    E E

    22 33

    0 012 2 2 12 2 2

    fx fx fxwx wx wxx wx wx x fx fx wx x

    b t tt h h t tI t h z b t h z

    0yI

    0

    ( / 2 / 2) ( / 2 / 2)wx wx wx fx fx fx wx

    x

    wx wx fx fx

    h t h t b t t h t z

    bt h t b t

    00 yz

    0.53 2 3 3

    0 0

    2

    ( / )( / 12 / ) /12 /

    ( / )( / ) ( / )( / )

    y x x x y y

    x

    x y x y y x

    E E Et Etz EI b Et Etz EI ac

    EI b E E EI a E E

    y

    y x

    x

    E

    E

    23

    0

    12(1 ) 1

    x x

    x

    x y x y

    Etz EIEtD

    b

    230

    12(1 ) 1

    y y

    y

    x y x y

    Etz EIEtD

    a

    31

    2 3y x x y xy

    tH D D G

    10

    7

    9

    247792.2794

    205800

    2.6967 10

    7.66886 10

    3.64605 10

    x

    y

    x

    y

    E Mpa

    E Mpa

    D Nmm

    D Nmm

    H Nmm

  • 8/3/2019 Determine Mode

    5/20

    Overall Collapse (Mode I)

    Determine value of Am in terms ofxav

    3 21 2 3 1

    22 4 4

    1 23 3 3 3

    2 2 4 2 2 4 2

    3 3 3 3 3

    2

    4 4

    0

    3,

    16 16

    2

    816

    m m m

    omx y x y

    omx y xav x y

    om xav

    C A C A C A C

    Am B L m B LC E E C E E

    L B L B

    A m B L m B m B m LC E E D H D

    L B L t L LB Bm B LB

    C A pL t

    22 4 4

    1 23 3 3 3

    22 2 4 2 2 2

    3 3 3

    2

    4 4

    3,16 16

    ( )8

    16

    om

    omxav rex rey

    om xav

    EAE m b a m b aC Ca b a b

    EA m b a m b a D m mb aC

    a b a b t ab a mb

    m B abC A p

    L t

  • 8/3/2019 Determine Mode

    6/20

    Overall Collapse (Mode I)

    Determine value of Am in terms ofxav

    9 9.5 10 10.5 11 11.5

    Am

    0

    100

    200

    300

    400

    500

    xav

    (MPa)

    0 0.5 1 1.5 2 2.5

    UC

    0

    100

    200

    300

    400

    500

    xav

    (MPa)

  • 8/3/2019 Determine Mode

    7/20

    9 9.5 10 10.5 11 11.5Am

    0

    100

    200

    300

    400

    500

    xav(MPa)

    Mode1-Area1(Am)

  • 8/3/2019 Determine Mode

    8/20

    0 0.5 1 1.5 2 2.5UC

    0

    100

    200

    300

    400

    500

    xav(M

    Pa)

    Mode1-Area1(UC)

  • 8/3/2019 Determine Mode

    9/20

    0 0.5 1 1.5 2 2.5UC

    0

    100

    200

    300

    400

    500

    xav(MPa)

    Mode1-Area2(UC)

  • 8/3/2019 Determine Mode

    10/20

    2 2

    yb ybxb xb

    Yeq Yeq Yeq Yeq

    1

    Overall Collapse (Mode I)

    2 22 2

    xb xav 2

    2 22

    yb 2

    ( 2 )

    8 2 1

    ( 2 )

    8 2 1

    eqx m m om mx x y

    x y

    y m m om eq mx y x

    x y

    tm E A A A A mE

    L L B

    E A A A t A mE

    B L B

    Yp Ys

    Yeq Yx 313.6sx sx

    sx sx

    Bt n A

    Bt n A

    Yx

    Yeq Yy

    Yx Yy

    for longitudinally stiffened panels

    for transversely stiffened panels

    ( ) / 2 for orthogonally stiffened panels

    Yeq=equivalent yield stress

    Collapse of plating together with stiffener as a unit

  • 8/3/2019 Determine Mode

    11/20

    Overall Collapse (Mode I)

    teq=equivalent plate thickness

    eq eq

    eq2

    x yt t

    t

    s ss seq eq

    ,y yx x

    x y

    n An At t t t

    B L

    2 22 2

    xb xav 2

    3 205800 ( 2 6.882) 19.265 3205800 0.3

    8 2550 2 1 0.09 2550 3400m m m

    A A A

    2 2

    yb ybxb xb

    Yeq Yeq Yeq Yeq

    1

  • 8/3/2019 Determine Mode

    12/20

    Biaxial Compressive Collapse (Mode II)

    - Thick plating and under predominant biaxial compressive stress

    - Mode of collapse

    plate stiffener interaction yields at the corner of plating between stiffener.

    22 4 4

    1 23 3 3 3

    22 2 4 2 2 2

    3 3 3

    2

    4 4

    3,

    16 16

    ( )8

    16( )

    om

    om

    xav rex rey

    om xav rex rey

    EAE m b a m b aC C

    a b a b

    EA m b a m b a D m mb a

    C a b a b t ab a mb

    m b a abC A p

    a b t

    22 4 4

    1 23 3 3 3

    22 2 4 2 2 2

    3 3 3

    2

    4 4

    3,16 16

    8

    16

    om

    omxav

    om xav

    EAE m b a m b aC C

    a b a b

    EA m b a m b D m mb aC

    a b a t ab a mb

    m b abC A p

    a t

  • 8/3/2019 Determine Mode

    13/20

    Biaxial Compressive Collapse (Mode II)

    2 2

    max av 2

    ( 2 ) 2cos

    8

    m m om t x x x

    m EA A A b

    a b

    - Thick plating and under predominant biaxial compressive stress

    - Mode of collapse

    plate stiffener interaction yields at the corner of plating between stiffener.

    2 2 2

    max maxmax max

    Y Y Y Y Y

    1y yx x av

    2 2 2

    max maxmax max

    Y Y Y Y Y

    1y yx x av

    2 2

    max av 2( 2 )

    8m m om

    x x x m EA A Aa

    2

    max 2

    ( 2 ) 2cos

    8

    m m om t y x

    EA A A m a

    b a

    2

    max 2

    ( 2 )

    8

    m m omy

    EA A A

    b

  • 8/3/2019 Determine Mode

    14/20

    5 10 15 20 25 30 35Am

    0

    100

    200

    300

    400

    500

    xav

    Mode2-(Am)

  • 8/3/2019 Determine Mode

    15/20

    Mode2-(UC)

    0 0.5 1 1.5 2 2.5UC

    0

    100

    200

    300

    400

    500

    xav(MPa)

  • 8/3/2019 Determine Mode

    16/20

    Beam-Column-type Collapse (Mode III)

    Effective width of plating between longitudinals:

    2 2

    min minmax max

    Y Y Y Y

    1y yx x

    Yeu

    xu

    b

    b

    2

    1.0 1

    2 / 1/ 1

    euforb

    b for

    Plate adge at mid-span:

    229.5xu

  • 8/3/2019 Determine Mode

    17/20

    Beam-Column-type Collapse (Mode III)

    Effective width of plating between longitudinals:

    PSC at mid-span:

    850 313.62.074

    16 205800

    Ypb

    t E

    0.18 459eb L mm

    2850 16 235 10 90 15 17,300p w f

    A A A A mm

    2459 16 235 10 90 15 11,044e pe w f A A A A mm

    20.5 ( 0.5 ) ( 0.5 )65.325

    e w w f w f

    p

    e

    b t A t h A t h t z mm

    A

    22 2 33 3

    12 2 12 2 12 2

    102919130.6

    f f fe w w we pe p w p f w p

    b t tb t t h t hI A z A z t A t h z

    maxmaxp xav p

    e

    Mz

    I

    max 2 maxqM C M

    2 2 2

    8

    [1 sec( / 2)]C kLk L

    2

    max 8qqL

    M

    maxmax ( )s xav w f p

    e

    Mt h t z

    I

  • 8/3/2019 Determine Mode

    18/20

    Collapse by Local Buckling of Stiffener Web (Mode IV)

    L WIV u u su

    s

    x x xx

    x

    bt A

    bt A

    L euu Yx

    b

    b

    22W W w

    E u w 2

    w12(1 )

    x

    tEk

    h

    2W w w

    w u 2

    w

    x

    h tk

    D

  • 8/3/2019 Determine Mode

    19/20

    Collapse by Tripping of Stiffener (Mode V)

    L euu Yx

    b

    b

    2 2 2 2 2T w f f w 4

    E 2 2 21,2,3...

    p p

    (J J ) 3( 1) 1min

    12m

    a G EI h m Sqa

    I a I I m

    L TV u u s

    s

    x x xxu

    x

    bt A

    bt A

  • 8/3/2019 Determine Mode

    20/20

    Gross Yielding (Mode VI)

    21 3

    M MM M

    VI VI VI VI VI

    u u u u u

    1

    cc c

    y yx x

    x x y y

    VI

    M ux x

    VI

    u Y eux

    b

    b

    2

    1.0 1

    2 / 1/ 1

    euforb

    b for