Column Slender

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    Interaction Diagram 2 side reinforcement

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 1 / 11

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    Interaction Diagram 4 side reinforcement

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 2 / 11

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    Slender or Long Column

    If column slenderness ratio exeedsthe limit for short column, thecompression member will buckleprior to reach its limit state ofmeterial failure.

    The effective length klu is used asthe modified length of the columnto account for end restraints otherthan pinned.

    The value ofk:Both ends fixed k= 0.5Both ends fixed, lateral motion exist k= 1.0Both ends pined, no leteral motion k= 1.0One ends fixed, other end free k= 2.0

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 3 / 11

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    Column in structural frame

    1 Braced compressive members.

    k= 0.7 + 0.05(A + B) 1.0k= 0.85 + 0.05min 1.0

    where:

    =EI/lucolumns

    EI/lnbeams

    lu is the unsupported length of column; ln is clear beam span.2 Unbraced compression members restrained at both end.

    For m < 2 : k=20 m

    20 1 + m

    For m 2 : k= 0.9

    1 + m

    where: m is the average of the value at the two ends.3 Unbraced compression members hinged at one end.

    k= 2.0+ 0.3

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 4 / 11

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    Effective Length Factor, k

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 5 / 11

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    Moment Magnification: First-Order Analysis

    Properties of member in a structure:1 Modulus of Elasticity: Ec = 4700

    fc

    2 Moment InertiaBeams 0.35Ig

    Columns 0.70IgWall : uncrack 0.7IgWall : crack 0.35IgFlat plates and flat slabs 0.25Ig

    3 Area: 1.0As4 Radius of giration: r = 0.30h for rectangular member, r = 0.25D

    for circular members.

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 6 / 11

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    Moment Magnification in Nonsway Frames

    Structure is nonsway if:

    Q =Pu0Vulc

    0.05

    Where: Pu and Vu are the total vertical load and the story shear, and 0 is the relative deflectionof that story due to VuThe slenderness effect can be disregarded if

    klur 34 12

    M1M2

    andM1M2

    0.5

    M1/M2 is positive if single curvature, and negative if double curvature.The magnified moment becomes

    Mc = nsM2

    where

    ns =Cm

    1 (Pu/0.75Pc) 1.0

    Pc =2EI

    (klu)2

    and

    EI=0.2EcIg + EsIse

    1 + dor EI=

    0.4EcIg

    1 + d

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 7 / 11

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    Moment Magnification in Nonsway Frames (cont.)

    Cm a factor relating the atual moment diagram to an equivalentuniform moment diagram. For member without transverse load, thatis, subjected to end loads only,

    Cm = 0.6 +M1

    M2

    0.4 where M2 M1

    M1/M2 is positif if column is bent in single curvature. For memberswith transverse load between support, Cm = 1.0Minimum factored moment M2 is

    M2,min = Pu(15 + 0.03h), where h in mm

    IfM2,min exceeded the applied moment M2, the value ofCm = 1

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 8 / 11

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    Moment Magnification in Sway Frames

    The slenderness effect can be disregarded if

    klur< 22

    The end moment M1 and M2 should be magnify as follows

    M1 = M1ns + sM1s

    M2 = M2ns + sM2s

    On the assumtion that M2 > M1, the design moment should be

    Mc = M2ns + sM2s

    Magnified sway moment can be calculated as

    sMs =Ms

    1 (Pu/0.75Pc) Ms, where s 2.5

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 9 / 11

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    Example:1. Sway frame

    Compute slenderness column A-B, with single curvature moment 75 KN-m , as picture

    300x450mm 300x450

    300x600 300x600

    300x500

    A

    B

    6000mm 7000

    3500

    3000

    Inertia :Top Col : 112 300 500

    3 = 3125000000 mm4

    Top Beam: 112 300 4503 = 2278125000 mm4Bot Beam: 112 300 600

    3 = 5400000000 mm4

    A =0.73125000000

    30000.352278125000

    6000 +0.352278125000

    7000

    = 2.95

    B =0.73125000000

    3000 +0.73125000000

    35000.3554000000006000 + 0.3554000000007000

    = 2.31

    from alignment chart k= 1.74.

    lu = 3000

    450

    2+

    600

    2

    = 2475

    klur

    = 1.74 24750.3 500

    = 28.71

    SNI code for shot column

    klur 34 12

    75

    75

    = 22

    Hence column A-B is slender columnFaimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 10 / 11

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    Example:2. NoSway

    2.5 m

    2.5 m

    90 kN

    650 kN

    650 kN

    Primary moment due to lateral load, Ec = 25000 MPa

    Mn =90 5

    4= 112.5 kN-m

    Pc =2EI

    (klu)2(euler bucling load)

    =

    2 25000 112 300 3003

    (1.0 5000)2

    = 6662 kN

    Magnified moment

    Mc

    = Mn

    1

    1 PPc

    = 112.51

    1 6506662= 112.5 1.11 = 124.875 kN-m

    Faimun (ITS Surabaya) Rekayasa Struktur Semester Genap 2011/2012 11 / 11

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