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Steel Structures Details - Column Problems

Apr 06, 2018

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Serkan Emir
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    Steel Structures

    N-W.F.P University of Engineering &

    Technology Peshawar

    CE - 411

    Instructor: Prof. Dr. Shahzad Rahman

    Lecturer: Engr. Kamran Ayub

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    Example Problem 1

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    Example Problem 1(Contd.)

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    Example Problem 1(Contd.)

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    Example Problem 2 - LRFD

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    Example Problem 2 (Contd.)

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    Example Problem 2 (Contd.)

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    Example Problem 2 (Contd.)

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    Example Problem 3

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    Example Problem 3 (Contd.)

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    Example Problem 3 (Contd.)

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    Example Problem 3 (Contd.)

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    Example Problem 3 (Contd.)

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    KL is called effective length of column and K

    effective length factor.

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    Effective length factors (AISC manual)

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    EFFECTIVE LENGTH OF

    COLUMNS IN FRAMES So far, we have looked at the buckling strength of

    individual columns. These columns had various

    boundary conditions at the ends, but they werenot connected to other members with moment

    (fix) connections.

    The effective length factor K for the buckling of an

    individual column can be obtained for theappropriate end conditions from Table C-C2.1 of

    the AISC Manual

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    Columns in Frames

    However, when these individual columns

    are part of a frame, their ends are

    connected to other members (beams etc.).

    These frames are sometimes braced and

    sometimes unbraced.

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    A Braced frame is one in which a sideway(joint translation) is prevented by means of

    bracing, shear walls, or lateral support fromadjoining structure.

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    A UnBraced does not have any bracingand must depend on stiffness of its ownmembers and rotational rigidity of joints

    between frame members to prevent lateralbuckling.

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    Conclusions

    Critical loads for a column depends on

    its stiffness relative to that of beamsframing into it and

    Presence or absence of restraint to

    lateral displacement of its ends.

    Effective length coefficient increases with

    decreasing stiffness of the beam and

    becomes unity with zero stiffness.

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    Braced & Unbraced Frames Similarly you can analyze

    multibay, multistory frames.

    Assumptions Subjected to vertical loads only

    All columns become unstable

    simultaneously

    All joint rotations at floor are equal Restraining moment distributed in

    proportion to stiffnesses.

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    Method of Analysis First, you have to determine whether the

    column is part of a braced frame or an

    unbraced (moment resisting) frame. Then, you have to determine the relative

    rigidity factor G for both ends of the column

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    G is defined as the ratio of the summationof the rigidity (EI/L) of all columns comingtogether at an end to the summation of therigidity (EI/L) of all beams coming together

    at the same end.

    G =

    It must be calculated for both ends of the

    column.

    b

    b

    c

    c

    L

    IE

    L

    IE

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    Then, you can determine the effective lengthfactor K for the column using the calculated value

    of G at both ends, i.e., GA

    and GB

    and the

    appropriate alignment chart.

    There are two alignment charts provided by the

    AISC manual,

    One is for columns in braced (sidesway inhibited)

    frames. See Figure C-C2.2a on page 16.1-191 ofthe AISC manual. 0 < K 1

    The second is for columns in unbraced (sidesway

    uninhibited) frames. See Figure C-C2.2b on page

    16.1-192 of the AISC manual. 1 < K

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    Inelastic Case

    G is a measure of the relative flexural rigidityofthe columns (EI

    c/L

    c) with respect to the beams

    (EIb/Lb) However, if column buckling were to occur in the

    inelastic range (c

    < 1.5), then the flexural rigidity

    of the column will be reduced because Ic

    will be

    the moment of inertia of only the elastic core ofthe entire cross-section.

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    rc = 10 ksi

    rt = 5 ksi

    rt = 5 ksi

    rt = 5 ksi

    rc = 10 ksi

    (a) Initia l state residual st ress (b) Partially y ielded sta te at buckling

    Yielded zone

    Elastic core, Ic

    rc = 10 ksi

    rt = 5 ksi

    rt = 5 ksi

    rt = 5 ksi

    rc = 10 ksi

    rc = 10 ksi

    rt = 5 ksi

    rt = 5 ksi

    rt = 5 ksi

    rc = 10 ksi

    (a) Initia l state residual st ress (b) Partially y ielded sta te at buckling

    Yielded zone

    Elastic core, Ic

    Yielded zone

    Elastic core, Ic

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    Inelastic stiffness

    The beams will have greater flexural rigidity

    when compared with the reduced rigidity

    (EIc) of the inelastic columns. As a result,

    the beams will be able to restrain the

    columns better, which is good for column

    design.

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    Inelastic Stiffness

    The ratio Fcr/ Fe is called

    Stiffness reduction factor

    ( )22

    658.0877.0877.0

    )658.0(

    ,

    , 2

    2

    cc c

    Fy

    c

    Fy

    elasticFcr

    inelasticFcr

    =

    =

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    Procedure for Column Design

    1. Design Load

    2. Assume Fcr

    Pn = Ag Fcr= Pu

    Find Ag

    Select a section

    3. Find

    1. Find

    c = E

    F

    r

    LK y

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    Column Design

    Forc

    1.5 Fcr

    = Fy

    Forc > 1.5 Fcr = Fy

    1. Fcr Calculated > Fcr Assumed

    2. P > Pu. Check3. IfP > Pu, Design is OK Else Repeat

    Steps 2 to 6

    2c658.0

    2c

    877.0

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    Column Design Using Design Aid

    LRFD manual contains variety of Design aids,helpful in making original trial section.

    1. Design load

    2. Find section for Corresponding P & KL using

    Column Tables in the Manual

    3. Calculate an equivalent (KL)eq =

    if strong axis buckling needs

    checking1. Use the calculated (KL)eq value to find (cPn)

    the column strength from column tables

    yx

    xx

    r/r

    LK

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    Problem 4-11-1

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    Solution

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    THANKS