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  • 8/12/2019 Section Propoerties CIVL3111

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    AS4100 Standard Grades and

    Sections

    Asst. Prof. Hang Thu Vu

    [email protected]

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    Lecture outline Industry uses AS4100 for general urose steel structure analysis

    and design. !ithin "IV#$111% we will refer to this standard as the&ain design code. 'eneral &aterial roerties to use for design to AS4100

    (iscuss availa)le standard grades and sections for design toAS4100

    'rades* overview of availa)ility. +ield stress and tensile strength Sections* overview of availa)ility. ,ffects of shaes on section

    caacity against loading actions Study the &eanings% usages and how to co&ute section

    ara&eters I% -% S

    ending of steel &e&)ers in elastic and lastic ranges Second &o&ent of area I ,lastic section &odulus - Plastic section &odulus S

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    Basic parameter values and adjustment

    for elevated temperatures

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    Standard Grades

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    Designation of Grades

    Table 2.1 in AS4100. This ta)le gives values of yieldstress and ulti&ate tensile strength for steelroducts that co&ly with the re/uire&ents of AS%AS-S &anufacturing standards

    Standard grade usually starts with the nu&)er of thestandard then characters and digits to stand for thegrade. ,2a&le* AS-S $35.1 $60#0

    ote* AS-S 1654 uses a different syste& ofgrade designation. 7efer to AS-S 1654 Section

    1.4

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    Hot-rolled and cold-form grades Hot8rolled roducts 9lates and sections: are in

    grades ;00% ;60% $00% $60% 400% 460% 600.These &ay )e o)tained with notch ductile/ualities 9with suffi2 #0 or #16: andor weather8resistant /ualities 9with refi2 !7:. !eatheringsteels are in 'rade $60 only

    Hot8rolled welded sections are roduced fro&AS-S $3< lates= oularly in 'rades $00%400% !7$60

    "old8for&ed hollow sections are with refi2es ".They are roduced in 'rades ";60% "$60% and"460. They &ay co&e with notch ductile #0/uality

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    Hot-rolled and cold-form grades

    (ata for design to AS4100 for

    the &ost co&&only used

    sections and lates in 'rades;60% $00% $60

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    alues of !ield stress f!

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    #$istence of residual stress

    Tis of flanges and &iddle of we) cool and harden% &ore

    /uic?ly than the rest of the cross8section.

    The harder arts are in a state of co&ression. The>unctions% )eing held )y the harder arts and una)le to

    contract as far as they would otherwise% are laced in

    tension.

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    Standard sections and plates

    Steel roducts are rovided in standard siesand shaes. or &aterial availa)ility and cost

    asect% it is reco&&ended to use standard

    sections in your design. elow are funda&ental

    sections

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    Standard sections and plates

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    #ffects of s"apes on mem%er strengt"

    It is o)served that steel is roduced in various sections.

    These include BlateB% Brounds% )ars and rodsB% BanglesB%BchannelsB and BI8sectionsB.

    The I8sections are roduced as B)ea&B sections with I yy

    &uch less than I22and Bcolu&nB sections with Iyyof closer

    value to I22. Cost of these sections are roduced )y rolling red hot

    steel. Cost sections have arallel flanges 9the BuniversalB)ea& and colu&n sections% and the channels:. So&eBtaer flangeB Is and channels are also roduced.

    It is ossi)le to &a?e very large sections 9e.g. for )ridge)ea&s: )y welding late into the for& of an I or )o2.#engths are availa)le fro& a &ini&u& of 3 &etres to a&a2i&u& of $0 &etres. 7efer to Ta)le ;% DneSteel BHot7olled and Structural ProductsB% 6thed.

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    #ffects of s"apes on mem%er strengt"

    However% if )uc?ling occurs% the )uc?ling loadthat the &e&)er can withstand deends onsecond &o&ent of area I22and Iyy.

    As the colu&n )uc?le a)out the a2is which is ofwea?er I% it is i&ortant to have I22and Iyyofsi&ilar &agnitude 9Eniversal colu&ns: whenthere is no lateral )racing for wea? a2is

    &

    &

    '(kL

    EIP

    cr

    =

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    #ffects of s"apes on mem%er strengt" Bending* stress in a )ea& deends on the second

    &o&ent of areaI

    The )ending &o&ent which a )ea& can carry )efore itsflange starts to yield is CF-fy% where - is the elastic&odulus.

    If the &o&ent is increased further% yielding sreadsthroughout the cross section. Total collase occurs at a&o&ent CFSfywhere S is the lastic section &odulus9study later:.

    I

    My=

    ma$y

    IZ=

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    )ompare section properties for sections

    of same amount of material Area A F 13000 &&;

    Sread &aterial further away fro& neutral a2is to

    &a?e rectangle% I shae 9310 E 1;6:% truss

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    Bending of steel mem%er in elastic and

    plastic ranges

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    *evision+ Structural anal!sis

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    *evision+ Structural anal!sis

    !e want to calculate the &a2i&u& values ofactions 9&o&ent% shear force% a2ial force ..:for &e&)er design

    ree )ody diagra&

    Vertical reaction Ay% e/uivalent load P. At thecut of distance fro& left end* shear force V%)ending &o&ent C

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    *evision+ Structural anal!sis The reaction at A is The e/uivalent oint load at a distance 2; fro& A is Ta?e &o&ent a)out the cut%

    orce e/uili)riu& for y direction%

    Ca2i&u& shear force haens at end Ca2i&u& )ending &o&ent haens at &iddle

    wLAy&

    1=

    wxP=

    &&

    1

    0&&

    1

    &wxwLxM

    xwxwLxM

    =

    =+

    wxwLV

    wxwLV

    =

    =+

    &

    1

    0&

    1

    wLV&

    1

    ma$=

    ,

    &

    ma$

    wLM =

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    Bending of a %eam mem%er

    ending stress J22of the cross8section of a )ea& varies along the)ea& height

    The )ea& is under &a2i&u& stress when CFC&a2and yFy&a2Fd;

    The e2tre&e fi)re of the cross8section starts to yield when J22F fy.Hence% the &o&ent caacity that a cross8section can ta?e is

    Z

    M

    I

    My==

    ZfM yy=

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    Bending of a %eam mem%er

    !hen the whole cross section yields the &o&ent

    caacity increases to Cs. or design urose 9lower )ound of lasticity:% strain

    hardening is ignored. The &aterial is ter&ed as ure

    lasticity 9see )elow figure:.

    It is assu&ed that the &a2i&u& stress that anywhere in

    the cross section can reach is fy9see )elow figure:

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    Bending of a %eam mem%er

    - is ter&ed elastic section &odulus

    S is ter&ed lastic section &odulus

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    Second moment of area

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    ormulae Second Co&ent of Area* also ?nown with other na&es

    Second Co&ent Df Inertia% Area Co&ent of Inertia The &athe&atical e/uations to calculate the Second

    Co&ent of Area *

    y is the distance fro& the neutral a2is 22 to aninfinitesi&al area dA

    2 is the distance fro& the neutral a2is yy to aninfinitesi&al area dA

    =

    =

    A

    yy

    A

    xx

    dAxI

    dAyI

    &

    &

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    #$ample 1+ *ectangular section

    ( )

    1&

    ,,..

    .

    ..&

    &

    .&

    &

    &&

    bdI

    ddbybbdyydAyI

    xx

    d

    d

    d

    dA

    xx

    =

    +====

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    #$ample &+ Hollo/ sections

    7ectangular hollow sections

    I sections

    1&1&

    .

    &&

    .

    11 dbdb

    Ixx =

    1&&

    1&

    .. chbdIxx =

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    #$ample .+ )ircular sections and

    )ircular "ollo/ sections

    4

    4rIxx

    =

    ( )4

    &

    4

    14 rrIxx =

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    eutral a$is (A' of non-s!mmetric

    sections !hen the section is non8sy&&etric% we need to find the

    location ycof the neutral a2is with resect to a datu&

    which is usually chosen at the )ase of the section

    The sign shows the contri)utions fro& all nele&ents of the cross section.

    =

    ==n

    i

    i

    n

    i

    ii

    c

    A

    hAy

    1

    1

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    2arallel a$is t"eorem The second &o&ent of area for the whole section

    with resect to the located neutral a2is is calculatedfro& the Parallel A2is Theore&

    I* the second &o&ent of area

    Ii* the second &o&ent of area of ele&ent ith

    Ai* area of ele&ent ith

    di* distance )etween the neutral a2is of ele&ent ith

    and the neutral a2is of the whole section

    =

    +=n

    i

    iii dAII1

    &

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    #$ample+ )alculate 3$$for section

    d1F 610 8 $36.6 F 144.6 &&

    d;F $36.6 8 ;60 F 116.6 &&

    I22F ;002;0$1; K ;002;029144.6:;

    K 102600$1; K 10260029116.6:;

    Hence

    I22F ;64%6;;%;60 &&4

    =

    +=n

    i

    iii dAII1

    &

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    #lastic section modulus

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    ormulae

    Elasticsection modulus- of a )ea& is the ratio of

    a cross sectionLs second &o&ent of area I to the

    distance of the extreme compressive fibrefro& the

    neutral a2is

    The elastic section &odulus &ar?s the yield oint ofthe &aterial when the &ost outer fi)re starts to yield

    due to )ending &o&ent CyF-fy

    ma$y

    IZ=

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    2lastic section modulus

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    Define location of t"e 2A

    The lastic neutral a2is PA% which is also referred to as

    the e/ual area a2is% is the a2is that slits the cross

    section into two e/ual areas. These areas refer to the

    e/ual a&ount of fi)res yielded under co&ression and

    tension resectively. or sy&&etric section% the lastic and elastic neutral

    a2is coincide. They are the a2is through the centroid of

    the section.

    or non8sy&&etric section% location y the PA withresect to a datu& which is usually chosen at the )ase

    of the section is defined

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    )alculate S

    S is co&uted as the su& of &o&ent of ele&ent

    areas a)out the PA

    S* the lastic section &odulus

    Ai* area of ele&ent ith

    ei* distance )etween the neutral a2is of ele&ent ith

    and the lastic neutral a2is of the whole section.

    ==n

    iiieAS 1

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    #$ample+ section

    yF$00

    S F 9;00 2 40 2 1;0: K 9100 2 40 2 60: K 9$002 40 2 160:

    Hence% S F ;530 2 10$&&$

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    e$t lecture

    Investigate the loads acting on the structure

    in ter&s of Per&anent load 9dead load:

    I&osed load 9live load: #oad factors to co&ly with li&it state design and

    &e&)er design to AS4100

    7eadAS-S 110.1*;00;