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    Lehigh University 

    Lehigh Preserve

    Fritz Laboratory Reports Civil and Environmental Engineering

    1-1-1963

    Flexural strength of steel and concrete composite beams,

    R. G. Sluer

    G. C. Driscoll Jr.

    Follow this and additional works at: hp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports

    is Technical Report is brought to you for free and open access by the Civil and Environmental Engineering at Lehigh Preserve. It has been accepted

    for inclusion in Fritz Laboratory Reports by an authorized administrator of Lehigh Preserve. For more information, please contact

    [email protected].

    Recommended CitationSluer, R. G. and Driscoll, G. C. Jr., "Flexural strength of steel and concrete composite beams, " (1963). Fritz Laboratory Reports. Paper1806.hp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports/1806

    http://preserve.lehigh.edu/?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPagesmailto:[email protected]://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports/1806?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPagesmailto:[email protected]://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports/1806?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/engr-civil-environmental-fritz-lab-reports?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPageshttp://preserve.lehigh.edu/?utm_source=preserve.lehigh.edu%2Fengr-civil-environmental-fritz-lab-reports%2F1806&utm_medium=PDF&utm_campaign=PDFCoverPages

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    279 15

    L IS

    T o F

    T: A B L E

    S

    AND

     IG

    U

    R S

    Table

    Page

    1

    SUMM RY

    OF

    BEAM

    TESTS

    27

    2

    SUMM RY

    OF

     E M

    TEST

    RESULTS

    28

    3a

    ULTIMATE STRENGTH

    OF STUD CONNECTORS

    29

    3b

    ULTIMATE STRENGTH OF SPIRAL CONNECTORS 29

    3c

    UL+IMATE

    STRENGTH OF

    CHANNEL

    CONNECTORS

    30

     

    4

    COMPARISON

    OF

    TEST RESULTS WITH

     

    ND

     

    31

    Figure

    11

    1

    2

    4

    5

    6

    7

    8

    9

    10

    11

    12

    13

    14

    DErAILS OF TEST

     E MS

    B1 THROUGH B13

    SUMM RY OF

    LOADING

    CONDITIONS

    DELAILS OF PUSHOUT SPECIMENS

    STRESS

    DISTRIBUTION

    AT

    ULTIMATE

    MOMENT

    SHEAR ~ O N N E T O R FORCES

    AT

    ULTIMATE M O M E N ~

    ULTIMATE

    STRENGTH OF STUD. SHEAR CONNECTORS

    ULTIMATE STRENGTH

    OF SPIRAL

    SHEAR

    CONNECTORS

    ULTIMATE

    STRENGTH

    OF CHANNEL

    SHEAR CONNECTORS

    MOMENT-DEFLECTION CURVES. FOR

     E MS

    B1

    TO

    B6

    MOMENT-DEFLECTION CURVES FOR

     E MS

    B7

    TO

    B12

    RELATIONSHIP BETWEEN

    SHEAR CONNECTOR

    STRENGTH

     ND

     

    MOMENT

    CAPACI

    TY

    MEASURED STRAINS

    ON

    MEM ERS AT

    MIDSPAN

    STRESS D I S T R I U T ~ O N AT

    MODIFIED

    ULTIMATE

    MOMENT

    MOMENT DEFLECTION CURVES

    FOR

    TESTS

    OF B10

    Bll

    ND

    B12

    32

    33

    34

    35

    36

    • 37

    38

    39

    40

    41

    42

    43

    44

    45

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    279.1?

    L I

    T

    L E

    S N

     

    F IG

    U

    RES  continued

    i i i

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    279.15

    S Y N

    P S

    S

    The resul ts of a

    research

    program to invest igate

    the

    ultimate

    strength

    of composite s teel and concrete members are reported. These

    resul ts

    along

    with informa tion on the 4ltimate

    strength of

    various

    types

    of

    mechanical

    shear

    connectors are used

    to

    develop cr i te r ia for minimum

    shear

    connector requi rements for composite building members The effect

    of s l ip between concrete slab and

    s tee l

    beam

    is

    shown to have no measur

    able

    effect

    on

    the ultimate

    moment of a member A method

    of determining

    the

    ultimate strength of members ~ i ~

    very

    weak shear connectors is

    developed and applied to the a naly sis o f

    tes t

    resu l t s

    This

    method of

    iv

    analysis is used

    to establ ish a

    defini te

    minimum

    number of

    shear connectors

    to be

    useq in

    pesign.

      t is

    shown

    that the

    redis t r ibut ion

    of load on

    shear

      o n n ~ t o r s a t high load makes

     

    unnecessary to space shear connectors in

    accordance

    with the shear diagram. One t e s t

    of

    a continuous member

    is

    presented

    to show that

    not

    only

    ultimate strength

    th eo ry but

    plas t ic

    design

    theory

    can

    be applied

    in a l imited way t o composite members

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    279.15

    .2 . E X P R

     

    M E N TAL PRO G RAM

    The

    twelve

    15

    feet simple span

    members

    te ste d a re

    described

    in

    Fig.

    1, and are

    d e s i g n a t ~ d ~ s ~

    through

    B12 The

    continuous

    member

    -4

    d e s i g n a t ~ d B consi st ed o f two spans of

    15 -0

    with the same cross

    section.  The shear connectors provided

    in each

    beam are l isted in Table 1

    along

    with

    the

    concrete

    strength

    for

    each ~ e m b e r

    Tests performed in

    this

    investigation

    w h ~ h

    th e

    resul ts

    qave

    not

    been

    previously published

    are

    ident if ied

    by an aster isk in the

    Reference

    Number columns of Tables 1, 3a,

    and 3c T ~ e l o ~ 4 i n g conditions for the tests of these members and

    the

    tests performed.by o th er in ve stig ato rs a re

    given

    in Fig.

    2 and Tab le

    2.

    The data

    o b t ~ i n ~ d

    for maximum applied moment

    type

    of

    f a i l u r ~

    maximum

    cpnnector force, and maximum end s l ip are also

    given

    in Table 2.

    will be ~ o t i c ~

    that

    some

    of

    the

    twelve

    members

    in this

    prQgram

    were tes ted several

    times.

    The procedm;e

    in these· tes,ts

    was

    to

    load the

     

    member up

    to

    a point a t which strains on the tqP of th e concret e

    slab

    a t

    midspan indicated t h a ~   r u s ~ i n g of the concrete was imminent. Then th e

    member was unloaded and loaded again with the load points further

    apart .

    The

    ultimate

    moment

    data

    for only the las t of such tests is used in the

    a n ~ l y s i s

    t

    is

    not

    known

    to

    what e x t ~ ~ t

    previous loadings

    may

    have

    s l ight ly

    reduced final. ultimate moment.attained. However the results

    for ultimate moment from these tests are

    conservative.

    N e a ~ u l ~ i m a t e l ~ a d

    i t

    is imposs ib le to determine the loads the

    shear

    c o n n e ~ t o r s by

    m ~ a s u r e m e n t s such as s l ip

    between beam

    and

    s lab.

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    279.15

      easurements of strain on the s urf ac e o f the connector

     

    r ~ s i n c e

     

    5

     

    m x mum

    load per connector m y occur

     ft r y ie ld in g o f the connector

    material

    Therefore

      ~ o t h e r

    means

    of

    determining

    the

    m x mum

    force

    which

    a

    connector

    can

    r s is t

    must

    be u ~ e d

    o ~ t investigators have used a pushout specimen such as

    th e

    one used in

    this

    i n v e s ~ i g t i o n and shown in Fig

    3.

    Nine of these

    were

     

    tested in this investigation.  he resul ts

    of

    these tests will

    be

    discussed

    in a l t r s ec tio n o f

    th e

    report .

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    279.15

    3. U L

    T I M

    A T E S T R E N G T H O F

    ME

    M B E R S

    Assuming

    t h a t

    a suff icient number

    o f s he a r

    connectors

    have been

    provided the

    sta t ic ul t i m at e s tr en gt h o f th e

    member may be

    determined

    from a fam i l i ar s i m p l i f i e d

    s t ress

    d i s t r i b u t i o n .   s shown

    in

    Fig .. 4 t h i s

    s tress d i s t r i b u t i o n is s i m i l a r

    to

    t h a t assumed in determining th e u l t i m a t e

    s t r e n g t h o f r ei nf or ce d c onc r e te

    members. In

    Fig. 4

    is

    th e 28-day

    c onc r e te

    s t r e n g t h f

    y

    is

    the

    y i e l d

    s t r e n g t h o f the

    s tee l

    an d

    a is

    the

    depth

    o f the compressive s t ress block in

    t he c on cr et e

    when tha t depth i s

    -6

    less than th e s l a b t hi ckness. The

    dimensions o f sla b w idth

    s l a b

    t hi ckness

    an d beam

    depth a re

    b t an d d r e s p e c t i v e l y . The to ta l compressive

    f or c e

    in

    t he c on cr et e

    s l a b is designated by C and the to ta l tensile

    f or c e

    i.n

    th e

    beam by

    T

    Any

    compressi.ve f or c e

    which may

    exis t

    i n

    th e

    s t ee l beam is

    designated

    by

    C .

    The moment arms

    from

    T

    to

    C

    and C a r e

    e

    an d

    e

     

    .

    Composite members may be c o nv e ni en tl y d i vi d ed

    into

    two cases as

    i ndi cat ed in

    Fig.

    4.

    Case

    I includes a l l members in which

    th e

    a r e a

    o f th e

    concrete

    s l a b i s suff icient

    to re s i s t the entire

    compressive

    force

    C

    requi red f or e qu il ib ri um .

    Case I I

    includes

    a l l members in which

    th e

    con-

    c r e t e

    area

    is

    n o t suf f ic ien t an d the

    top

    flange o f th e s t ee l

    beam

    is

    s t r e s s e d to

    f

    y

    in compression. The

    s tee l

    member may

    c o n s i s t

    of

    a r o l l e d

    s e c t i o n

    b u i l t - u p

    s e c t i o n

    o r

    a

    s t ee l

    j o i s t

    Regardless

    o f th e dimensions

    o f the cr os s

    s e c t i o n

    the ul t i m at e

    moment may

    be c a l c u l a t e d

    by

    th e

    following

    equations:

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    279. 15

    -7

    Case I :

    C

    =

    0.

    85f

    d

    1

    T

    =

      s

    f

    y

     2

    C =

    T

    f

    y

      s

     3

    a

    =

    0 8 5 f ~

    c

    ~

      t

    a

     4

    =

    -

    2

    2

    Cd

     D

     5

    u

    =

    =   s

    f

    y

      t

    Case

    I I : C = 0.85 bt

    T = C   C 1

    2

    M u = C e C

    e

     6

    7

    8

    In these equations   i s the ultimate moment and   s i s the

    t o t a l

    area of

    the

    s t e e l

    sect ion.

    For

    Case I I , th e valu es of e and e are

    dependent

    upon

    th e

    shape

    of the cross s e c t i o ~

    The assumption

    that th e concr ete does

    npt

    act in

    tension

    has been

    made

    for t hi s ca lcu la ti on .

    Hence

    a t sections

    where negative moment

    occurs,

    only the

    s t e e l

    member

    plus

    the

    slab

    reinforcing s t e e l   r e c o n ~ i d e r e d

    I f

    slab s teel

    i s

    neglected, the ultimate

    moment of

    th e sect ion reduces to the

    plast ic

    moment

    of

    the s t e e l member.

    The

    ultimate

    s t ~ e n g t h

    has

    been

    determined

    assuming

    that

    a

    sufficient

    number

    of shear connectors

    has

    been provided to completely

    develop

    the

    con-

    crete

    slab. I t ~ h p ~ l d be noted that e l a s t i c

    design

    methods do not neces-

    s a r i l y i n s ~ r e

    that th is

    condition i s s at is fi ed .

    ht   b d {

    t v s   se.t:- / )Y[

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    279.15

      U L TIM   T S T R

     NG

    T H

    o F

    SH R NN

    C TOR S

    The minimum shear connector r e q u i r ~ m e n t may be d e f i n ~ d by con

    s i d e r ~ n g a free body

    of

    a

    portio n o f

    t he concret e slab between the cross

    section

      t

    ultimate moment and th e end of the member as shown in Fig.

    5.

    The force C is

    resisted

    by

    the

    f o r c e s ~ A u or the sum of the u 1 t i ~ t e

    s tre ng th s o f

    shear

    connectors

    in

    the

    ~ e n g t h

    of

    slab

    L

    s

    ·

    This

    provides

     9

    a means

    of

    determining the

    force

    on a

    shear c o n ~ e c t o r

    in a beam   t

    ultimate

    load only when th e member has more than the minimum number

    required.

      t

    will be shown that

    th e

    ultimate

    strength

    of a member with less than the

    minimum

    requirement

    can be

    determined

    once the m i n i ~ u m n u m b ~ r is ~ n o w n

    for that member.

    · Ev en

    though

    previous investigators had

    ignored

    the

    ultimate

    strength

    of c o n n e ~ t o r s

    their work

    produced

    some rel iable data on this

    property.

    Pushout

    tes t data was more

    r ead il y avai lab le

    t an beam tes t

    data because beam

    tests

    of ~ e m ~ e r s with minimum numper of connectors

    h ~ d not

    been

    made by o t h e r ~ Unfortunately not   l l of the pushout t es t

    data

      v i b ~ ~ c o u d be

    ~ s e d because the true

    ultimate

    strength qf a con-

    nector

    was

    not

    obtained

    i f the

    concrete

    slab

    was

    not

    adequately

      ~ ~ ~ ~

    or

    t he ooncr et e s t r n s ~ h

    was

    not

    adequate.

    The

    data

    t h t ~ d ~

     

    tJl f 1afe

    f h ~ f A

    or

      4JMt.- hrl.

    ~ s been a r r a n g ~ d

    in

    Table 3

    in the order

    of

    decreasing

    magnitude

    of

    the

    ultimate loa4

    per

    cQnnector for welded

    studs s p ~ r a 1 and channel

    connectors.

    The scat ter in

    the ~ a t a is

    in part

    due to the

    lack of a

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    279.15 -14

    6.

    U L

    T IM

      TE

    S

    T R

    ENG

    THO

    F . M E M

    B

    E R

    S

    WIT

    H I N A D E QUA T E CON: N E C

    TOR

    S

    I t is p o s s i b l ~ to write an empirical equation 9£ the sloping

    l ine

    in th e l e f t portion of Fig 11 w h i ~ h

    WOUld

    g ~ v e a good approximation for

    th e ultimate strength of members with iqadequateshear connectors as

    follows:

      u=

     

    qu

     

    98C

     

    15

    This

    equation helps to evaluate th e degree of seriousness of a weak s h e ~ r

    connection

    upon the u 1 t i m a ~ e strength

    of

    a member. However

    this

    equation

    can

    not be e x t ~ n d e d to c o m p a ~ i t e sections and a m o ~ e basic

    u n ~ e r

    standing of this problem is

    necessary

    In

    ~ e s t s

    of

    members

    with inadequate sqear

    fonnectors

    i t

    was

    ob-

    serveq

    that generally

    c o n n ~ c t o r s failed

    9n1y

    after

    the maximum moment had

    been attained In cases w h e ~ ~ the connector s t r e ~ g t h was greater than 8

    of

    a d e q ~ a t e

    a flexural fai lure resulted without connector f a i ~ u r e .

    T y p i c ~ l s t r ~ i n m ~ s u r m n t s m ~ on two members are shown in Fig.

    12.

    Compared

    in

    Fig 12 are i d e n ~ i c a l members

    except that

    member

    B3

    had

    sl ight ly

    less than

    adequate cqnnectors whi le

    B6 had

    approximately half

    that number. ~ t u d y of

    these

    straiq diagrams and types of

    failures

    in-

    dicated that the stress

    block

    in th e concrete a t maximum

    load

    was similar

    to the concrete s t r e s ~

    b l o c ~

    in

    members

    with

    an adequate number of connectors.

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    279.15

    7. I

    N L

    U  N e E 0 F S   P

      18

    Previously

    investigators

    have been

    great ly

    concerned

    about

    the

    effect

    of s l ip on the completeness of interaction between slab

    an d

    beam

    , 1- - f rtl f

    v ~ S h ·

    +· O

    This factor has

      ~ e n

    i g n o r e ~ i n considering

    the

    ultimate strength of

    members The maximum sl ip measured

    a t

    th e end

    of

    the beam wil l

    be used

    in the

    i l lus t ra t ions

    which

    follow to show that s l ip is not a

    s ignif icant

    parameter

    when consi de ri ng t he ultimate strength of members

    A careful reco rd o f s l ip was made

    on the three

    members B10 Bll

    and B12

    Maximum

    end s l ip for these members is plot ted as abscissa in

    Fig 15 with applied moment divided by theoret ical ultimate moment

    plot ted

    as ordinate.

    The curves for these members with midspan deflect ion

    instead of s l ip plot ted as abscissa

    nearly

    coincided. However there is

    considerable

    d if fe re nc e i n

    Fig

    15

    between

    th e

    curve

    for

    B 2

    and

    the

    curves

    for

    BlO

    an d Bll. At M M

    u

    of

    0 80 th e maximum end s

    l ip for

    members

    BlO

    an d

    Bll is n ea rl y t hr ee times

    the

    value of B12 However a t a

    higher

    load

    the

    connector forces in

    the

    three members become

    redis t r ibuted

    an d

    the

    sl ip

    of the three members becomes more nearly

    equal.

    This

    is

    somewhat

    analgous

    to the redistribution of load which takes place in a

    r iveted

    jo int af te r

    y ie ld in g o f the

    r ivets

    occurs

    This further

    i l lust ra tes that the spacing

    of connectors need not be in accordance with

    the shear

    diagram.

    To further i l lust ra te

    that

    s l ip is not an important factor a t

    ultimate

    l oad consider t he load versus maximum end sl ip

    curves

    of members

    BI

    BII an d BIll given in Fig. 16. In Fig. 16 the maximum en d sl ip is

  • 8/20/2019 Compostie Beams

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    279.15

    plot ted as abscissa and th e applied moment divided by the theoretical

    ultimate

    m o m ~ n t is p ~ o t t e d

    as

    ordinate. All

    three of these members

    are

    ident ical in

    cross

    section

    concrete

    strength

    and

    loading

    condition.

    The members d i f f ~ r e d only

    in

    n ~ m b e r of shear connectors in the

    shear

    span

    although

      l l

    members had more than a d ~ q u a t e shear

    connectors

    t

    will be

    n q t ~ c e d

    that   l l

    t h r e ~

    members reached

    the

    theoretical ultimate

    strength.

    However the maximum end s l ~ p

    of

    the member with the leas t

    number of c o n n e c t o r ~ was approximately four

    times

    the maximum sl ip of

    the

    member with the most c o n n ~ y t o r s t should aleo

    noted

    that

    the

    tot l

    amount of

    sl ip

    shown up

    to about

    60 of

    ultimate

    moment in both

    Figs 15

    and 16 is less than 0 02 inch This

    is

    ~ e s s th an tw ice

    the

    thickness

    the le t te r

     1

    on

    ~ h i s page

    an amount which cal . not be

    considered

    as

     

    19

    disastrous

    structural

    d ~ m g e fp e

    engineer

    need not

    pay

    any at tent ion   ~

    to this because i t would nqt affect the strength of beam. The sl ip

      t working load in a n o n c o m p o s i t ~ beam could be ten

    times

    this amount.

    The midspan

    deflection is

    plot ted

    as ~ b s c i s s a

    for the same

     

    members BI ~ I I and BIll Fig 17 with the applied moment divided by

    t h e o r e t i c ~ l ultimate moment as ordinate The

    t h r e ~

    moment versus  

    deflection

    curves

    n e a r ~ y

    coincide throughout

    the

    loading range

    and

    fact do coincide   t

    loads

    near ultimate.

    This further

    i l lust r tes that

    sl ip does not a f f ~ c t magnitude of the

    u l ~ i m a t e

    moment provided that

    the

    number of shear c

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    279.15

    8 CON

    T

    U 0 U S M E M B E R S

    The design of

    comppsite

    construction might be made even more

    economical

    by applying the

    concepts of

    plast ic analysis along with ul

    timate strength

    design.

    To i n v e ~ t i g a t e whether this application

    of

    plast ic design

    is

    feasible one

    two span

    continuous member designated as

    B 3 was

    tested. This

    member was ident ical to members Bl

    through

    B in

    cross

    section and c on sis te d o f two

    f i f t e ~ n foot spans

    The

    ultimate strength

    of this member

    d ~ t e r m i n e d

    using

    both

    plast ic analysis and ultimate s t r ~ t h theory. The ultimate moment of

    the

    posi t ive

    moment

    region

    was taken as M

    u

    of

    the composite section

    w h r ~ s the ultimate moment

    of the

    negative moment region was taken as

      the

    s tee l member

    plus t he loqgi tud inal

    slab reinforcement.

    The

    m e ~ b e r

    was tested

    f i r s t

    by l oa ding only

    one span

    a t a

    time

    and

    stopping

    the loading

    below

    u l t i ~ t e Final ly the member was tested

    to fai lure with two concentrated loads on each sp an Fig 18

    s h o ~ s

    the

    midspan

    deflection of

    both

    spans

    plotted

    as abscissa with

    th e

    total

    ap

    plied load P divided by

    theoret ical load a t

    collapse P

    p

      The load

    P

    p

    was exceeded

    in the

    t es t

    even

    though

    the

    value of ~ q u was

    only

    0.888

    for

    the

    ends and

    0.978

    for the in te r ior portion

    of

    the two span

    member

    t was observed d u r i n ~ the tests of this member that wide

    cracks

    formed

    in t he n eg at iv e moment region even a t loads below working

    load.

  • 8/20/2019 Compostie Beams

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    279.15

      21

    A means of

    controlling

    this cracking should be employed

    in

    the design

    ei ther

    in the

    form

    of an expansion jo int

    or

    suff ic ien t slab

    reinforcement

    to

    distr ibute

    cracks along the

    member However

    in

    members

    where

    th e

    negative

    plast ic hinge

    forms

    f i r s t appears

    that composite members could

    be

    designed

    by

    plast ic analysis .   f buil t up

    members were employed

    in

    which

    the positive plast ic hinge

    formed

    f i r s t the rotat ion

    capacity of

    the

    posi t ive h in ge c ou ld

    be insuff ic ient

    to allow

    a mechanism

    to

    form.

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    279.15

      22

    9. CON   LUS I ON S

    The

    ultimate

    strength of composite beams was carefully in

    vestigated

    and

    this

    was used

    as

    a basis for the determination of

    minimum shear

    connector requirements

    for composite members The fol

    lowing c o n c l u s ~ o n s may

    be

    reached

    as a r sul t of th e testing program:

    1.

    III

    t imate

    s t r ngth

    analysis p1P Viaea   defini te

     1

    k ~ d r J J O r J f . h c . o . . f e

    ~ o t N J - N 1 -

    minimum shear

    connector

    r e q u i r e m e n t ~ b s e d upon

    the

    ultimate

    strength

    of

    shear connectors.

    2. The ultimate moment of a member

    wil l

    be attained

    provided

    the

    ultimate

    strength

    of

    the shear

    con

    nectors in th e shea r span equals or

    exceeds

    th e

    3.

    compressive

    force

    in

    t he concret e

    slab.

    The

    shear

    connectors may be

    spaced

    uniformly

      ~

    O _ j ~

     

    /4.

     

    gardless

    of

    th e shape

    of the

    shear

    diagram.

    4.

    The ultimate

    strength

    of a member may be deter

    mined

    i f

    the number of shear connectors

    is

    in

    adequate.

     

    5.

     f number of

    shear connectors

    is

    adequate

    sl ip

    does

    not

    affect

    the

    load

    versus

    deflection

    curve

    within

    pract ical

    l imits .

    6.

    Composite

    members may be designed by plastic

    analysis on a   i m i t e ~

    basis.

  • 8/20/2019 Compostie Beams

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    279,15 -23

    10.

      C K

    NOW

    LED

    G

    MEN

    T S

    .This study is part of a

    research

    project ent i t led  Investigation

    of

    Composite

    Design for

    Buildings

    being carried out

    a t

    the

    Fri tz

    En-

    gineeringLaboratory

    of Lehigh

    University

    under

    th e g enera l d ir ec tio n o f

    Dr. L S Beedle. The investigation is sponsored by the American

    Inst i tute

    of

    Steel

    Construction,

    and

    guidance

    for the

    p r o j e c ~

    is

    sup

    plied by the

      ISC

    Committee on Composite Design

     Dr.

    T R Higgins,

    C h a i r ~ n The original p l a n n i ~ g of the program was conducted under the

    supervision of Dr Bruno Thurlirnann.

    W e ~ d e d

    stud shear connectors

    for the

    experimental

    investigation

    were supplied and welded by

    KSM Products,

    Inc

    Moorstown,

    New Jersey.

    The

    tests were

    planned and conducted by Messrs . Charles

    G

    C ~ l v e r

    and Paul

    J.

    Zarzeczny

    as a part

    of

    their

    programs

    for the Master

    of

    Science

    Degree. The

    authors

    wish to express their t n ~ s to

    Mrs. Dorothy Fielding

    who did the typing and for Mr Richard Sopko for his

    assistance

    with the

    drawings.

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  • 8/20/2019 Compostie Beams

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    279.15

      P

    P N

    D

    I .

    X NOT   T  ON  continued

    -25

     

    theoret ical

    ult imate

    moment

    for

    member

    with inadequate

    u

    shear

    connectors

    P   to ta l applied

    load

    P

    p

      theoret ical plast ic collapse load

    qu  

    ult imate

    strength

    of

    a

    shear

    connector

    qu   sum

    o f u ltim ate

    strengths

    of a l l shear

    connectors in

    shear

    span

    Q  s ta t i ca l moment of transformed slab area

    t  

    thickness of concrete

    slab

    T  

    tens i le force

    in

    the .gteel

    member

    v   horizontal shear per uni t

    len gth o f

    member

      to ta l

    applied shear

    w  

    length

    of channel shear connector

  • 8/20/2019 Compostie Beams

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    279 15 26

      2 TAB L S F

     

    GU

    RES

  • 8/20/2019 Compostie Beams

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    279.15.-

    TABLE 1.

    SUMM RY

    OF

     E M TESTS

    -27

     

    Specimen

    Reference Steel

    Size

    Test

    Type of

    Connector

    Concre

    Section

    Concrete Span Connectors Spacing

    Streng

    Slab

    (in.

     

    (psi

    B1

    *

    12

     

    27

    4 x 48

    15 -0

    11

    None

    ---

    360

    B2

    *

    12   27

    4 x 48

    15 -0

    11

    None

     

    360

    B3

    *

    12   27 4 x 48

    15

     -a  

    1/2

    11

    studs 2

    @ 7.5 360

    B4

    *

    12   27 4 x 48

    15 -0

     

    1/2

    11

    studs

    2

    @

    .7.5

    360

    B5

    *

    12  

    27 4 x 48

    15 -0

     

    3

    C 4.1

    4

    @

    20

    360

    B6

    *

    12   27 4 x 48

    15 -0

    11

    1/2  

    studs

    1

    @

    7.5 360

    B7

    * 12

     

    27 4 x 48

    15 -0

     

    J/2

    11

    studs

    2

    @

    .7.5

    333

    \

    B8

    *

    12   27 4 x 48

    15 -0  

    1/2

    11

    studs

    2

    @

    7.5

    333

    B9

     i t

    12

     

    27 4 x 48

    15  -0 1

    3/4

    11

    studs 2

    @

    15

    333

    B10

    *

    12   27

    4 x 48

    15

     -a 

    1/2

    11

    studs

    2

    @

    9

    359

    B11

    *

    12   27 4 x 48

    15 -0

    11

    1/2

    11

    studs

    2

    @

    9

    359

    B12

    *

    12 W 27

    4 x

    48

    15

    -0

     

    1/2  

    studs

    Variable

    359

    BI

    5

      Vf

    17 3 x 24 to  -a

     

    1/2  

    studs

    3

    @

    5.5 556

    BII

    5

     

    17

    3 x

    24

    10

     -0

     

    1/2  

    studs

    2

    @

    5.5

    556

    BIll ·

    5

     

    17 3 x 24

    10 I

    -0

     

    1/2

     

    studs

    2

    @

    7 556

    B21S

    6

    21  If 68 6.25

    x

    7

    37 -6

    11

    4

    C

    5.4

    I

    6

    @ 14.5

    648

    B21W

    6

    21

     If 68

    6.17

    x  

    37 -6

    11

    4

    C

    5.4

    4

    @

    36

    558

    B24S

    6

    24  If

    76

    6.25 x 7

    37 -6

    11

    41:

    5.4

    6

    @

    14.5

    562

    B24W

    6

    24   76

    6.11

    x

    7

    37 -6

    11

    4 [

    5.4

    6

    @

    18

    550

    Bridge

    7 18   5

    6 x

    65.5

    30

     -0  

    1/2

    11

    studs

    3

    @

    14

    328

    1 8

      If

    17

    7.5

    x 30

    21

    -0

     

    Spirals

    Variable

    738

    2

    8

      17

    7.5

    x 30

    21 -0 Spirals

    Var:iab1e 704

    3

    8

     

    17 7.5 x 30

    21 -0

     

    Spirals

    Variable

    738

    4

    8

     

    17

    7.5

    x

    30

    21

     -a

    Spirals

    Variable 704

    *Tests performed

    in th is in ve stig atio n

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    TABLE

    20

    SU RY

    OF

    BEAM

    IEST RESULTS

    -28

    Member

    Test

    Type of

    Maximum

    Theoretical

    Values

    Apparent

    Maximum

    Maximu

    Failure

    Test

    Mu

    Mu

    Connector Force

    End Sl

    Moment

    (*)

      f

    (kip-in.  

    (kip-ino)

    (kip-ino) (kips per Connector)

    (ino)

    B3 T2

    A 2708 2880

    --

    1204 (per

    1/2

    stud) 0.040

    I4

    A 2636 2880

    --

    12.9-

    0.077

    T7

    D 2514 2880

    2647 1507 0.092

    B4

    T2

    A

    2571 2750

    --

    n .7 (per

    1/2

    11

    stud) 00015

    I4

    A

    2546 2750

     

    1205 00020

    T8 D

    2614 2750

    2490 16.6 00126

    B5 T2 A 2695

    2880

    -- 5401

    (per

    4

    11

    channel) 00029

    T4

    A

    2758 2880

    -- 7005

    00046

    I I I

    B

    2418 2880

    2401

    7204 0.207

    B6

    I2 D 2416 2880 2440

    1708 (per

    1/2

      stud)

    0.120

    B7

    T2 A

    2506 27.30

    --

    11.2 (per

    1/2

    11

    stud)

    0.059

    T4

    C

    2554

    2730

    2691

    1300

    0.139

    B8

    T2

    A 2618 2730

     

    1204

    (per

    1/2

    stud)

    0.035

    T4

    A

    2.6.34

    2730

    --

    1400

    0.063

    T9 C 2491 2730 2557

    1504 00129

    T2

    A

    2586

    2730

    --

    22.1 (per

    3/4

    11

    stud)

    0.040

    I5

    A

    2514

    2730

    --

    2604

    0.039

     flO

    B

    2514 2730 2626

    31.4 0.198

    B10

    T13 D

    2596

    2760 271.7 1302 (per 1/2

    11

    stud)

    0.268

    B11

    I13

    D 2556 2760 2717 1208 (per

    1/2

    stud)

    0.199

    B12 .

    I13

     

    2626 2760 2717

    1306

    (per

    1/2

    11

    stud) 0.170

    B1

    I3

     

    1178 1141

     

    700

    (per

    1/2

    11

    stud)

    0.004

    B11

    T3 A 1164

    1141

    --

    1006

    (per

    1/2

      stud)

    00008

    1 4

     

    12.14

    1141

    --

    1201

    0.044

    .

    BIll T3

    A 1154 1141

    --

    1304

    (p er

    1/2

     

    stud)

    00021

    I4

    A

    1146 1141

    --

    15.4

    00071

    I6

    D

    1085 1141 1051

    1606

    0.092

    B21S

    Tl

    C

    12678 11920

    --

    50.8 (per 4

    11

    channel) 0.010

    B21W I1

     

    10057 11480

    9589

    91.7 (per 4

    channel)

    00077

    B24S

    I l

    A

    14100

    13600

    -- 54.3

    (per 4

    channel)

    0.006

    B24W

    T1

    A

    13690

    13710

    --

    51.4

    (per 4

    11

    channel)

    0.009

    Bridge

    Tl C 16740 16455

    -- 1304

    (per 1/2

    stud)

    0.028

    IFl

    Il2

    C

    2572 2.150

    --

    17.0

    (per 1/2

    spiral)

    0.006

     

    . T12 A

    2362

    2i50

    --

    15.6 (per

    1/2 spiral)

    00007

     

    . T12

    A

    2272 2150

    --

    1500 (per 1/2

    spiral)

    00004

    Ift

    T12 A

    2402 2150

    \

     

    15.9

    (per 1/2

    11

    spiral)

    0.009

    *See Figo 2

    f

    Test

    stopped before fai lure

    B Failure to

    carry

    addit ional load

    C

    Crushing of concrete slab

    D Tensile fai lure

    of

    connectors

    E

    Failure

    by tensi le

    cracking of slab

    F Failure by connectors

    pulling

    out

    of concrete

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    279.15

    TABLE 3a.

    ULTIMAtE

    SIRENGTH

    OF STUD CONNECWRS

    Specimen

    Reference

    Stud type of

    H/d

    Type of

    Concrete

    Max.

    Q

    u

    1t.

    S

    Diameter Test

    Failure

    Strength  

    Slip

    S

      in . )   psi)

      in . )

     

    2

    9

    1/2

    Pushout

    4.5 D 5000

    --

    14.5

    4A

    10

    1/2

    Pushout

    8.0

    D

    3840

    0.163

    14.4

    4B

    10 1/2

    Pushout 8.0 D 4390 0.170 13.9

    B12-T13

    *

    1/2 Beam 4.5

    D

    3595 0.170

    13.6 6

    Bridge

    7

    1/2

    Beam

    3.8

    C 3280

    --

    13.4

    .BlO-I13

     

    1/2

    Beam

    4.5

    D

    3595

    0.198

    13.2

    B7-T4

    *

    1/2

    Beam

    4.5

    C

    3337

    0.139 13.0

    3

     9

    1/2

    Pushout

    4.5 D

    5000

    --

    12.9

    B11-l 13

     

    1/2 Bea m 4.5 D 3595

    0.199 12.8

    P5

     

    1/2

    Pushout

    4.5 D

    3600

    0.265

    12.1

    P6

    *

    1/2

    Pushout

    4.5

    D

    3680 0.290

    12.1

    .

    P8

     

    1/2

    Pushout 4.5  D 3063

    0.335

    12.1

    Pl

    *

    1/2 Pushout

    5

    ·D

    3600 0.200

    11.0

    P4

    *

    1/2

    Pushout

    4.5 D

    3600

    0.190 10.4

    SA

    10

    .5/8

    Pushout 6.3

    D

    3790

    0.319

    23.8

    5B

    10

    5/8

    Pushout

    6.3

    ·D

    4250 0.279

    22.5

    6F

    10

    3/4

    Pushout 6.7 D

     g

    0.364

    34.8

    6B

    10 3/4

    Pushout 5.2

    D 4240

    0.246

    32.5

    6A

    10

    3/4

    Pushout

    5.2

    D

    3870

    0.382 32.0

    6G

    10

    3/4

    Pushout 9.3

    D 4590

    0.276

    31.5

    7H

    10 7/8

    Pushout

    10.0

    D 3440

    0.278 45.0

    *Performed this

    ~ n v s t ~ g t i o n

    TABLE

    3b .

    ULTIMA IE

    STRENGTH

    OF SPIRAL CONNECTORS

    Specimen

    Reference

    Spiral Type of Type

    of Concrete

    Max.

    Qu1t.

    S

    Diameter

    Iest

    ,Failure

    Strength Slip

    S

      in . )

      ps i)

     

    4A

    10 1/2

    Pushout

    D

    2990

    0.250 34.5

    4B

    10

    1/2

    Pushout

    D

    2990

    0.247

    29.3

    5B

    10

    5/8

    Pushout

    E

    3520

    0.139

    5A

    10

    5/8

    Pushout

    E

    3520

    0.190 43.7

    2-1

    11

    5/8

    Pushout

     

    4540

    0.047

    42.9

    2-2

    11

    5/8

    Pushout

    D

    3080

    0.068

    38.5

    1 1

     

    ,3/4

    Pushout D

    5120

    0.023 58.3

    6B

    10

    3/4

    Pushout

    E

    3250

    0.075

    54.9

    6A

    10 3/4

    Pushout

     E

    .3250

    0.088

    52.3

     

    1-2

    U

    3/4

    Pushout

    E 2965

    0.034

    .51.1

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    279.15 -30

     fABLE

    3c. ULTIMATE

    STRENGTH

    OF

    CHANNEL

    CONNEC ORS

    Specimen

    Reference

    Size of

    Type

    of

    Type

    of

    Concrete

    Load per

    Channel Test

    Failure Strength

     in. 

    B5

     

    3

    t

    4.1

    Beam

    C

    3600

    18.1

    3C 3H3

    6

    3 t

    4.1

    Pushout

    D

    3920 14.9

    3C 3H2

    6

    3 C 4.1

    Pushout

    D

    3310

    12.6

    P2

     

    3 C 4.1

    Pushout

    E

    3600

    11.9

    3C 3H

    6

    3 C

    4.1

    Pushout

    D

    2810 10.5

    B2 W

    6

    4 C 5.4

    Beam

    C

    558Q

    22.9

    4C 3W2

    6

    4 [

    5.4

    Pushout

    D

    4430

    20.4

    4C 3ell.

    6

    D

    6320

    19.

     

    4C 3C9

    6

    D

    5340 19.4

    4C 3e10

    6

    D

    5740

    18.7

    4e 3e7

    6

    D

    4140

    17 .1

    4C 3eB

    6

    D

    4770

    16.4

    4C

    3F4

    I

    ]}I

    4690

    16.2

    4C 3e 6

    6

      l

    3500

    15.8

    4C 3C5

    6

    D

    3470

    15.2

    4C

    3F3

    6

    D

    4600

    15.1

    4C 3S2

    6

    E

    T970

    15.0

    4C 3W

    6

    D

    2810

    15.0

    4C

     c

    6

    D

    3140

    13.2

    4e 3e1

    6

    D

    2010

    12.5

    4C 3F2

    6

    ·

    2650 12.4

    4C 3F5

    6 D

    3080

    1203

    4C 3C2

    6

    D

    2300

    12.1

    4C 3D2

    6

    D

    3310

    11.6

    4C 3e3

    6

    D

    2510

    11.2

    4e

    3D

    6

    D

    2990

    9.9

    4e

    3Fl

    6

     

    it

    D

    2580

    9.6

    4C 381

    6. E

    1340

    8.0

    4C

    5 8

    6

    4 [ 1.25

    Pushout

     .I 1.

    5050 21.8

    .4C 5 I7

    6

    D

    4360

    17.1

    4C 4T

    6 D

    4010

    16.4

    4C 5F

    6 D

    2110

    16.4

    4e

    5T6 6

    D

    3530

    15.8

    4C 5 f3

    6 D

    3130

    15.1

    4e

    5 2

    6 D

    2910 14.5

    4C 5 I4

    6 D

    3190 14.2

    4C 5 5

    6

    D

    3310 14.1

    4e 5S

    6 D

    2720

    14.0

    4C

    5

    6

    D

    2300

    13.2

    5C 3H2

    6

    5 [

    6.7

    Pushout

    D

    3260 15.2

    5C

    3H 6

    5 L 6.1

    Pushout

    D

    3110

    14.9

      Performed

    in this

    investigation

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    ~ ~ r ~ T : ~ : ; : : i

     

    L4

    N=

    I

    SECTION  

    ELEVATION 8 TO 8 2

     

    ELEVATION 8

      3

      ig DETAILS OF

    TEST

    BEAMS   l THROUGH

    B

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    279 15

     33

     I

    L

     

    8

     b

    4

    L

     

    1 1

    88

    L

     

    8

    t

     

    P

    4 4

    l

     

    t

    L

    L

     

    2

     

    2

    I

    I

     

    t

    L

     

    \

    I

    Test TI Test TI

    L

     b b

     b L L

     

    p

     5

     

    L

     I

     ·

    L

     

    Test

    x in inches

    Test

    TI

    T2

    9

    T3

      2

    T4

      8

    T5

    2

    T6

    23

    T7

    28

    T8 30

    T9

    33

    TIO

    36

    Til

    38

    Fig 2 SUMMARY OF LOADING CONDITIONS

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    v

     

    \J

    ELEVATION

    Spherical Bearing

    612 6

    Mesh

    Plywood

     

     

    r

    1

    ~ i =

    A l I ~

    =

     

    :

     

    I

    i f

     

    -

    1

     

    . .

      :

    :

    1

    ;; .

     

    ...

     

    SECTION B B

    Fig DET ILS OF PUSHOUT SPE IMENS

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    e

    c

     

    - . - -

    r

    _

     

    y

    I

    e

    T

    O 8 f ~

    tC

    N A

    e

    c

    T

    L 0 8 5 f ~

    N.A.-T-

    b

      : .

    p l

    10 :1

    4 ·· ··

    • A·.·

    , I I , •

    J

     

     

    y

      SE  

    y

      SE  

    Fig

    STRESS DISTRIBUTION AT

    ULTIMATE K>MENT

    I

    W

    \Jl

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    x x

     

    p

     

    l

    M

    I   J

    -p P P

    _

     onnector orces

      qu

     

    ig SHE R ONNE TOR FOR ES  T ULTIM TE MJMENT

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    80

    o

    o

    o

    12

     

    o

    o

    o

    o

    • Beam Test

    o

    Pushout Test

    D

    Recent Lehigh U Tests

      AISC Design   t res _

    930

    /3000

      ~ L ~ ~ = = ~ ; -

    As

      8

     eight   iameter

    of

    Stud

     HId

    20

    220

    Hd

    s

      3000

    60 AS

     

    c

     

    40

     

    ig ULTIMATE STRENGTH   STUD SHEAR CONNECTORS

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    8

    o

    6

    o

    o

     

    9

    o

    4

    o Pushout Tests

     

    -----

      o O ~

    S

    o ~ q ~ -

    ~

    ------

     

    ------

     

    60

     

    40

      f

    c

     

    .=

     

    Q)

     

    20

      0

     

    J

    d

    s

      i[ for Spiral

    Fig

    7 ULTIMATE STRENGTH OF

    SPIRAL

    SHEAR

      ONNE TORS

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    3

    o Pushout Tests

    • Beam Tests

    • b Recent Lehigh

    U

    Tests

    en

    C

    c

    .

    2

    Q

    c

    c

     

    s ;

    U

     

    0

     s ;

    1

    c

     

    Q

    C

    0

     

    0

      J

     

    q u = 5 5 0 h + O . 5 t v 1 ~

     

    o

    o

    o

      o

    o cPc9  

    to  

    o  

    o  

    2

    3

    o

    4

    h+O.5t for

      hannel

    Section

    Fig 8 ULTIMATE STRENGTH OF CHANNEL SHEAR CONNECTORS

     

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    279 15

     40

    M/M

    u

    1

    Loads Suspended from

    Steel Beam

    Bl

    T2 - o -

    Slab

    and Beam

    Separated

    2 3

    4 5

     in

    1 0

    B

    T2 - o -

    80n

    0

    2 3

    4 5 8 in

    c

    B3

     

    E

    T2 - o -

     

    T ~

    T ~

     ; -.

     

    0

    0

    4

    5

    8 in

    ~

      >

    Loads

    Suspended

    +

    from Steel Beam

    B4

     

    T

    c

    T ~

     

    E

    T 8 ~

    0

     

    0 2 3

    4 5

    80n

    -0

    Q

    a

    B5

    a

    «

    T

    T ~

      ~

    0

    4 5

    8

     in

    1 0

    B6

    T

    Midspan Deflection in Inches

    Fig

    9

    MOMENT DEFLECTION CURVES

    FOR BEAMS

      l

    TO B6

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     4

    279 15

    M M

    u

    1

    87

    T2  

    T4

     

    2 3

    4 5

    8 in

    88

    T 2 o

    T4

     

    T9  

    2 3 4 5

    8 in

    :

    Q

    E

     

    89

    Q

    T2  

    T5

     

    TIO O

    ::J

    -I-

      2

    3

    4

    5

     

    c:

    81

    E

     

    T13

    0

    Q

    a.

      2 5

    8  in

    .

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    M/M

     

    =0 846

    M M

    u

    =0 908

    8

    o qu

     

    =0 944

    86 T2

     

    qu

     

    =0 473

    M/M

    u

    =0 744

    M M

     

    =0 858

    Strain Distri bution at Midspan

      ig MEASURED

    STRAINS

    ON M M RS AT MIDSPAN

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      ' , >

     i : ' ' :

      ::

    .,.'.'-:   :

    ....

     ,::

      .;.:-: ::

    ;'.

     

    .F

    :

    ~ c o

    ~ § 8 § 5 § f ~

     

    _N _

     

    I

     

    d

      _ 

    ig

    STRESS

    DISTRIBUTION  T MO IFIE ULTIM TE MOMENT

      I I ~ T . . . .

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    M M

    u

      t

    1

    Q

    § 0 8

     

    Q

    E

      0.6

    ::>

     

    Q

    E

     

    0.4

      C

    Q

    .

    a

    a

    0 2

     Lqu C 

    888

    for

    all

    Members

    o B 12 Variable Connector Spacing

    o B II Uniform Connector

    Spacing

    B

    1

    Uniform Connector Spacing

    o

    0 05 0.10

      15

    0 20

    Maximum End

    Slip

    in Inches

    Fig 15 MOMENT END SLIP CURVES FOR TESTS OF   ID Bll

    and

    B 2

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    M M

     

    1

    .

    I

    VI

    o Test S I T3 Iqu C = 2 4

    • Test SIT T3

    Iqu C

    = 1 36

     

    Test

    Sm T3 I

     

    C= 1 06

     

    c

    Q)

    E

    0

     

    Q)

     

    c

    E

     

    c

    Q)

    E

    0

     

    0

    Q)

     

    Q

    0 2

     

    «

    0.2

      4

    0.6

    0.8

    1

    1 2 1 4

    1 6

    Deflection

    at

    Midspan in

    Inches

    Fig.

    17 MOMENT

    DEFLECTION CURVES

    FOR

    TESTS OF

    BlO,

      ll an d B12

    I

     

    co

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    2 0 0

    P/Pp

     

    3 0 0

     0

    P/Pp ... - - ,

    1 :

    0 8 1 : 8

    c

    c

    0

    0

      J

      J

    Q

    Q

    c

    c

    E

      6

    E

      6

     

    -

    1 :

    1 :

    p p p p

    c

    c

    4 4

    4 4

    0 4

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      4

      J

    rY

     

    :

    1 :

    Q

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    a.

    a.

    a.

    a.

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    279 15   50

    13

    REF

    E R EN C   S

    1

    American

    Inst i tute of Steel

    Construction

    SPECIFICATION FOR THE DESIGN FABRICATION AND ERECTION

    OF STRUCTURAL STEEL FOR BUILDINGS

    .

    New

    York New York 1961

    2 American

    Association

    of State Highway

    Officials

     

    STANDARD SPECIFICATIONS FOR

    HIGHWAY

    BRIDGES 7th

    e d i t i o n ~

    Div I Sect 9 1957

    3.. TENTATIVE RECOMMENDATIONS FOR THE DESIGN AND CONSTRUCTION

    OF

    COMPOSITE

    BEAMs

    AND

    GIRDERS

    FOR.BUILDINGS

    Proceedings

    ASCE

    Vol 8S

    No. ST12 December 1960

    4

    Siess C.

    P Viest I M

    Newmark N.

    M.

    STUDIES

    OF SLAB AND BEAM BRIDGES PART I I I   SMALL

    SCALE TESTS

    OF SHEAR CONNECTORS

    AND COMPOSITE

    T BEAMS

    University of

    I l l inois Bulletin No.

    396

    1952

    5

    Culver

    G.

    and

    Coston R.

    TESTS OF

    COMPOSITE BEAMS

    WITH STUD

    SHEAR.

    CONNECTORS

    Proceedings ASCE Vol

    87 No. ST2 February 1961

    6 Viest 1 M Siess C. P Appleton J H Newmark N. M.

    FULL

    SCALE

    TESTS

    OF CHANNEL

    SHEAR

    CONNECTORS AND

    COMPOSITE

    T BEAMS

    University of

    Il l inois

    Bulletin No.

    405

    1952

    7. Thurlirnann B.

    COMPOSITE

    BEAMS WITH STUD SHEAR CONNECTORS

    Highway Research Board National Academy

    of

    Science

    Bulletin

    No.

    174

    1958

    8

    REPORT OF

    TESTS OF COMPOSITES TEEL AND CONCRETE BEAMS

    Fritz Engineering Laboratory May 1943

    9

    10

    Thur lirnann B.

    FATIGUE AND STATIC STRENGTH OF STUD

    SHEAR CONNECTORS

    ACI  Journal

    Vol

    30 June 1959

    Viest 1 M.