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Design TBeam

Apr 14, 2018

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    Analysis and design of T-beam

    Effective Flange Width be

    Portions near the webs are more highly stressed than areas away fromthe web.

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    Analysis and design of T-beam

    ACI Code Provisions for Estimating beff

    According to ACI code, effective flange width of a T-beam, beis notto exceed the smallest of: One-fourth the span length of the beam, L/4. Width of web plus 16 times slab thickness, bw+16 hf .

    Center-to-center spacing of beams, bactual.

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    Analysis and design of T-beam

    ACI Code Provisions for Estimating beff

    According to ACI code, effective flange width of a L-beam, beis notto exceed the smallest of: bw+ L/12. bw+ 6 hf .

    bw+ 0.5x(clear distance to next web).

    For isolated T-beams, the flange thickness is not to exceed half the webwidth, bw/2 , and the effective flange width be not more than fourtimes the web width, 4 bw.

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    Analysis and design of T-beam

    T- versus Rectangular Sections

    Compression zoneTension

    zone

    Sec A-A Sec B-B

    When T-shaped sections are subjected to negative moments, the flange

    is located in the tension zone. Since concrete strength in tension is

    usually neglected in ultimate strength design, the sections are treated asrectangular sections of width bw and when sections are subjected to

    positive moments, the flange is located in the compression zone and

    the section is treated as a T-section.

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    Analysis and design of T-beam

    Strength of T-Beam

    effc

    ys

    yseffc

    b'f0.85

    fA

    aTCmequilibriuFrom

    fAT&ba'f0.85C

    Case 1:when a hf [Same as rectangular section]Assume steel yields

    1] Equilibrium

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    Analysis and design of T-beam

    2

    adfAM ysn

    004.0003.0c

    cd

    ac

    t

    1

    Case 1:when a hf

    2] Confirm

    3] Calculate Mn

    Strength of T-Beam

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    Analysis and design of T-beam

    wc

    fwcys

    wf

    ys

    wcw

    fwcf

    bf0.85

    hbbf0.85-fA

    CC

    fATabf0.85C

    hbbf0.85C

    a

    T

    Case 2:when a > hf Assume steel yields

    1] Equilibrium

    From equilibrium of forces

    Strength of T-Beam

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    Analysis and design of T-beam

    004.0003.0c

    cd

    ac

    t

    1

    2

    hdC

    2

    adCM ffwn

    Case 1:when a > hf

    2] Confirm

    3] Calculate Mn

    Strength of T-Beam

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    Analysis and design of T-beam

    Minimum Reinforcement, As,min

    dbf

    14.06

    dbf

    f8.0

    oflargerA

    wy

    w

    y

    c

    s(min)

    bw

    dhf

    As

    beff

    bw

    d

    hfAs

    beff

    +veMoment

    -veMoment

    dbf

    14.06db

    f

    f0.8

    dbf

    f1.6

    ofsmallerA

    eff

    y

    eff

    y

    c

    wy

    c

    s(min)

    Flange in compression

    Flange in tension

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    Analysis and design of T-beam

    Flange Reinforcement

    Main Reinforcement

    min (beff & l/10)Additional

    ReinforcementAdditional

    Reinforcement

    -vemoment

    when flanges of T-beams are in tension, part of the flexuralreinforcement shall be distributed over effective flange width, or a

    width equal to one-tenth of the span, whichever is smaller

    If beff > l/10, some longitudinal reinforcement shall be provided inouter portions of flange.

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    Analysis and design of T-beam

    Analysis of T-Beam

    'f0.85

    fAATCmequilibriuFrom

    c

    ys

    c

    bw

    dhf

    beff

    Af

    1- Check As,used >As,min

    2- Compute T = Asfy

    3- Determine the area of the concrete in compression (Ac) stressed to

    0.85fc

    If Ac Af = beff x hf [a < hf ]

    If Ac > Af = beff x hf [a > hf ]

    4- Calculate a, c, and checkt (t 0.004; < max)

    5- Calculate Mn.

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    Example 1

    Example Problems

    2

    useds,

    2

    mins,

    mins,

    w

    y

    w

    y

    c

    mins,

    cm42.41(7.07)6Acm5.08A

    60.725420014.0660.7525

    42002800.8A

    dbf

    14.06db

    f

    'f0.8A

    cm60.752

    2.531.0470d

    25

    630

    10

    150

    70

    10

    Determine the ACI design moment strength Md (Mn )of the T-beamshown in figure if fc =280 kg/cm

    2 and fy= 4200 kg/cm2.

    Solution:-

    1- Checking min. Steel Percentage

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    Example 1

    Example Problems

    25

    630

    10

    150

    7

    0

    10

    ton178.1210

    420042.41fAT

    3ys

    cm10cm0.535.7

    178.12a

    TCforcesofmequilibriufrom

    tona7.5310

    a1500.85(280)ba'0.85fC3c

    2- Compute T and a

    assuming that a < hf= 10cm

    i.e. assumption is rightSame as rectangular section

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    Example 1

    Example Problems

    25

    630

    St.10

    150

    7

    0

    10

    t.m93.382

    5.060.75

    10

    178.120.9

    2

    a

    dTM

    0.90.0050.028

    0.0035.88

    5.8860.750.003

    c

    cd

    cm5.880.85

    5.0

    ac

    2

    d

    t

    t

    1

    3- Calculate Mn

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    Example 2

    Example Problems

    2

    useds,

    2

    mins,

    mins,

    w

    y

    w

    y

    c

    mins,

    cm34.46(8.04)8Acm6.6A

    55.6503420014.0655.6503

    42002500.8A

    dbf

    14.06db

    f

    'f0.8A

    cm55.652

    2.53.21.0475d

    30

    832

    1075

    10

    90

    Determine the ACI design moment strength Md (Mn )of the T-beamshown in figure if fc =250 kg/cm

    2 and fy= 4200 kg/cm2.

    Solution:-

    1- Checking min. Steel Percentage

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    Example 2

    Example Problems

    ton23.70210

    420034.46fAT

    3ys

    cm10cm13.1419.13

    270.23a

    TCforcesofmequilibriufrom

    tona13.1910

    a090.85(250)ba'0.85fC3c

    30

    832

    1075

    10

    90

    abf0.85C

    hbbf0.85C

    wcw

    fwecf

    2- Compute T and a

    assuming that a < hf= 10cm

    i.e. assumption is wrong

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    Example 2

    Example Problems

    cmaa

    C

    a

    f

    39.2238.65.12723.270

    CTforcesofmequilibriufrom

    ton38.610

    a032500.85ba'f0.85C

    ton127.510

    1030902500.85h)b(b'f0.85C

    w

    3wcw

    3fwecf

    855.0)00447.0(3.83483.0

    3.83483.00.0040.00447

    0.00326.34

    34.6255.650.003c

    cd

    cm34.620.85

    22.39

    ac

    tt

    t

    1

    3- Calculate and Md

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    Example 2

    Example Problems

    mt

    hdC

    adC

    tonaC

    f

    fw

    w

    .34.132

    2

    1055.655.127

    2

    39.2255.6574.142

    10

    855.0

    22M

    74.14239.2238.638.6

    2

    d

    3- Calculate Mn

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    Analysis and design of T-beam

    Design of T-Beam

    bw

    dhf

    As

    beff

    2

    ef fc

    u

    5

    y

    c

    db'f0.85

    M2(10)11

    f

    'f0.85

    effc

    ys

    b'f0.85fAa

    The design of a T-section involves the determination of 5 unknowns;be , hf , bw , h , and As.

    1- Establish hfbased on flexural requirements of the slab.

    2- Determine be according to ACI limits.

    3- Choose bwand d4- CalculateAs assuming that a < hfwith beam width = beff & =0.90

    As = beffd

    5- If a < hfthe assumption is right & if not reviseAs using T-beam equations.

    6- Check to ensure that t0.004 and min

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    Example Problems

    Example 1

    Spandrel

    beam

    10

    .0m

    3.0 m

    3.0 m

    3.0 m

    hf Slab

    bw

    A floor system consists of a 14.0cmconcrete slab supported by continuous

    T-beams with a 10m span, 3.0m on

    centers. Web dimensions are bw=30cm

    and d=55cm.

    Use fc =280 kg/cm2 and fy = 4200 kg/cm2

    Requireda] What tensile steel is required at midspanto resist a service dead load moment 32t.mand a service live load moment 25t.m.

    b] What tensile steel is required at supportto resist a factored moment 50t.m

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    Example 1

    Example Problems

    30

    5514

    As

    200

    2

    ef fc

    u

    5

    y

    c

    db'f0.85

    M2(10)11

    f

    'f0.85

    55

    30

    As

    14

    200

    78.4

    t.m

    beff is the smallest of:- l/4 = 800/4 = 200 cm

    - bw+16(hf) = 30 +16 (14) = 254 cm

    - Center-to-center-spacing of beams = 300 cm

    beffis taken as 200 cm, as shown in Figurea] for positive moment

    Mu+ve = 1.2(32)+1.6(25)=78.4 t.m

    Assuming that a

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    Example 1

    Example Problems

    2

    2

    5

    93.385520000354.0

    00354.0

    550028020.859.0

    4.8710211

    4200

    2800.85

    cmdbA effs

    OKcm39.27Acm5.52A

    55304200

    14.065530

    4200

    2800.8Adb

    f

    14.06db

    f

    'f0.8A

    14cmhcm3.472002800.85

    420039.27

    b'f0.85

    fAa

    2

    useds,

    2

    mins,

    mins,w

    y

    w

    y

    c

    mins,

    f

    effc

    ys

    30

    5514

    As

    200

    78.4

    t.m

    Use 825mm (As,used= 39.27 cm2) arranged in two layers.

    The assumption is right

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    Example 1

    Example Problems

    OK9.0005.00374.0

    0.0034.08

    08.4550.003

    c

    cd

    cm08.40.85

    3.47

    ac

    t

    1

    t.m78.4Mt.m79.072

    3.47

    5510

    420039.270.9

    2

    adfAM

    u5

    ysd

    55

    308

    25

    14

    200

    Check=0.9

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    Example 1

    Example Problems

    2wc

    u

    5

    y

    c

    db'f0.85

    M2(10)11

    f

    'f0.85

    30

    55As

    50t.m

    2

    2

    5

    35.2855300172.0

    0172.055308020.859.0

    5010211

    4200

    2800.85

    cmdbA ws

    b] for negative momentMu-ve= 50 t.m

    Rectangular section with b=bw

    Mu= 50 t.m, bw= 30cm, d=55cm and assume that =0.9

    Use 625mm (As,used= 29.45 cm2) arranged in one layers.

    Distribute the bars over a distance [min. (200, l/10=800/10=80)]=80cm

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    Example 1

    Example Problems

    55

    30

    14

    200

    80

    As

    Check As,used > As,minFlange in tension

    OK2useds,2

    s(min)

    2

    2

    s(min)

    cm29.45Acm10.52A

    cm36.82552004200

    14.06

    552004200

    2800.8

    cm10.5255304200

    2801.6

    A

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    Example 1

    Example Problems

    t.m50Mt.m6.152

    17.3355

    10

    420045.290.9

    2adfAM

    ]004.0[

    0.90.0050.0051

    0.00320.38

    38.02550.003c

    cd

    cm38.020.85

    17.33

    ac

    33.173028085.0

    420045.29

    b'f0.85

    fAa

    u5

    ysd

    maxt

    t

    t

    1

    wc

    ys

    used

    m

    55

    30

    1

    4

    200

    80

    As