Column and Foundation Design

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  • 7/30/2019 Column and Foundation Design

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    Exp 4.1

    4.4.1.2

    Column is subjected to an axial load of 373kN Where axial load =

    (w/2 + L/2) x Ultimate load

    ( 12.85/2 + 4.5/2) x 43 = 373 kN.

    A horizontal load due to wind actions on the overall structure is 2.381kN

    The column is 300 mm square by 3300mm long measured from top of foundation to the centre of slab.

    The column is subjected to a 1 hour fire resistance on three exposed sides. Assuming the base spring and

    top is unbraced.

    Cover

    cnom = cmin +

    cdev

    where cmin = max[cmin,b, cmin,dur]

    where

    cmin,b = diameter of bar. Assume 40 mm main bars and 10 mm links

    cmin,dur= minimum cover due to environmental conditions.

    Assuming primarily XC3 / XC4, secondarily XF1, cmin,dur = 35 mm

    cdev = allowance in design for deviation = 10 mm try cnom = 40 + 10

    =50

    = 50 mm to main bars

    or = 35 + 10 = 45 mm to 10 mm links (45+10 = 55mm to main bars) Therefoere use Nominal cover,

    cnom = 45 mm to 10 mm links

    3300mm

    Column

    300 x 300

    Slab

    Foundation

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    Istruct E

    T5.15

    BS EN

    1992-1-1

    6.4.5

    2.4.2.4.1

    5.1

    Fire resistance

    Fire resistance R 60 and use conservative value offi = 0.7

    Therefore Minimum dimensions = 300 and a= 40mm

    check on cnom: 45mm + 40mm/2 = 65 mm > 40 mm

    Effective depth d

    d = 350mm - 65mm =285 mm ;d =285mm

    Design yield strength of reinforcement

    fywd,ef = 250 + 0,25 d fywd 250 + 0.25 x 285 = 321.25 N/mm2

    fywd = k x fyk / s = 1.05 x 500 / 1.15 = 457 N/mm2 therfore fywd,ef =321.25 N/mm2

    Design value of concrete compressive strength

    fck = 30 N/mm2 fcd = cc fck / c = 1 x 30/1.5 = 20 N/mm

    2

    Imperfections of columns

    Imperfections as represented by an inclination , given by

    i= 0hm

    where 0 is the basic value: 0 = 1/200 = 0.005

    h is the reduction factor for length or height = 1m is the reduction factor for number of members = 1

    Therefore i = 0.005 x 1 x 1 = 0.005

    Therefore flexibility of rotation restraint

    k = (i / M)(E / l) where k recommended = 0.1where:

    Mz = Horizontal force x l = 2.381kN x 4.5m = 10.7kNm = 10.7x 106

    n/mm

    cm = fck+ 8 & Ecm = 22 (fcm/10)0.3

    & E = Ecm =33000N/mm2

    I = 300mm x 300mm3

    /12 = 75 x106

    mm4

    k1 = (0.005 / 12 x 106) x (33000 x 75 x 10

    6/4500) = 3.30 > 0.1

    therefore k1 = 3.3 & k2 = (no restrains)

    Io = l x max { (1+10 x 1)1/2 = 111/2 = 3.32 ; (1 + 3.3/4.3) x (2) = 3.5}

    lo = 4.5 x 3.5 = 15.74 m = 15740mm

    e i = eccentricity due to imperfections & e i = i l0/2 = 0.005 x 15.74 /2 = 0.04mm

    ei min = h/30 but not less than 20 mm 300/30=10mm ei min = 20mm < 30mm

    ok

    321.25

    N/mm2

    20 N/mm2

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    5.8.3.2

    5.8.8.2

    First order moments

    M02 = Mz + ei x Ned2.381kN x 4.5m + 0.04 x 373 = 25.63 kNm

    Slenderness

    Slenderness = lo/i

    where i = ( I/A)

    i = Radius of gyration

    = 15740mm / (75x 106/(300x300)) =545

    Slenderness lim

    lim = 20 ABC / n0.5

    here A = 1 / (1+ 0.2ef)

    (if ef is not known A may be taken as 0.7)A = 0.7

    B = (1 + 2)^0.5 = 1.1

    C = 1.7 rm C = 1.7 0 = 1.7

    where:

    rm = M01 / M02 = 0 / M02 rm = 0

    n = relative normal force = NEd / Acfcd

    n = 373 x 103 /

    (3002

    x 20) = 0.15

    Therefore lim =(20 0.7 1.1 1.7 / 0.150.5

    ) = 67.6 < 545

    > lim Therefore column is slender about z axis.

    Second order moment

    M2 = nominal 2nd order moment = Ned x e2

    e = 0.1x l2

    x [ Kr x Kx ( fyd / (Es 0.45d))]

    Kr = (nu n) / (nu nbal) 1.0

    where : nu = 1 + = & 1 + 0.39 = 1.39n = NEd/Ac fcd n = 0.15 & nbal = 0.4

    Kr= (1.39 0.15 ) / ( 1.39 0.5) = 1.41 > 1 Therefore Kr = 1.0

    K= 1 + ef 1

    where = 0.35 + (fck/200) (/150)

    = 0.35 + (30/200) (545/150) =-3.13

    K=1 +(-3.13) x 1.6 = -4.28 < 1.0 therefore use = K= 1

    e2 =0.1 x (15.74 x 103)2

    [1 x 1 x (321.25 / (205000 0.45 x 285))] = 303mm

    M2 =303 x 10-3

    x 373 =113 kNm

    545

    0.7

    1.1

    1.7

    303mm

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    Design Moment

    Med = M02 + M2 = 37.2+ 113=150.2 kNm

    Ned = 373 kN

    Therefore Calculating As required by using Column charts

    d/h = 285 mm / 300 mm =0.95 use chart for 0.95

    M/bh2

    fck = 150.2 x 106

    / ( 300 x 3002

    x 30) = 0.19N/bhfck = 373 x 10

    3/ ( 300 x 300 x 30)m= 0.14

    Therefore: chart value = 0.3

    As = 0.3 x b x h x fck / fyk = 0.3 x 300 x 300 x 30 / 500 = 1620 mm2

    Check minimum reinforcement!

    Rules for detailing

    Longitudinal reinforcement

    As,min maximum of (0.1NEd/fyd ; 0.002Ac)

    As,min = 0.1 x 373x 103

    / 321.25 = 116mm2

    0.002 x 3002

    = 180mm2

    As,req = 1620mm2

    As, prov = 1625mm2

    As, max < 0.04 Ac < 0.04 x 3002

    = 3600mm2

    > 1625mm2

    Transversal reinforcement

    Smax = 20 x 30= 600mm

    Smax = < 300mm

    Smax = 400

    Therefore Smax = 300mm

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    Concise

    EC2

    Design BasisThe limit states of stability strength and serviceability needs to be considered.

    Design Action

    Permanent load

    Slab = 25 x 3.5 x 2.25 x 0.22 = 43.31 kN

    Roof = 2.35 x 3.5 x 2.25 = 18.51 kN

    Beam = 25 x 0.5 x 0.3 x ( 3.5 + 2.25) = 21.56 kN

    Column = 25 x 0.3 x 0.3 x 2.38 = 5.36 kN

    Sum of permanent load = 43.31 + 18.51 + 21.56 + 5..36 + 0.2 ( services) = 88.94 kN

    Therefore Gk= 88.94 kN

    Variable load

    Imposed load = 0.6 kN/m2

    x 3.5 x 2.25 = 4.725kN

    Horizontal load ( wind action )

    Assuming half of the wind directly hitting the wall acting on the foundation

    Aref = (4.5 x 2.38 )/ 2 = 5.355

    Fwe = 1 x (-0.323 x 5.4) = -1.74 KN

    Fwi = 1 x ( -0.04 x 5.44) = -0.216 kN

    Therefore the total force acting on foundation = -1.74(- 0.216) = - 1.52 kN

    Axial load

    ULS

    NED = 1.35 Gk + 1.5 Qk = 1.35 x 88.94 + 1.5 x 4.725 = 131.63 kN

    HORIZONTAL LOAD (ULS)

    NED = 1.35 x 0 + 1.5 x -1.52 = -2.28 kN

    Design Moment

    From column calculation Design Moment (Med = M02 + M2 = 37.2+ 113=150.2 kNm)

    Therefore determining ULS ( Geo) Assuming 50% permanent action & 50 % variable action

    MED = 29.95 KNm

    Member size of foundation

    To satisfy eccentricity

    e = Med/ Ned = 29.95 / 131.63 = 0.228

    To achieve e d/6 try d = b = 1.36m

    Try 1.5m x 1.5m x 0.8m deep e < d/6

    Ground bearing pressure:

    88.94 kN

    4.725kN

    - 1.52 kN

    131.63 kN

    -2.28 kN

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    Exp 4.1

    Istruct E

    Table B2

    Annex C

    Table C1

    Size of foundation = 131.63 / 120 = 1.097 m2

    ( Area of foundation)Therefore the size of foundation is> 1.097 Thus a moment will add up to the ground pressureHence try 2m x 2 m x 0.8m

    Checking ground bearing pressure

    Nfound = 25 x 2 x 2 x 0.8 = 80 kN

    Structural resistance = NED, found = 1.35 x 80 = 108kN

    P = NED+ NED, found = 373 kN + 108 = 481 kN

    2 = 481 / 2 x 2 29.95 x 6 /( 2 x 22) = 120.25 22.46

    = 142.85 < 168 & = 97.65

    Flexibility of foundation

    d = 2 & d column = 0.3 , h = 0.8 ,Vmax = 0.8

    Therefore V = 2/20.3/2 = 0.85> 0.8 Therefore foundation is flexible.

    Cover

    Cover

    cnom = cmin +cdev

    where cmin = max[cmin,b, cmin,dur]

    where

    cmin,b = diameter of bar. Assume 20 mm main bars

    cmin,dur= minimum cover due to environmental conditions = 40mm

    Assuming primarily XC3 / XC4, secondarily XF1, cmin,dur = 35 mm

    cdev = allowance in design for deviation= 10 mm try cnom= 40 + 10 =50

    = 50 mm to main bars

    d = 800- 50mm = 75020/2 = 740mm

    Yield Strength of reinforcement

    Fywd, eff = 250 + 0.25 Fywd = 250 + 0.25 x 740 = 435 N/mm2

    Fywd = k x fyk/ = 1.05 x 500/1.15 = 457 N/mm2

    K=(fe/fy) k1.05 for steel grade A

    Concrete compressive strength

    Fck = 30 N/mm2

    , fcd = = 1 x 30 / 1.5 = 20 N/mm2

    Flexure design

    Design moment at face of column

    Mean GBP = (120.25 + 142.25)/ 2 = 131.25 kN/ m2

    M = w x v2/2 = 131.25 x 0.85

    2/2 = 47.41 knm

    K = MED / bd2fck = 47.41x10

    6/ ( 1000 x 740

    2x 30)= 0.003

    Limit z/d to 0.95

    ok

    OK

    740mm

    435 N/mm2

    20 N/mm2

    z/d = 0.97

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    Table 6.1

    Z = 0.95 x 740 = 703mm

    Klim > Kf ; Therefore NO compression reinforcement needed

    Reinforcement required

    As = M / ( 0.87z Fyk) = 47.71 x 106

    / 0.87 x 703 x 500 = 156 mm2

    As, min = 0.26 fcm, btd/fyk

    Fctm = 3.08 N/mm2

    Bt = 1

    Asmin = 0.26 x 3.08 x 1000 x 740/500 = 1185 > 156 & 0.0013 x 1000 x 740 = 962 > 156

    Try H20 B : As, prov = 7 x 320 = 2240

    Asreq/As,prov = 1185/2240 = 0.53 : Therefore aggregate needs to be limited to 0 20mm

    Punching shear design

    Ved =Ned = 373KN

    A1 = 3002

    = 0.09m2

    Ved, red = Ved -

    = A1 x ( GBPSelf weight of foundation)

    =0.09 x ( 120.25( 25 x 0.8) = 9kN

    Ved,red= 3739 = 364 kN

    Shear stress at column face

    Ved,max = Ved,red/ud

    D = mean effective depth of slab (dy + dz)/2

    Dy = hCnom0.5 = 800500.5 x 20 = 740

    Dz = hCnom1.5 = 800501.5 x 20 = 720

    D = ( 740 + 720 ) / 2 = 730mm

    Vo = 300 x 4 = 1200

    K = 0.7

    W1 = c12/2 + c1c2 + 4c2d + 16 d

    2+2dc1

    W1 = 3002/2 + 300 x 300 + 4 x 300 x 730 + 16 x 730

    2+ 2 x 730 x 300 = 10913419mm2

    U2 = 2 x 730 = 1460

    U1 = 1460 x 2 = 9174mm

    = 1 + k Med/ved x u1/w1

    156 mm2

    Use

    Asmin

    364 kN

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    Bs EN 1992(6.50)

    = 1 + 0.6 x 47.41/373 x 103 x 9173 / 10913418 = 1 N/mm2Ved,max = 1 x 373 x 10

    3/ 1200 x 730 = 0.43 N/mm2

    Shear resistance of strutVrd,max = 0.5v, fcdFcd = 30/1.5 = 20

    V = 0.6 ( 1FCK/250) = 0.6 ( 130/250) = 0.530.5 x 0.53 x 20= 5.3 N/mm2

    Vrd, max = 5.3 N/mm2 > Ved, max = 0.43 N/mm2

    Maximum shear strength Vrd

    Vrd = Crdc k ( 100, fck)1/3

    Crdc = 0,12

    K = 1 + 200/d = 1 + 200/730 = 1.52

    Vrdc = 0.12 x 1.52 ( 100 x 0.003 x 30 )1/3

    = 0.36N/mm2

    As.bwd = 2240/ 1000 x740 = 0.003

    Vrdc= Vmin x d/a

    Vrdc = 0.035 fck x k3/2 x 2d/a

    Vrdc = 0.035 x 303/2

    x 1.523/2

    x 2 = 0.36 N/mm2

    Uout, eff = x Ved / ( Vrdc x d)

    = 1.52 x 373 x 103/ 0.36 x 730 = 2157mm

    Distance from column face = Uout eef4h / 2

    = 2157mm4 x 800 / 2 = 0.36N/mm2

    Shear stress at Uo2

    Ved,red (Uo2) = 0.5d

    A0.5 = ( 0.5d + dcol/2)

    2

    x = (730 x 0.5 + 300/2)2

    x = 0.83Ved,red = Ved - Ved

    Ved = 0.83 x ( 120.2525 x 0.8 ) = 83.2kN

    Ved,red = 37383.2 = 289.6

    Perimeter at 0.5 d = 0.5 x 730 = 365mm

    Uo5 = 365 x 2 x + 300 x 4 = 3493.4mm

    Ved at U2 = x Ved /( Uo5 x d )

    1.52 x 113 x 103 / ( 3493 x 730 ) = 0.06 N/mm2 < 1.52N/mm2 = Ved

    Therefore No shear reinforcement required

    ok

    0.36N/m

    m2

    2157mm

    0.36N/mm2

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    Therefore N

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