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    Practical Design to Eurocode 2

    Beams

    Bending / Flexure Shear

    Detailing

    Anchorage & Laps

    Members & particular rules

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    Beams

    Flexure

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    Section Design: Bending

    Flexural design is generally the same as BS8110 in

    principle

    Modified for high strength concrete

    EC2 presents the principles only

    Design manuals will provide the standard solutions for

    basic design cases.

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    As

    d

    fcd

    Fs

    x

    s

    x

    cu3

    FcAc

    fck50 MPa 50 < fck90 MPa 0.8 = 0.8 (f ck 50)/400 1.0 = 1,0 (fck 50)/200fcd = ccfck /c

    = 0.85fck /1.5

    Rectangular Concrete StressBlock (3.1.7, Figure 3.5)

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    Maximum neutral axis depth

    M

    b

    MomentBendingElastic

    MomentBendingtedRedistribu du21 xkk EC2 Equ 5.10a

    xu = Neutral axis depth after redistribution

    EC2 NA gives k1 = 0.4 and k2 = 1.0

    dux0.4

    0.4-d

    x u

    ck

    2fbdMK

    Value of K for maximum value of M

    with no compression steel and

    when x is at its maximum value.If K > K Compression steel required

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    Analysis of a Singly ReinforcedBeam3.1.7 EN 1992-1-1

    Design equations can be derived as follows:

    For grades of concrete up to C50/60, cu= 0.0035, = 1 and = 0.8.fcd = 0.85fck/1.5,

    fyd =fyk/1.15

    Fc = (0.85 fck/ 1.5) b (0.8x) = 0.453 fckb x

    Fst = 0.87As fyk

    Take moments about the centre of the tension force

    M = 0.453 fckb x z 1

    M

    b

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    0 = (z/ d)2 (z/ d) + 0.88235K

    Solvi ng t he quadrat ic equat ion:

    z/ d= [1 + (1 - 3.529K)0.5]/2

    z = d[ 1 + (1 - 3.529K)0.5]/2

    Rearranging

    z = d[ 0.5 + (0.25 K / 1.134)0.5]

    This compares to BS 8110

    z = d[ 0.5 + (0.25 K / 0.9)0.5]

    The lever arm for an applied moment is now known

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    Higher Concrete Strengthsfck 50MPa )]/23,529K(1d[1z

    )]/23,715K(1d[1z fck = 60MPa

    fck = 70MPa

    fck = 80MPa

    fck = 90MPa

    )]/23,922K(1d[1z

    )]/24,152K(1d[1z

    )]/24,412K(1d[1z

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    Take moments about the centre of the compression force

    M = 0.87Asfyk z

    Rearranging

    As = M /(0.87fyk z)

    The required area of reinforcement can now be:

    calculated using these expressions

    obtained from Tables (eg Table 5 of How t o beams and ConciseTable 15.5 )

    obtained from graphs (eg from the Green Book )

    However, it is often considered good practice to limit the depth of the

    neutral axis to avoid over-reinforcement (ie to ensure a ductile failure).

    This is not an EC2 requirement and is not accepted by all engineers. A

    limiting value for Kcan be calculated (denoted K) as follows.

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    Design aids for flexureConcise: Table 15.5

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    k1 + k2xu/d

    where

    k1 = 0.4

    k2 = 0.6 + 0.0014/ cu2 = 0.6 + 0.0014/0.0035 = 1

    xu = depth to NA after redistribution

    = Redistribution ratio xu = d (- 0.4)

    Substituting forx in eqn 1 above and rearranging:

    M = b d2fck (0.6 0.18 2 - 0.21)

    K = M /(b d2fck) = (0.6 0.18 2 - 0.21)

    From BS 8110 K = (0.55 0.182 0.19) rearranged

    Some engineers advocate takingx/d< 0.45, and K < 0.168

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    Beams with Compression

    Reinforcement

    There is now an extra force Fsc

    = 0.87As2

    fyk

    The area of tension reinforcement can now be

    considered in two parts, the first part to balance the

    compressive force in the concrete, the second part is to

    balance the force in the compression steel. The area of

    reinforcement required is therefore:

    As

    = Kfck

    b d 2 /(0.87fyk

    z) +As2

    where z is calculated using K instead of K

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    As2 can be calculated by taking moments about the centre of the tensionforce:

    M = Kfck b d2 + 0.87fykAs2 (d - d2)

    Rearranging

    As2 = (K- K)fck b d2 / (0.87fyk (d - d2))

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    Calculate lever arm zfrom:

    * A limit of 0.95dis considered good practice, it is not a requirement of Eurocode 2.

    *95.053.3112

    dKd

    z

    Check minimum reinforcement requirements:

    dbf

    dbfA t

    yk

    tctmmin,s 0013.0

    26.0

    Check max reinforcement provided As,max 0.04Ac (Cl. 9.2.1.1)Check min spacing between bars > bar > 20 > Agg + 5

    Check max spacing between bars

    Calculate tension steel required from: zf

    MA

    yd

    s

    Flow Chart for Singly-reinforced

    Beam

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    Flow Chart for Doubly-

    Reinforced Beam

    Calculate lever arm zfrom: '53.3112

    Kd

    z Calculate excess moment from: '' 2 KKfbdM

    ck

    Calculate compression steel required from:

    2yd2s'

    ddfA

    Calculate tension steel required from:

    Check max reinforcement provided As,max 0.04Ac (Cl. 9.2.1.1)Check min spacing between bars >

    bar> 20 > A

    gg+ 5

    2syd

    2

    s' A

    zfbdfKA ck

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    Flexure Worked Example

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    Worked Example 1Design the section below to resist a sagging moment of 370 kNm assuming

    15% moment redistribution (i.e. = 0.85).

    Takefck

    = 30 MPa andfyk

    = 500 MPa.

    d

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    Initially assume 32 mm for tension reinforcement with 25 mm nominal cover

    to the link (allow 10 mm for link) and 20mm for compression reinforcement

    with 25 mm nominal cover to link.Nominal side cover is 35 mm.

    d = h cnom -link - 0.5

    = 500 25 - 10 16= 449 mm

    d2 = cnom +link + 0.5

    = 25 + 10 + 10

    = 45 mm

    449

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    provide compression steel

    mm368

    168.053.3112

    449

    '53.3112

    Kd

    z

    '204.0

    30449300

    103702

    6

    ck2

    K

    fbd

    MK

    168.0'K K1.00 0.208

    0.95 0.195

    0.90 0.182

    0.85 0.168

    0.80 0.153

    0.75 0.137

    0.70 0.120

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    kNm

    KKfbdMck

    3.65

    10)168.0204.0(30449300

    ''

    62

    2

    2

    6

    2yd

    2s

    mm372

    45)(449435

    10x65.3

    '

    ddf

    MA

    2

    6

    2s

    yd

    s

    mm2293

    372364435

    10)3.65370(

    '

    Azf

    MMA

    368

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    Provide 2 H20 for compression steel = 628mm2 (372 mm2 reqd)

    and 3 H32 tension steel = 2412mm2 (2296 mm2 reqd)

    By inspection does not exceed maximum area or maximum spacing ofreinforcement rules

    Check minimum spacing, assuming H10 links

    Space between bars = (300 35 x 2 - 10 x 2 - 32 x 3)/2

    = 57 mm > 32 mm OK

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    Factors for NA depth (=nd) and lever arm (=zd) for concrete grade 50 MPa

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    M/bd2fck

    Factor

    n 0.02 0.04 0.07 0.09 0.12 0.14 0.17 0.19 0.22 0.24 0.27 0.30 0.33 0.36 0.39 0.43 0.46

    z 0.99 0.98 0.97 0.96 0.95 0.94 0.93 0.92 0.91 0.90 0.89 0.88 0.87 0.86 0.84 0.83 0.82

    0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.10 0.11 0.12 0.13 0.14 0.15 0.16 0.17

    lever arm

    NA depth

    Simplified Factors for Flexure

    (1)

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    Factors for NA depth (=nd) and lever arm (=zd) for concrete grade 70 MPa

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    M/bd2fck

    Facto

    r

    n 0.03 0.05 0.08 0.11 0.14 0.17 0.20 0.23 0.26 0.29 0.33

    z 0.99 0.98 0.97 0.96 0.95 0.94 0.93 0.91 0.90 0.89 0.88

    0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.10 0.11 0.12 0.13 0.14 0.15 0.16 0.17

    lever arm

    NA depth

    Simplified Factors for Flexure

    (2)

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    Shear in Beams

    Shear design is different from BS8110

    Shear strength should be limited to the value for

    C50/60

    The shear effects in links and longitudinal steel have to

    be considered explicitly

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    Definitions Resistance of member without shear reinforcement

    VRd,c

    Resistance of member governed by the yielding ofshear reinforcement - VRd,s

    Resistance of member governed by the crushing ofcompression struts - VRd,max

    Applied shear force - VEd

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    Members Requiring Shear

    Reinforcement (6.2.3.(1))

    s

    d

    V(cot - cot

    V

    N M z

    zVz = 0.9d

    Fcd

    Ftd

    compression chord compression chord

    tension chordshear reinforcement

    angle between shear reinforcement and the beam axis

    angle between the concrete compression strut and the beam axis

    z inner lever arm. In the shear analysis of reinforced concrete

    without axial force, the approximate value z= 0,9dmay normallybe used.

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    cotswsRd, ywdfzs

    AV

    tancot

    1maxRd,

    cdwcw fzbV

    21.8 < < 45

    Strut Inclination Method

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    Shear Design: LinksVariable strut methodallows a shallower strut angle

    hence activating more links.

    As strut angle reduces concrete stress increases

    Angle = 45 V carried on 3 links Angle = 21.8 V carried on 6 links

    d

    V

    z

    x

    d

    x

    V

    z

    s

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    shear reinforcement control

    VRd,s =Asw z fywd cot/s Exp (6.8)

    concrete strut controlVRd,max = z bw1fcd /(cot + tan) = 0,5zbw fcd sin2

    Exp (6.9)

    where = 0,6(1-fck/250) Exp (6.6N)

    1 cot 2,5

    Basic equations

    d

    V

    z

    x

    d

    x

    V

    z

    s

    Shear Resistance of Sections with

    Shear Reinforcement

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    fck vRd, cot = 2.5 vRd, cot = 1.0

    20 2.54 3.6825 3.10 4.5

    28 3.43 4.97

    30 3.64 5.28

    32 3.84 5.58

    35 4.15 6.02

    40 4.63 6.72

    45 5.08 7.38

    50 5.51 8.00

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    Shear - Variable strut method Concise Fig 15.1 a)

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    Shear - Variable strut method Concise Fig 15.1 b)

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    Where av 2dthe applied shear force, VEd, for a point load(eg, corbel, pile cap etc) may be reduced by a factor av/2d

    where 0.5 av 2d provided:

    dd

    av av

    The longitudinal reinforcement is fully anchored at the support. Only that shear reinforcement provided within the central 0.75av is

    included in the resistance.

    Short Shear Spans with Direct

    Strut Action (6.2.3)

    Note: see PD6687-1:2010 Cl 2.14 for more information

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    Shift Rule For members without shear reinforcement this is satisfied with al = d

    a lFtd

    a l

    Envelope of (MEd /z+NEd)

    Acting tensile force

    Resisting tensile force

    lbd

    lbd

    lbd

    lbd

    lbd lbd

    lbd

    lbdFtd

    For members with shear reinforcement: Conservatively al = 1.125d

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    Shear Example

    Design of shear reinforcement using

    Eurocode 2

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    Design Flow Chart for Shear

    Yes (cot = 2.5)

    Determine the concrete strut capacity vRd when cot = 2.5vRd = 0.138fck(1-fck/250)

    Calculate area of shear reinforcement:

    Asw/s = vEdbw/(fywd cot )

    DeterminevEd where:

    vEd = design shear stress [vEd = VEd/(bwz) = VEd/(bw 0.9d)]

    Determine from: = 0.5 sin-1[(vEd/(0.20fck(1-fck/250))]Is vRd >vEd?No

    Check maximum spacing of shear reinforcement :

    s,max = 0.75 dFor vertical shear reinforcement

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    Calculate

    0.35

    250/30-130x20.0

    96.4sin5.0

    )250/1(20.0sin5.0

    1

    ckck

    Ed1

    ff

    v

    43.1cot Asw/ s = vEdbw/ (fywdcot )Asw/ s = 4.96 x 140 / (435 x 1.43)

    Asw/ s = 1.12 mm

    Tr y H10 l i nks wi t h 2 legs.

    Asw = 157 mm2

    s < 157 / 1. 12 = 140 mm

    pr ovid e H10 l i nks at 125 mm spacing

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    Beam Example 1

    Cover = 40mm to each face

    fck = 30

    Determine the flexural and shearreinforcement required

    (try 10mm links and 32mm main steel)

    Gk = 75 kN/m, Qk = 50 kN/m , assume no redistribution and useequation 6.10 to calculate ULS loads.

    8 m

    450

    1000

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    Beam Example 1 BendingULS load per m = (75 x 1.35 + 50 x 1.5) = 176.25

    Mult = 176.25 x 82/8

    = 1410 kNmd = 1000 - 40 - 10 32/2

    = 934

    120.030934450

    1014102

    6

    ck

    2 fbdMKK = 0.208

    K < KNo compression reinforcement required dKdz 95.0822120.0x53.311

    293453.311

    2

    2

    6

    yd

    smm3943

    822x435

    10x1410 zf

    MA

    Provide 5 H32 (4021 mm2)

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    Workshop Problem

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    Workshop Problem

    Cover = 35 mm to each face

    fck = 30MPa

    Check the beam in flexure and shear

    Gk = 10 kN/m, Qk = 6.5 kN/m (Use eq. 6.10)

    8 m

    300

    450

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    Solution - FlexureULS load per m = (10 x 1.35 + 6.5 x 1.5) = 23.25Mult = 23.25 x 8

    2/8

    = 186 kNm

    d = 450 - 35 - 10 32/2

    = 389

    137.030389300

    101862

    6

    ck

    2 fbdMK

    K = 0.208

    K < KNo compression reinforcement required dKdz 95.0334137.0x53.311

    2

    38953.311

    2

    2

    6

    yds mm1280

    334x435

    10x186 zf

    MA

    Provide 3 H25 (1470 mm2)

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    Solution - ShearShear force, VEd = 23.25 x 8 /2 = 93 kN

    Shear stress:

    vEd

    = VEd

    /(bw

    0.9d) = 93 x 103/(300 x 0.9 x 389)

    = 0.89 MPa

    vRd = 3.64 MPa

    vRd > vEd

    cot = 2.5Asw/s = vEd bw/(fywd cot )

    Asw/s = 0.89 x 300 /(435 x 2.5)

    Asw/s = 0.24 mm

    Try H8 links with 2 legs.

    Asw = 101 mm2

    s < 101 /0.24 = 420 mm

    Maximum spacing = 0.75 d= 0.75 x 389 = 292 mm

    provide H8 links at 275 mm spacing

    fck

    vRd (whencot = 2.5)

    20 2.54

    25 3.1028 3.43

    30 3.64

    32 3.84

    35 4.15

    40 4.63

    45 5.08

    50 5.51

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    Detailing

    www ukcares co uk

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    UK CARES (Certification - Product & Companies)

    1. Reinforcing bar and coil2. Reinforcing fabric

    3. Steel wire for direct use of for further

    processing

    4. Cut and bent reinforcement

    5. Welding and prefabrication of reinforcingsteel

    www.ukcares.co.uk

    www.uk-bar.org

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    Reinforced Concrete Detailing

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    Reinforced Concrete Detailing

    to Eurocode 2

    Section 8 - General RulesAnchorage

    LapsLarge Bars

    Section 9 - Particular RulesBeams

    SlabsColumns

    Walls

    Foundations

    Discontinuity Regions

    Tying Systems

    Cover Fire

    Specification and Workmanship

    Section 8 - General Rules

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    Clear horizontal and vertical distance , (dg +5mm) or 20mm

    For separate horizontal layers the bars in each layer should be

    located vertically above each other. There should be room to allow

    access for vibrators and good compaction of concrete.

    Section 8 General Rules

    Spacing of barsEC2: Cl. 8.2 Concise: 11.2

    Min Mandrel Dia for bent bars

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    To avoid damage to bar is

    Bar dia 16mm Mandrel size 4 x bar diameterBar dia > 16mm Mandrel size 7 x bar diameterThe bar should extend at least 5 diameters beyond a bend

    Minimum mandrel size, mMin. Mandrel Dia. for bent bars

    EC2: Cl. 8.3 Concise: 11.3

    Min. Mandrel Dia. for bent bars

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    Minimum mandrel size, m

    To avoid failure of the concrete inside the bend of the bar: m,min Fbt ((1/ab) +1/(2 )) /fcdFbt ultimate force in a bar at the start of a bend

    ab for a given bar is half the centre-to-centre distance between bars.

    For a bar adjacent to the face of the member, ab should be taken as

    the cover plus /2Mandrel size need not be checked to avoid concrete failure if :

    anchorage does not require more than 5 past end of bend bar is not the closest to edge face and there is a cross bar inside bend mandrel size is at least equal to the recommended minimum value

    Min. Mandrel Dia. for bent bars

    EC2: Cl. 8.3 Concise: 11.3

    Bearing stressinside bends

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    Anchorage of reinforcementEC2: Cl. 8.4

    Ultimate bond stress

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    The design value of the ultimate bond stress,fbd = 2.25 12fctdwherefctd should be limited to C60/75

    1 =1 for good and 0.7 for poor bond conditions

    2 = 1 for 32, otherwise (132-)/100

    a) 45 90 c) h> 250 mm

    h

    Direction of concreting

    300

    h

    Direction of concreting

    b) h 250 mm d) h > 600 mmunhatched zone good bond conditions

    hatched zone - poor bond conditions

    Direction of concreting

    250

    Direction of concreting

    EC2: Cl. 8.4.2 Concise: 11.5

    300

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    Design Anchorage Length, lbd

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    lbd = 1 2 3 4 5 lb,rqdlb,minHowever: (2 3 5) 0.7lb,min > max(0.3lb,rqd ; 10, 100mm)

    g g g , bd

    EC2: Cl. 8.4.4 Concise: 11.4.2

    Alpha valuesEC2: Table 8.2

    Table requires values for:

    Cd Value depends on cover and bar spacing, see Figure 8.3

    K Factor depends on position of confinement reinforcement,

    see Figure 8.4

    = (Ast

    Ast,min

    )/ As

    Where Ast

    is area of transverse reinf.

    Table 8.2 - Cd & K factors

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    d

    Concise: Figure 11.3EC2: Figure 8.3

    EC2: Figure 8.4

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    Alpha values

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    EC2: Table 8.2 Concise: 11.4.2

    Anchorage of links

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    g

    Concise: Fig 11.2EC2: Cl. 8.5

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    LapsEC2: Cl. 8.7

    Design Lap Length, l0 (8.7.3)

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    l0 = 1 2 3 5 6 lb,rqdl0,min

    6 = (1/25)0,5 but between 1.0 and 1.5

    where1 is the % of reinforcement lapped within 0.65l0 from the

    centre of the lap

    Percentage of lapped bars

    relative to the total cross-

    section area

    < 25% 33% 50% >50%

    6 1 1.15 1.4 1.5Note: Intermediate values may be determined by interpolation.

    1 2 3 5 are as defined for anchorage length

    l0,min max{0.3 6 lb,rqd; 15; 200}

    EC2: Cl. 8.7.3 Concise: 11.6.2

    Arrangement of Laps

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    EC2: Cl. 8.7.3, Fig 8.8

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    Worked example

    Anchorage and lap lengths

    Anchorage Worked Example

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    Anchorage Worked Example

    Calculate the tension anchorage for an H16 bar in the

    bottom of a slab:

    a) Straight bars

    b) Other shape bars (Fig 8.1 b, c and d)

    Concrete strength class is C25/30

    Nominal cover is 25mm

    Assume maximum design stress in the bar

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    Basic anchorage length, lb,req

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    lb.req = (/4) ( sd/fbd) EC2 Equ 8.3

    Max stress in the bar, sd = fyk/s = 500/1.15

    = 435MPa.

    lb.req = (/4) ( 435/2.693)

    = 40.36

    For concrete class C25/30

    Design anchorage length, lbd

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    g g g , bd

    lbd = 1 2 3 4 5 lb.req lb,min

    lbd = 1 2 3 4 5 (40.36) For concrete class C25/30

    Alpha values

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    EC2: Table 8.2 Concise: 11.4.2

    Table 8.2 - Cd & K factors

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    Concise: Figure 11.3EC2: Figure 8.3

    EC2: Figure 8.4

    Design anchorage length, lbd

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    lbd = 1 2 3 4 5 lb.req lb,min

    lbd = 1 2 3 4 5 (40.36) For concrete class C25/30

    a) Tension anchorage straight bar

    1 = 1.0

    3 = 1.0 conservative value with K= 0

    4 = 1.0 N/A

    5 = 1.0 conservative value

    2 = 1.0 0.15 (Cd )/

    2 = 1.0 0.15 (25 16)/16 = 0.916

    lbd = 0.916 x 40.36 = 36.97 = 592mm

    Design anchorage length, lbd

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    lbd = 1 2 3 4 5 lb.req lb,min

    lbd = 1 2 3 4 5 (40.36) For concrete class C25/30

    b) Tension anchorage Other shape bars1 = 1.0 Cd = 25 is 3 = 3 x 16 = 48

    3 = 1.0 conservative value with K= 0

    4 = 1.0 N/A

    5 = 1.0 conservative value

    2

    = 1.0 0.15 (Cd

    3)/ 1.0

    2 = 1.0 0.15 (25 48)/16 = 1.25 1.0

    lbd = 1.0 x 40.36 = 40.36 = 646mm

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    Anchorage /lap lengths for slabs

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    Table 5.25: Typical values of anchorage and lap lengths for slabs

    Bond Length in bar diameters

    conditions fck /fcu

    25/30

    fck /fcu

    28/35

    fck /fcu

    30/37

    fck /fcu

    32/40

    Full tension and

    compression anchorage

    length, lbd

    good 40 37 36 34

    poor 58 53 51 49

    Full tension andcompression lap length, l0

    good 46 43 42 39poor 66 61 59 56

    Note: The following is assumed:

    - bar size is not greater than 32mm. If >32 then the anchorage and lap lengths should be

    increased by a factor (132 - bar size)/100

    - normal cover exists- no confinement by transverse pressure

    - no confinement by transverse reinforcement

    - not more than 33% of the bars are lapped at one place

    Lap lengths provided (for nominal bars, etc.) should not be less than 15 times the bar size

    or 200mm, whichever is greater.

    Manual for the design of concrete structures to Eurocode 2

    Arrangement of LapsEC2: Cl. 8.7.2 Concise: Cl 11.6

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    Laps between bars should normally be staggered and not located in regions

    of high stress, the arrangement of lapped bars should comply with the

    following (see Figure 8.7 on next slide):

    The clear distance between lapped bars should not be greater than4 or 50 mm otherwise the lap length should be increased by a length

    equal to the clear space where it exceeds 4 or 50 mm

    The longitudinal distance between two adjacent (staggered?) laps

    should not be less than 0,3 times the lap length, l0; In case of adjacent laps, the clear distance between adjacent bars

    should not be less than 2 or 20 mm.

    When the provisions comply with the above, the permissible percentage of

    lapped bars in tension may be 100% where the bars are all in one layer.Where the bars are in several layers the percentage should be reduced to

    50%.

    All bars in compression and secondary (distribution) reinforcement may be

    lapped in one section.

    Arrangement of LapsEC2: Cl. 8.7.2, Fig 8.7 Concise: Cl 11.6.2

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    g

    Transverse Reinforcement at LapsBars in tension Concise: Cl 11.6.4

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    Where the diameter, , of the lapped bars 20 mm, the transversereinforcement should have a total area, Ast 1,0As of one spliced bar. Itshould be placed perpendicular to the direction of the lapped

    reinforcement and between that and the surface of the concrete.

    If more than 50% of the reinforcement is lapped at one point and the

    distance between adjacent laps at a section is 10 transverse bars shouldbe formed by links or U bars anchored into the body of the section.

    The transverse reinforcement provided as above should be positioned at

    the outer sections of the lap as shown below.

    l /30A /2

    st

    A /2st

    l /30FsFs

    150 mm

    l0

    EC2: Cl. 8.7.4, Fig 8.9 Rules apply if bar diameter 20mm

    Figure 8.9 bars in tension

    Transverse Reinforcement at LapsBars in compression

    EC2 Cl 8 7 4 Fi 8 9

    Concise: Cl 11.6.4

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    EC2: Cl. 8.7.4, Fig 8.9

    In addition to the rules for bars in tension one bar of the transverse

    reinforcement should be placed outside each end of the lap length.

    Figure 8.9 bars in compression

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    SECTION 9

    Detailing of members and particular rules

    Beams (9.2)

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    As,min = 0,26 (fctm/fyk)btd but 0,0013btd

    As,max = 0,04Ac

    Section at supports should be designed for a

    hogging moment 0,25 max. span moment

    Any design compression reinforcement () should be

    held by transverse reinforcement with spacing 15

    Beams (9.2)

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    Tension reinforcement in a flanged beam at

    supports should be spread over the effective width

    (see 5.3.2.1)

    Curtailment (9.2.1.3)

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    (1) Sufficient reinforcement should be provided at all sections to resist the

    envelope of the acting tensile force, including the effect of inclined cracks

    in webs and flanges.

    (2) For members with shear reinforcement the additional tensile force, Ftd,

    should be calculated according to 6.2.3 (7). For members without shear

    reinforcement Ftdmay be estimated by shifting the moment curve a

    distance al = d according to 6.2.2 (5). This "shift rule may also be used

    as an alternative for members with shear reinforcement, where:

    al = z (cot - cot )/2 = 0.5 z cot for vertical shear links

    z= lever arm, = angle of compression strut

    al = 1.125 d when cot = 2.5 and 0.45 d when cot = 1

    Curtailment of reinforcementEC2: Cl. 9.2.1.3, Fig 9.2 Concise: 12.2.2

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    For members without shear reinforcement this is satisfied with al = d

    a lFtd

    a l

    Envelope of (MEd /z+NEd)

    Acting tensile force

    Resisting tensile force

    lbd

    lbd

    lbd

    lbd

    lbd lbd

    lbd

    lbd Ftd

    Shift rule

    For members with shear reinforcement: al = 0.5 zCot But it is always conservative to use al = 1.125d

    Anchorage of BottomReinforcement at End Supports

    (9 2 1 4)

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    lbd is required from the line of contact of the support.

    Simple support (indirect) Simple support (direct)

    As bottom steel at support 0.25As provided in the span

    Transverse pressure may only be taken into account with

    a direct support.

    Shear shift rule

    al

    Tensile Force Envelope

    (9.2.1.4)

    Simplified Detailing Rules for

    BeamsConcise: Cl 12 2 4

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    Beams

    How to.EC2

    Detailing section

    Concise: Cl 12.2.4

    Supporting Reinforcement atIndirect Supports

    EC2: Cl 9 2 5

    Concise: Cl 12.2.8

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    h /31

    h /21

    B

    A

    h /32 h /22

    supporting beam with height h1

    supported beam with height h2 (h1 h2)

    The supporting reinforcement is in

    addition to that required for other

    reasons

    A

    B

    The supporting links may be placed in a zone beyond

    the intersection of beams

    Plan view

    EC2: Cl. 9.2.5

    C t il t b t f th Shift l d

    Solid slabsEC2: Cl. 9.3

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    Curtailment as beams except for the Shift rule al = d

    may be used

    Flexural Reinforcement min and max areas as beam

    Secondary transverse steel not less than 20% main

    reinforcement

    Reinforcement at Free Edges

    Detailing Comparisons

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    d or 150 mm from main bar9.2.2 (8): 0.75 d 600 mm

    9.2.1.2 (3) or 15 from main bar

    st,max

    0.75d9.2.2 (6): 0.75 dsl,max

    0.4 b s/0.87 fyv9.2.2 (5): (0.08 b s fck)/fykAsw,min

    Links

    Table 3.28Table 7.3NSmax

    dg + 5 mm or 8.2 (2): dg + 5 mm or or 20mmsmin

    Spacing of Main Bar s

    0.04 bh9.2.1.1 (3): 0.04 bdAs,max

    0.002 bh--As,min

    Main Bar s i n Compr essi on

    0.04 bh9.2.1.1 (3): 0.04 bdAs,max

    0.0013 bh9.2.1.1 (1): 0.26fctm/fykbd 0.0013 bd

    As,min

    ValuesClause / Val uesMain Bar s i n Tensi on

    BS 8110EC2Beams

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    Detailing Comparisons

    BS 8110EC2P hi Sh

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    Columns

    150 mm from main bar9.5.3 (6): 150 mm from main bar

    129.5.3 (3): min (12min; 0.6 b;240 mm)Scl,tmax

    0.25 or 6 mm9.5.3 (1) 0.25 or 6 mmMin size

    Links

    0.06 bh9.5.2 (3): 0.04 bhAs,max

    0.004 bh9.5.2 (2): 0.10NEd/fyk 0.002bhAs,min

    Main Bar s i n Comp r ession

    1.5d9.4.3 (1):

    within 1st control perim.: 1.5d

    outside 1st control perim.: 2d

    St

    0.75d9.4.3 (1): 0.75dSr

    Spacing of Li nks

    Total = 0.4ud/0.87fyv9.4.3 (2): Link leg = 0.053 sr st(fck)/fyk

    Asw,min

    ValuesClause / Val uesLinks

    BS 8110EC2Punching Shear