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    Practical Design to Eurocode 2

    Week 4 - Slabs

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    Outline Week 4

    We will look at the following topics:

    Designing for shear including punching shear

    Serviceability cracking and deflection

    Detailing Solid slabs

    Workshop serviceability cracking & deflection

    Flat Slab Design includes flexure workshop

    Tying systems

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    Designing for Shear

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    Shear

    There are three approaches to designing for shear:

    When shear reinforcement is not required e.g. slabs

    When shear reinforcement is required e.g. Beams

    Punching shear requirements e.g. flat slabs

    The maximum shear strength in the UK should not exceed thatof class C50/60 concrete

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    Shear resistance without shearreinforcement

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    where:

    k = 1 + (200/d) 2.0l = Asl/bwdAsl = area of the tensile reinforcement,

    bw = smallest width of the cross-section in the tensile area [mm]

    cp = NEd/Ac < 0.2 fcd [MPa] Compression +veNEd = axial force in the cross-section due to loading or pre-stressing [in N]

    Ac = area of concrete cross section [mm2]

    VRd,c = [0.12k(100 lfck)1/3 + 0.15cp] bwd (6.2.a)

    with a minimum ofVRd,c = (0.035k

    3/2fck1/2 + 0.15 cp) bwd (6.2.b)

    Without Shear ReinforcementCl. 6.2.2 7.2

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    Shear- Table 7.1

    vRd,c resistance of members without shear reinforcement, MPa

    As(bd) %

    Effective depth, d(mm)

    200 225 250 275 300 350 400 450 500 600 7500.25 0.54 0.52 0.50 0.48 0.47 0.45 0.43 0.41 0.40 0.38 0.36

    0.50 0.59 0.57 0.56 0.55 0.54 0.52 0.51 0.49 0.48 0.47 0.45

    0.75 0.68 0.66 0.64 0.63 0.62 0.59 0.58 0.56 0.55 0.53 0.51

    1.00 0.75 0.72 0.71 0.69 0.68 0.65 0.64 0.62 0.61 0.59 0.57

    1.25 0.80 0.78 0.76 0.74 0.73 0.71 0.69 0.67 0.66 0.63 0.61

    1.50 0.85 0.83 0.81 0.79 0.78 0.75 0.73 0.71 0.70 0.67 0.65

    1.75 0.90 0.87 0.85 0.83 0.82 0.79 0.77 0.75 0.73 0.71 0.68

    2.00 0.94 0.91 0.89 0.87 0.85 0.82 0.80 0.78 0.77 0.74 0.71

    k 2.00 1.94 1.89 1.85 1.82 1.76 1.71 1.67 1.63 1.58 1.52

    Table derived from: vRd,c = 0.12 k (100Ifck)(1/3) 0.035 k1.5fck0.5 where k = 1 + (200/d) 2 and I =As/(bd) 0.02

    Note: This table has been prepared forfck = 30. Where I exceeds 0.40% the following factors may be used:

    fck 25 28 32 35 40 45 50

    factor 0.94 0.98 1.02 1.05 1.10 1.14 1.19

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    Shear in Slabs

    Most slabs do not require shear

    reinforcement

    Check VEd < VRd,c

    Where VRd,c is shear resistance of

    members without reinforcement

    vRd,c = 0.12 k (100 Ifck)1/3

    0.035 k1.5fck0.5

    Where VEd > VRd,c,

    shear reinforcement is required

    and the strut inclination method

    should be used

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    Shear resistance with shearreinforcement

    See Week 2 Beams

    Variable strut inclination method

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    EC2: Cl 6.2.3

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    cotswsRd, ywdfzs

    AV

    tancot

    1maxRd,

    cdwcw fzbV

    21.8 < < 45

    Variable Strut Inclination MethodCl. 6.2.3

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    fck

    vRd,cot =2.5

    vRdcot =1.0

    20 2.54 3.68

    25 3.10 4.50

    28 3.43 4.97

    30 3.64 5.28

    32 3.84 5.58

    35 4.15 6.0240 4.63 6.72

    45 5.08 7.38

    50 5.51 8.00

    Variable strut inclination method

    Cl. 6.2.3

    vRd,max

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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 = vEd bw/(fywd cot )

    Determine vEd 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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    Punching shear

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    Punching shear does not use the Variable Strut inclination method

    and is similar to BS 8110 methods

    The basic control perimeter is set at 2dfrom the loaded area

    The shape of control perimeters have rounded corners

    bz

    by

    2d 2d 2d

    2du1

    u1 u1

    Punching ShearCl. 6.4 Figure 8.3

    Where shear reinforcement is required the shear resistance is the

    sum of the concrete and shear reinforcement resistances.

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    For structures where:

    lateral stability does notdepend on frame action

    adjacent spans do not differ

    by more than 25%

    the approximate values for

    shown may be used:

    The applied shear stress should be taken as:

    vEd = VEd/ui d where =1 + k(MEd/VEd)u1/W1

    Punching Shear (2)

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    For a rectangular internal columnwith biaxial bending the following

    simplification may be used:

    = 1 + 1.8{(ey/bz)2 + (ez/by)

    2}0.5

    where by and bz are the dimensions

    of the control perimeter

    For other situations there is plenty of guidance on determining given in Cl 6.4.3 of the Code.

    Where the simplified arrangement is not applicable then can be

    calculated

    c1

    c2

    2d

    2d

    y

    z

    Punching Shear (3)

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    kd

    Outer control

    perimeter

    Outer perimeter of shear

    reinforcement

    1.5d(2dif > 2dfrom

    column)

    0.75d

    0.5dA A

    Section A - A

    0.75d

    0.5d

    Outer control

    perimeter

    kd

    The outer control perimeter at

    which shear reinforcement is not

    required, should be calculatedfrom:

    uout,ef = VEd / (vRd,c d)

    The outermost perimeter ofshear reinforcement should be

    placed at a distance not

    greater than kd( k = 1.5)

    within the outer control

    perimeter.

    Punching Shear Reinforcement (1)Cl. 6.4.5 Figures 12.5 & 12.6

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    1,5d

    2d

    d

    d

    > 2d

    1,5d

    uout

    uout,ef

    Where proprietary systems are used the control perimeter at which

    shear reinforcement is not required, uout or uout,ef(see Figure) should be

    calculated from the following expression:

    uout,ef = VEd / (vRd,c d)

    Punching Shear Reinforcement (2)Cl. 6.4.5 Figure 8.10

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    EC 2: Concise:

    NA - Check vEd 2 vRdc at basic control perimeter

    The minimum area of a link leg:

    Asw,min (1.5 sin+ cos)/(sr st) (0.08 (fck))/fyk equ 9.11

    Where shear reinforcement is required it should be calculated in

    accordance with the following expression:

    vRd,cs = 0.75 vRd,c + 1.5 (d/sr)Aswfywd,ef(1/(u1d)) sinAsw = area of shear reinforcement in each perimeter around the col.

    sr = radial spacing of layers of shear reinforcement

    = angle between the shear reinforcement and the plane of slab

    fywd,ef = effective design strength of the punching shear reinforcement,= 250 + 0.25 dfywd (MPa.)

    d = mean effective depth of the slabs (mm)

    V

    v vu dEd

    Ed Rd,max0

    = 0.5 f

    cdMax. shear stress at column face,

    Punching Shear Reinforcement (3)Cl. 6.4.5 8.5

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    Check vEd 2 vRdc at basic control perimeter

    Note: UK NA says first control perimeter, but the paper* on which

    this guidance is based says basic control perimeter

    The minimum area of a link leg (or equivalent),Asw,min, is given by the

    following expression:

    Asw,min (1.5 sin+ cos)/(sr st) (0,08 (fck))/fyk equ 9.11

    Asw,min (0,053 sr st (fck)) /fyk

    Punching Shear Reinforcement (4)

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    Punching shearWorked example

    From Worked Examples to EC2: Volume 1 Example 3.4.10

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    Punching shear

    At C2 the ultimate column

    reaction is 1204.8 kN

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    Solution1. Check shear at the perimeter of the column

    vEd = VEd/(u0d) < vRd,max

    = 1.15

    u0 = 4 x 400 = 1600 mm

    d = (260 + 240)/2 = 250 mm

    vEd = 1.15 x 1204.8 x 1000/(1600 x 250)

    = 3.46 MPa

    vRd,max = 0.5 fcd

    = 0.5 x 0.6(1-fck/250) x ccfck/m

    = 0.5 x 0.6(1-30/250) x 1.0 x 30 /1.5 = 5.28 MPavEd < vRd,max ...OK

    = 1,4

    = 1,5

    = 1,15

    C

    B A

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    Solution2. Check shear at the basic control perimeter

    vEd = VEd/(u1d) < vRd,c

    u1= 2(c

    x+ c

    y) + 2x 2d

    = 2(400 + 400) + 2x 2 x 250 = 4742 mm

    vEd = 1.15 x 1204.8 x 1000/(4742 x 250) =

    = 1.17 MPa

    vRd,c = 0.12 k(100lfck)1/3

    k = 1 + (200/d)1/2

    = 1 + (200/250)1/2 = 1.89

    l = (lylz)1/2 = (0.0085 x 0.0048) 1/2 = 0.0064

    vRd,c = 0.12 x 1.89(100 x 0.0064 x 30)1/3 = 0.61 MPa

    vEd > vRd,c ...Punching shear reinforcement required

    NA check vEd 2vRd,c at basic control perimeter

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    Solution3. Perimeter at which punching shear no longer required

    uout = VEd/(dvRd,c)

    = 1.15 x 1204.8 x 1000/(250 x 0.61)= 9085 mm

    Rearrange: uout = 2(cx + cy) + 2rout

    rout = (uout - 2(cx + cy))/(2)

    = (9085 1600)/(2) = 1191 mm

    Position of outer perimeter of reinforcement from column face:

    r = 1191 1.5 x 250 = 816 mm

    Maximum radial spacing of reinforcement:

    sr,max = 0.75 x 250 = 187 mm, say 175 mm

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    Solution4. Area of reinforcement

    Asw (vEd 0.75vRd,c)sru1/(1.5fywd,ef)

    fywd,ef = (250 + 0.25d) = 312 MPa

    Asw (1.17 0.75 x 0.61) x 175 x 4741/(1.5 x 312)

    1263 mm2/perim.

    Minimum area of a link leg:

    Asw,min (0.053 sr st (fck)) /fyk = 0.053 x 175 x 350 x 30 / 500

    36 mm2

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    Solution

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    Outline Week 4

    We will look at the following topics:

    Designing for shear

    Serviceability

    Detailing Solid slabs

    Workshop - serviceability

    Flat Slabs

    Tying systems

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    Serviceability

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    EC 2: Concise:

    What does Eurocode 2 Cover?Cl. 7.2 10.1

    Stress limitation (7.2)

    Stress checks in reinforced concrete members have not been

    required in the UK for the past 50 years or so and there has beenno known adverse effect. Provided that the design has been carried

    out properly for ultimate limit state there will be no significant

    effect at serviceability in respect of longitudinal cracking PD

    6687 Cl. 2.20

    Control of cracking (7.3)

    Control of deflections (7.4)

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    Crack control

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    Control of Cracking

    In Eurocode 2 cracking is controlled in the following ways:

    Minimum areas of reinforcement cl 7.3.2 & Equ 7.1

    As,mins = KcKfct,effAct this is the same as

    Crack width limits (Cl. 7.3.1 and National Annex). These limits

    can be met by either:

    direct calculation (Cl. 7.3.4) crack width is Wk

    deemed to satisfy rules (Cl. 7.3.3)

    Note: slabs 200mm depth are OK if As,min is provided.

    Equ 9.1N

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    Minimum Reinforcement AreaThe minimum area of reinforcement for slabs (and beams) is given by:

    dbf

    dbfA t

    yk

    tctmmin,s 013.0

    26.0

    EC2: Cl 9.2.1.1

    9.1N

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    Crack Width Limits - use Table NA.4

    Recommended values ofwmax

    Exposure class RC or unbonded PSC

    members

    Prestressed

    members with

    bonded tendons

    Quasi-permanent load Frequent load

    X0,XC1 0.3* 0.2XC2,XC3,XC4 0.3

    XD1,XD2,XS1,

    XS2,XS3

    Decompression

    * Does not affect durability, may be relaxed where appearance

    is not critical (eg use 0.4 mm)

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    Crack Control Without Direct

    CalculationCrack control may be achieved in two ways:

    limiting the maximum bar diameter using Table 7.2

    limiting the maximum bar spacing using Table 7.3

    Note: For cracking due to restraint use only max bar size

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    EC 2: Concise:

    Maximum Bar Diameters

    Cl. 7.3.3 Table 10.1

    0

    10

    20

    30

    40

    50

    100 150 200 250 300 350 400 450 500

    Reinforcement stress, s(N/mm2)

    maximumb

    ar

    diameter(mm

    )

    wk=0.3 mm

    wk=0.2 mm

    wk = 0.4

    (Stress due to quasi-permanent actions)

    Crack Control

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    EC 2: Concise:

    Maximum Bar Spacings

    Cl. 7.3.3 Table 10.2

    0

    50

    100

    150

    200

    250

    300

    150 200 250 300 350 400

    stress in reinforcement (MPa)

    Maximumb

    ar

    spacing(mm) wk = 0.4

    wk = 0.3

    wk = 0.2

    (Stress due to quasi-permanent actions)

    Crack Control

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    Deflection control

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    EC 2: Concise:

    Deflection Limits (7.4.1)

    Cl. 7.4.1 -

    Span/250 under quasi-permanent loads to avoid impairment ofappearance and general utility

    Span/500 after construction under the quasi-permanent loads toavoid damage to adjacent parts of the structure.

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    EC 2: Concise:

    Deflection Control

    Cl. 7.4 10.5

    Deflection control may be achieved by the followingmethods:

    Direct calculation (Eurocode 2 methods considered to

    be an improvement on BS 8110) See How

    toDeflection calculations

    Using simplified span-to-effective depth limits from

    the code (control of deflection without calculation)

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    Deflection calculations

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    Deflection: L/d check

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    EC 2: Concise:

    Limiting Span-effective-depth ratios

    Cl 7.4.2 & Exp (7.16a & b) 10.5.2

    K factor taking account of the different structural systems

    0 reference reinforcement ratio = fck 10-3

    required tension reinforcement ratio at mid-span to resist the momentdue to the design loads (at support for cantilevers)

    required compression reinforcement ratio at mid-span to resist themoment due to design loads (at support for cantilevers)

    23

    0ck

    0ck 12,35,111

    ffK

    d

    l if 0

    0

    ck0

    ck

    '

    12

    1

    '5,111

    ffK

    d

    lif> 0

    There are adjustments to these expressions in cl 7.4.2 (2) for the

    steel stress, flanged sections and long spans with brittle finishes.

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    EC 2: Concise:

    Basic span/effective Depth Ratios

    Table 7.4(N) use Table NA.5 Table 10.3

    Structural system K =1.5%

    =0.5%

    S.S. beam or slab 1.0 14 20

    End span 1.3 18 26

    Interior span 1.5 20 30

    Flat slab 1.2 17 24

    Cantilever 0.4 6 8

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    EC 2: Concise:

    Graph of Exp. (7.16)

    - Figure 15.2

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    EC2 Span/Effective Depth Ratios

    18.5

    Percentage of tension reinforcement (As,reqd/bd)

    Spantodepthratio(l/d)

    This graph has beenproduced for K = 1.0

    StructuralSystem

    K

    Simply

    supported

    1.0

    End span 1.3

    Interior Span 1.5

    Flat Slab 1.2

    How to guide Figure

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    Flow Chart

    Is basic l/dx F1 x F2 x F3 >Actual l/d?

    Yes

    No

    Factor F3 accounts for stress in the reinforcementF3 = As,prov / As,reqd 1.5 or 310/s 1.5 (UK NA)

    Check complete

    Determine basic l/d

    Factor F2 for spans supporting brittle partitions > 7mF2 = 7/leff

    Factor F1 for ribbed and waffle slabs only

    F1 = 1 0.1 ((bf/bw) 1) 0.8

    IncreaseAs,provor fck

    No

    F t t b li d

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    Factors to be applied

    EC2: cl 7.4.2 & NA Concise 10.5.2

    F1 - Flanged sections

    where the ratio of the flange breadth to the rib breadth exceeds3, the values of l/d given by Expression (7.16) should bemultiplied by 0.8.

    F2 Brittle partitions

    For slabs (other than flat slabs), with spans exceeding 7.0 m,which support partitions liable to be damaged by excessive

    deflections, the values of l/d given by Expression (7.16) should bemultiplied by 7.0/ leff(leff in metres, see 5.3.2.2 (1)).

    For flat slabs, with spans exceeding 8.5 m, which supportpartitions liable to be damaged by excessive deflections, thevalues of l/d given by Expression (7.16) should be multiplied by8.5 / leff(leffin metres, see 5.3.2.2 (1)).

    F3 s Steel stress under service loadMay be adjusted by 310/ s 1.5 or As,prov/As,req 1.5where s calculated using characteristic loads.

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    Outline Week 4

    We will look at the following topics:

    Designing for shear

    Serviceability

    Detailing Solid slabs

    Workshop - serviceability

    Flat Slabs

    Tying systems

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    Detailing - Solid slabs

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    Where partial fixity exists, not taken into account in design: Internal

    supports:As,top 0,25As for Mmax in adjacent spanEnd supports: As,top 0,15As for Mmax in adjacent span

    This top reinforcement should extend 0,2 adjacent span

    2h

    h

    Reinforcement at free edges should include u bars and longitudinal

    bars

    Detailing Solid slabsRules for one-way and two-way solid slabsEC2 9.3

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    Outline Week 4

    We will look at the following topics:

    Designing for shear

    Serviceability

    Detailing Solid slabs

    Workshop - serviceability

    Flat Slab Design

    Other slabs

    Tying systems

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    Workshop serviceability

    www.eurocode2.info

    Introduction to workshop

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    Introduction to workshop

    problem

    This is example 3.4

    ofWorked examples

    to Eurocode 2:

    Volume 1.

    Week 4 - Workshop problems

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    Week 4 Workshop problems

    Design information

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    Worked example

    For the slab strip along grid line C check deflection is

    within design limits and ensure the crack widths inthe bottom of the slab are also limited.

    Design strip along grid line C

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    Design strip along grid line C

    Assume strip is 6 m wide

    As,req

    = 1324 mm2 B G

    = 1.25

    Check deflection andcracking slab along

    grid line C.

    Deflection

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    Deflection

    Check: basic l/dx F1 x F2 x F3 actual l/d

    1. Determine basic l/d

    The reinforcement ratio, =As,req/bd= 1324 x 100/(1000 x 260)

    = 0.51%

    Basic Span-to-Depth Ratios

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    Basic Span to Depth Ratios

    (for simply supported condition)

    20.5

    Percentage of tension reinforcement (As,reqd/bd)

    Spantodept

    hratio(l/d)

    This graph has beenproduced for K = 1.0

    StructuralSystem

    K

    Simply supported 1.0

    End span 1.3

    Interior Span 1.5

    Flat Slab 1.2

    Deflection

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    Deflection

    Check: basic l/dx F1 x F2 x F3 actual l/d

    1. Determine basic l/d

    The reinforcement ratio, =As,req/bd= 1324 x 100/(1000 x 260)

    = 0.51%

    From graph basic l/d= 20.5 x 1.2 = 24.6 (K= 1.2 for flat slab)

    2. Determine Factor F1

    F1 = 1.0

    3. Determine Factor F2(Assume no brittlepartitions)

    F2 = 1.0

    For flanged sections where the ratio of the flangebreadth to the rib breadth exceeds 3, the values ofl/dgiven by Expression (7.16) should be multiplied by 0.8.

    For flat slabs, with spans exceeding 8.5 m, whichsupport partitions liable to be damaged by excessivedeflections, the values of l/d given by Expression (7.16)should be multiplied by 8.5 / leff(leff in metres, see5.3.2.2 (1)).

    Deflection

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    4. Determine Factor F3

    As,req = 1324 mm2

    (ULS)Assume we require H16 @ 100 c/c (2010 mm2) to control deflection

    F3 =As,prov /As,req = 2010 / 1324 = 1.52 1.5

    24.6 x 1.0 x 1.0 x 1.5 9500 / 260

    36.9 36.5

    Crack Control Without Direct

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    CalculationEC2: Cl. 7.3.3

    Example Check cracking in bottom of slab.Gk = 8.5 kN/m

    2 Qk = 4.0 kN/m2

    2 = 0.3 (office loading) G = 1.25

    As,req = 1324 mm2/m

    Try H16 @ 100 As,prov = 2010 mm2/m

    Cracking

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    g

    Action 0 1 2Imposed loads in buildings,

    Category A : domestic, residentialCategory B : office areasCategory C : congregation areas

    Category D : shopping areas

    Category E : storage areas

    0.70.7

    0.7

    0.7

    1.0

    0.50.5

    0.7

    0.7

    0.9

    0.30.30.6

    0.6

    0.8Category F : traffic area, 30 kNCategory G : traffic area, 30160 kN

    Category H : roofs

    0.7

    0.7

    0.7

    0.50

    0.6

    0.30

    Snow load: H 1000 m a.s.l. 0.5 0,2 0Wind loads on buildings 0.5 0,2 00.7

    Determination of Steel Stress

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    252

    RatioG

    k/Q

    k

    Un

    modifiedste

    elstress,su

    Ratio Gk/Qk = 8.5/4.0 = 2.13

    Crack Widths

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    From graph su = 252 MPa

    s = (suAs,req) / (As,prov)

    s = (252 x 1324)/(1.0 x 2010)

    = 166 MPa

    For H16 @ 100 c/c

    Design meets both criteria

    Maximum bar size or spacing t o l imit

    cr ack wid t h

    Steelstress(s) MPa

    wmax

    = 0.3 mm

    Maximumbar size(mm)

    OR

    Maximumbar spacing(mm)

    160 32 300

    200 25 250

    240 16 200

    280 12 150

    320 10 100

    360 8 50

    For loading

    or restraintFor loading

    only

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    www.eurocode2.info

    Workshop problem

    Deflection & Cracking

    Workshop problem

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    For the edge stripindicated checkdeflection is within

    design limits andensure the crackwidths in the bottomare also limited.

    As,req = 959 mm2/m B

    d= 240 mm

    G = 1.25

    Design for this span

    Deflection

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    Check: basic l/dx F1 x F2 x F3 actual l/d

    1. Determine basic l/d

    The reinforcement ratio, =As,req/bd= 959 x 100/(1000 x 240)

    = 0.40%

    Basic Span-to-Depth Ratios

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    (for simply supported condition)

    26.2

    Percentage of tension reinforcement (As,reqd

    /bd)

    Spantodepthratio(l/d)

    This graph has beenproduced for K= 1.0

    StructuralSystem

    K

    Simply supported 1.0

    End span 1.3

    Interior Span 1.5

    Flat Slab 1.2

    Deflection

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    7.4.2 EN 1992-1-1

    Check: basic l/dx F1 x F2 x F3 actual l/d

    1. Determine basic l/d

    The reinforcement ratio, =As,req/bd= 959 x 100/(1000 x 240) =0.40%

    From graph basic l/d= 26.2 x 1.2 = 31.4 (K= 1.2 for flat slab)

    2. Determine Factor F1

    F1 = 1.0

    3. Determine Factor F2F2 = 1.0

    For flanged sections where the ratio of the flangebreadth to the rib breadth exceeds 3, the values ofl/dgiven by Expression (7.16) should be multiplied by 0.8.

    For flat slabs, with spans exceeding 8.5 m, whichsupport partitions liable to be damaged by excessivedeflections, the values of l/d given by Expression (7.16)should be multiplied by 8.5 / leff(leff in metres, see5.3.2.2 (1)).

    Deflection

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    4. Determine Factor F3

    As,req = 959 mm2

    (ULS)Assume we require H16 @ 200 c/c (1005 mm2) to control deflection

    F3 =As,prov /As,req = 1005 / 959 = 1.05 1.5

    31.4 x 1.0 x 1.0 x 1.05 5900 / 240

    33.0 24.5

    Cracking

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    Action 0 1 2Imposed loads in buildings,

    Category A : domestic, residentialCategory B : office areasCategory C : congregation areas

    Category D : shopping areas

    Category E : storage areas

    0.70.7

    0.7

    0.7

    1.0

    0.50.5

    0.7

    0.7

    0.9

    0.30.30.6

    0.6

    0.8Category F : traffic area, 30 kNCategory G : traffic area, 30160 kN

    Category H : roofs

    0.7

    0.70.7

    0.7

    0.50

    0.6

    0.30

    Snow load: H 1000 m a.s.l. 0.5 0,2 0Wind loads on buildings 0.5 0,2 0

    Determination of Steel Stress

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    252

    Ratio Gk

    /Qk

    Unmodifiedste

    elstress,su

    Ratio Gk/Qk = 8.5/4.0 = 2.13

    Crack Widths

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    From graph su = 252 MPa

    s

    = (su

    As,req

    ) / (As,prov

    )

    s = (252 x 959) /(1.0 x 1005)

    = 240 MPa

    For H16 @ 200 c/c

    Design meets both criteria

    Maximum bar size or spacing t o l imit

    cr ack wid t h

    Steel

    stress(s) MPa

    wmax = 0.3 mm

    Maximumbar size(mm)

    OR

    Maximumbar spacing(mm)

    160 32 300

    200 25 250

    240 16 200

    280 12 150

    320 10 100

    360 8 50

    For loading

    or restraintFor loading

    only

    Outline Week 4

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    We will look at the following topics:

    Designing for shear

    Serviceability

    Detailing Solid slabs Workshop - serviceability

    Flat Slab Design

    Tying systems

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    Flat Slab Design

    Paul Gregory

    Flat Slab Design

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    g

    Flat slabs - Introduction

    EC2 particular rules for flat slabs

    Initial sizing

    Analysis methods - BMs and Shear Force

    Design constraints

    Punching shear

    Deflection

    Moment transfer from slab to column

    Flat Slabs - Introduction

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    What are flat slabs?

    Solid concrete floors of constant thickness

    They have flat soffits

    Flat Slabs - Introduction

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    Column Head

    Waffle Slab

    Drop Panel

    Flat Slabs - Introduction

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    1. HANSON COBIAX2. BUBBLEDECK

    VOIDED SLABS

    Flat Slabs - Introduction

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    Hybrid (PC & In-situ) flat slabs

    Flat Slabs - Introduction

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    Hybrid (PC & In-situ) flat slabs

    Particular rules for flat slabs

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    Particular rules for flat slabs

    EC2 sections relevant to Flat Slabs:

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    Section 6 Ultimate Limit States

    cl 6.4 Punching (shear) & PD 6687 cl 2.16, 2.17 & 2.1.8

    Section 9 Detailing of members and particular rules

    Cl 9.4 Flat slabs

    9.4.1 Slab at internal columns

    9.4.2 Slab at edge and corner columns

    9.4.3 Punching shear reinforcement

    Annex I (Informative) Analysis of flat slabs and shear walls

    I.1 Flat Slabs

    I.1.1 General

    I.1.2 Equivalent frame analysisI.1.3 Irregular column layout

    The Concrete Society, Technical Report 64 - Guide to the

    Design and Construction of Reinforced Concrete Flat Slabs

    Particular rules for flat slabs

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    Distribution of momentsEC2: Figure I.1 Concise Figure 5.11

    Di ib i f

    Particular rules for flat slabs

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    Distribution of moments

    EC2: Table I.1 Concise: Table 5.2

    Particular rules for flat slabs

    EC2 Cl 9 4 C i 12 4 1

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    Arrangement of reinforcement should reflect behaviour

    under working conditions.

    At internal columns 0.5At should be placed in a width =0.25 panel width.

    At least two bottom bars should pass through internalcolumns in each orthogonal directions.

    EC2: Cl. 9.4 Concise: 12.4.1

    Particular rules for flat slabs

    EC2 Fig 9 9 C i Fig 5 12

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    Design reinforcement at edge and corner reinforcement

    should be placed within the becz

    cy

    y

    be = cz + y

    A

    cz

    cyy

    A

    be = z + y/2

    z

    A

    EC2: Figure 9.9 Concise Figure 5.12

    The maximum moment that can be transferred from the

    slab to the column should be limited to 0.17bed2fck

    Initial sizing

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    3 methods:

    1. Simple span to depth table

    2. Use Economic Concrete Frame Elements

    Imposed Load, Qk (kN/m2) 2.5 5 7.5 10

    Multiple Span 28 26 25 23

    3 methods:

    Initial sizing

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    3 methods:

    1. Simple span to depth table

    2. Use Economic Concrete Frame Elements

    3. Use Concept.xls

    Initial sizing

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    Initial sizing

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    8mEquivalent frame method

    Analysis Methods

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    Elastic Plane Frame Equivalent Frame Method, Annex I

    Tabular Method - Equivalent Frame Method, Annex I

    Grillage

    Yield Line Plastic method of design

    Finite Element Analysis

    Elastic method

    Elastic Plane Frame Equivalent Frame Method Annex I

    Analysis Methods

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    Elastic Plane Frame Equivalent Frame Method, Annex I

    Apply in both directions X and Y

    Method of Analysis for Bending Moments & SFs

    Equivalent Frame - the Beams are the Slab width

    Kslab = use full panel width for vertical loads.

    Kslab = use 40% panel width for horizontal loads. Annex

    I.1.2.(1)

    Analysis Methods

    L d

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    Load cases

    NA can use single load case provided:

    Variable load 1.25 x Permanent load Variable load 5.0 kN/m2

    Condition of using single load case is that Support BMs should be

    reduced by 20% except at cantilever supports

    Analysis Methods

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    TR 64 Figure 14

    Reduction in maximum hogging moment

    at columns

    Analysis Methods Equi Frame

    Distribution of Design Bending Moments, Annex I

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    Distribution of Design Bending Moments, Annex I

    Table I.1 Column Strip Middle Strip

    Negative 60 - 80% 40 - 20%

    Positive 50 - 70% 50 - 30%At = Reinforcement area to resist full negative moment. Cl 9.4.1

    Analysis Methods Equi Frame

    Distribution of Design Bending Moments - Example

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    400 mm2

    /m

    100 mm2/m

    100 mm2/m

    200 mm2/m

    200 mm2/m

    Distribution of Design Bending Moments ExampleTable I.1 Column Strip Middle Strip

    Negative 75% 25%

    At = Reinforcement area to resist full negative moment. Cl 9.4.1

    = 1600 mm2

    Column strip = 1200 mm2 Middle strip = 400 mm2

    Equivalent frame method

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    Equivalent frame method

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    Equivalent frame method - Elastic Plane Frame

    Analysis Methods

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    q

    Computer software normally used to assess bending moments and

    shear forces

    Design forfull load in both directions RC spreadsheet TCC33.xls will carry out the analysis and design

    Tabular MethodSimplest method

    Analysis Methods

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    Simplest method

    Use coefficients from Concise Tables 15.2 and 15.5 to determine

    bending moments and shear forces

    Design forfull load in both directions

    Frame lateral stability must not be dependent on slab-col connections

    There must be at least three approx equal spans.

    Method uses single load case. Note: No column BM given in table.

    Yield Line Method

    Analysis Methods

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    Equilibrium and work methods.

    work method

    External energy expended by

    the displacement of loads

    Internal energy dissipated by

    the yield lines rotating

    =

    Analysis Methods

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    Yield Line Method

    Suitable for:

    irregular layouts

    Slabs supported on 2 or 3

    edges only

    Detailed guidance and numerous

    worked examples contained in:

    Practical Yield Line Design

    Deflection design to simplified rules

    Finite Element Method

    Analysis Methods

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    Suitable for:

    irregular layouts

    slabs with service openings

    post tensioned design

    (specialist software)

    Common pitfalls:

    Use long term E-values (typically 1/3 to 1/2 short term value)

    Use cracked section properties (typically 1/2 gross

    properties) by adjusting E-value to suit

    Therefore appropriate E-values are usually 4 to 8 kN/mm2

    Finite Element Method

    Analysis Methods

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    Design moment is the integral of the section through the contour

    plot or the bay width

    Peak

    moment

    Integral for

    bay width

    Finite Element - Design moments

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    Distribution of top reinforcementAssume a total area ofsteel, At = 8000 mm

    2

    Distribution 75% Column strip & 25% Middle strip

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    Distance (m)

    600

    100

    200

    300

    400

    500

    0

    Bendingm

    oment(kNm/m)

    0 1 2 3 4 5 6 7 8

    Centre column strip:4000 mm2 or 2000 mm2/m

    Outer column strip:0.75 x 8000 4000= 2000 mm2 or 1000 mm2/m

    Middle strip:0.25 x 8000 = 2000 mm2

    or 500 mm2/m

    p p6000 mm2 2000 mm2

    Punching Shear - EC2: cl 6.4 and cl 9.4.3

    Design Constraints

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    g

    Traditional links

    Shear Rails

    Deflection:

    Design Constraints

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    Wherever possible use the span/effective depth ratios, cl 7.4.2 (2)

    Span is based on the longer span and the K factor is 1.2

    Reduction factor for brittle finishes for spans greater than 8.5m

    Moment Transfer from slab to column:

    Design Constraints

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    Edge and corner columns have limited capacity to transfer moments

    from slab redistribution may be necessary (Annex I.1.2 (5), EC2 cl

    9.4.2 & TR 64)

    Mt max = 0.17 be d2 fck

    Effectivewidth, be.

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    Flat slab Workshop

    Cover and Flexure

    Introduction to workshop

    problem

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    This is example 3.4ofWorked examples

    to Eurocode 2:

    Volume 1.

    Design strip along grid line C

    Determine the cover andreinforcement slab

    along grid line C

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    Assume strip is 6 m wide

    along grid line C.

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    Flat slab

    Workshop cover

    Worked example

    Determine Cover

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    Flat slab

    Workshop Flexure

    Sagging reinforcement Worked example

    Hogging reinforcement Workshop problem

    Design strip

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    From analysis

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    From analysis

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    (Using Concise table 15.5)

    z= d[ 1 + (1 - 3.529K)0.5]/2 = 260[1 + (1 3.529 x 0.069)0.5]/2 = 243 mm

    Alt

    ernativ

    e

    Workshop problem

    Now determine the reinforcement for the hogging

    moments

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    moments

    Hint: You will need to work out reinforcement for both

    column and middle strips and then work out how it is

    distributed.

    Solution

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    (Using Concise table 15.5)

    z= d[ 1 + (1 - 3.529K)0.5]/2 = 260[1 + (1 3.529 x 0.109)0.5]/2 = 232 mm

    Alte

    rnativ

    e

    Solution

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    (Using Concise table 15.5 )

    z= d[ 1 + (1 - 3.529K)0.5]/2 = 260[1 + (1 3.529 x 0.069)0.5]/2= 243 mm < 0.95d< 247 mm

    Alte

    rnativ

    e

    0.047

    Reinforcement distribution

    Total area of reinforcement:

    As tot = 2213 x 3 + 887 x 3 = 9300 mm2

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    As,tot 2213 x 3 887 x 3 9300 mm

    50% As,tot = 9300/2 = 4650 mm2

    This is spread over a width of 1.5m

    As,req = 4650/1.5 = 3100 mm2/m

    Use H20 @ 100 CTRS (3140 mm2/m)

    Remaining column strip:As,req = (2213 x 3 4650)/1.5 = 1326 mm

    2/m

    Use H20 @ 200 CTRS (1570 mm2/m)

    Middle strip: As,req = 887 mm2/m

    Use H16 @ 200 CTRS (1010mm2/m)

    Outline Week 4

    We will look at the following topics:

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    We will look at the following topics:

    Designing for shear

    Serviceability

    Detailing Solid slabs

    Workshop - serviceability

    Flat Slab Design

    Tying systems

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    Tying systems

    Tying systems (1) ALL concrete structures

    Peripheral ties (9.10.2.2) & NA:

    Ftie per = (20 + 4n0)l i 60kN where n0 is the number of storeys

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    Ftie,per (20 4n0)l i 60kN where n0 is the number of storeys

    Internal ties (including transverse ties) (9.10.2.3) & NA :

    Ftie,int = ((gk + qk)/7.5)(lr/5)Ft Ft kN/mWhere (gk + qk) is the sum of the average permanent and variable floor loads (kN/m2), lr is the

    greater of the distances (m) between the centres of the columns, frames or walls supporting any two

    adjacent floor spans in the direction of the tie under consideration and Ft = (20 + 4n0) 60kN.

    Maximum spacing of internal ties = 1.5 lr

    Horizontal ties to columns or walls (9.10.2.4) & NA :Ftie,fac = Ftie,col (2 Ft (ls /2.5)Ft) and 3% of NEdNEd = the total design ultimate vertical load carried by the column or wall at that level. Tying

    of external walls is only required if the peripheral tie is not located within the wall. Ftie,fac in

    kN per metre run of wall, Ftie,col in kN per column and ls is the floor to ceiling height in m.

    Internal Ties: EC2 specifies a

    Tying systems (2)

    ALL concrete structures

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    20kN/m requirement which is

    significantly less than BS8110.

    UK NA requirements similar to BS 8110

    Tying systems (3)

    Vertical ties (9.10.2.5):In panel buildings of 5 storeys or more, ties should be provided in

    columns and/or walls to limit damage of collapse of a floor

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    columns and/or walls to limit damage of collapse of a floor.

    Normally continuous vertical ties should be provided from the lowest

    to the highest level.

    Where a column or wall is supported at the bottom by a beam or slab

    accidental loss of this element should be considered.

    Continuity and anchorage ties (9.10.3):Ties in two horizontal directions shall be effectively continuous and

    anchored at the perimeter of the structure.

    Ties may be provided wholly in the insitu concrete topping or at

    connections of precast members.

    Week 4

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    END


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