Kruger & RA

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    18|The Structural Engineer 17 May 2005

    technical note: bs 8007

    I

    n a previous Technical Note by one of

    the authors2 it was shown that the sepa-

    rate equations for flexure and combined

    tension are based on similar premises.A

    method was proposed to proportion the

    tensile stiffening force to the two layers of

    reinforcement by considering horizontal

    and moment equilibrium of the stiffening

    forces.This method results in the neutral

    axis of the stiffening strain diagram not

    coinciding with the neutral axis of the

    section under the applied forces.

    Some literature suggests, however, that

    the stiffening strains should emanate from

    the neutral axis position in all cases.This

    approach gives a seamless consistency

    throughout the whole range of possible

    combinations of moment and tensile force.The authors set out an improved method

    for proportioning the tensile stiffening

    force to the two layers of reinforcement for

    certain cases in order to achieve this.It

    also provides revised equations for the

    case where the neutral axis is between

    face 2 and its adjacent reinforcement.

    Notationa1 distance from face 1 to centroid of

    reinforcement at face 1

    a2 distance from face 2 to centroid of

    reinforcement at face 2

    acr distance from point considered to

    surface of the nearest longitudinal barAs1 area of reinforcement at face 1

    As2 area of reinforcement at face 2

    b width of section considered (normally

    1m)

    cmin minimum cover to tension steel

    c1 minimum cover to reinforcement at

    face 1

    c2 minimum cover to reinforcement at

    face 2

    e eccentricityT

    M=

    Ec modulus of elasticity of concrete (1/2

    the instantaneous value when used

    to determine e)

    Es modulus of elasticity of reinforcement

    fc compressive stress in concretefcu 28 day characteristic (cube) strength

    of concrete

    fs1 stress in reinforcement at face1

    fs2 stress in reinforcement at face2

    fs1 stiffening stress in reinforcement at

    face 1

    fs2 stiffening stress in reinforcement at

    face 2

    fstif1 stiffening tensile stress in concrete at

    face 1

    fstif2 stiffening tensile stress in concrete at

    face 2

    fy characteristic strength of reinforce-

    ment

    Fstif total stiffening tensile force in

    concrete

    Fstif1 portion of stiffening tensile force

    acting at level of steel at face 1

    Fstif2 portion of stiffening tensile force

    acting at level of steel at face 2

    h overall depth of section

    k1 a constant h a

    a1

    2

    = -< Fk2 a constant a

    h a1

    2=

    -< FK a constant for a particular section

    under a certain configuration of

    moment and axial tension

    eh

    a

    eh

    a

    2

    2

    1

    2

    =- +

    + -J

    L

    KKKK

    N

    P

    OOOO

    M applied moment at section considered

    n1 ratio hx

    T applied axial tension at section

    consideredw design surface crack width

    w1 design surface crack width at face 1

    w2 design surface crack width at face 2

    x distance to the neutral axis from

    face 2

    xstif apparent neutral axis depth of stiff-

    ening strain from face 2

    e modular ratioE

    Es

    c=b l

    11 strain at face 1 ignoring stiffening

    effect of concrete

    12 strain at face 2 ignoring stiffening

    effect of concrete

    m average strain at level where crack-ing is being considered

    s1 strain in reinforcement at face 1

    s2 strain in reinforcement at face 2

    s1 strain reduction in reinforcement at

    face 1 due to tension stiffening of

    concrete

    s2 strain reduction in reinforcement at

    face 2 due to tension stiffening of

    concrete

    1 ratio of reinforcement at face1

    bhAs1

    =d n2 ratio of reinforcement at face2

    bhAs2

    =d nNote:Generally subscripts 1 and 2 refer to

    faces 1 and 2 of the section respectively

    IntroductionThe author2 showed that the separateequations for flexure and direct tension

    are based on similar premises,and that

    eqn (1) of BS8007:Appendix B, i.e.

    w

    h xa c

    a

    1 2

    3

    mincr

    cr m=

    +-

    -

    f

    d n...(1)

    can be used both for flexure and for

    direct tension.He then indicated that it

    can therefore be assumed that eqn (1) will

    also apply to the case of combined flexure

    and direct tension.

    Combined flexure and direct tensionFor combined flexure and direct tension,two cases; (i) Complete section in tension

    and; (ii) Section partially in compression,

    can be considered:

    Case 1:Complete section in tension

    Determining the neutral axis depth:

    Equations (9) to (15) in Kruger2 still apply.

    Proportioning the stiffening force:

    Previous method:Consider a section as

    shown in Fig1.The author2 proposed a

    method for proportioning the total stiffen-

    ing force to the two layers of reinforcement

    by considering horizontal and moment

    equilibrium of the stiffening forces,Fstif1andFstif2.

    Apportionment according to this

    method results in the neutral axis of the

    stiffening strain diagram not coinciding

    with the neutral axis of the section under

    the applied forces,i.e. xstifx. However, the

    lecture notes of the British Cement

    Association3 contains a figure that seems

    to suggest that the stiffening strains

    should emanate from the neutral axis

    position.It is generally accepted that this

    is the case when the neutral axis lies

    within the section,so it would be consis-

    tent to adopt the same approach when the

    neutral axis is beyond the section.Proportioning the stiffening force:

    Improved method:Consider a section

    with width, b, as shown in Fig 2.Sayfs1andfs2 are the tensile stiffening stresses

    in the two layers of reinforcement.With

    Improved crack width calculation method toBS 8007 for combined flexure and direct tension

    BS 80071

    includes recommendations for the calculation ofdesign crack widths for sections under flexure and forsections under direct tension. It does not providerecommendations for sections under the combined forces. Ina previous technical note2 Erhard Kruger set out a method forcalculating crack widths under combined loads. Now withRobin Atkinson he proposes an improvement on the method.

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    17 May 2005 The Structural Engineer|19

    technical note: bs 8007

    the neutral axis position at x 0,the

    maximum stiffening tensile stress in the

    concrete is:

    .

    .

    /

    /

    f for w

    and f for w

    N mm mm

    N mm mm

    23

    0 2

    1 0 1

    stif

    stif

    12

    12

    = =

    = =

    ...(2)

    Sincex is negative,it follows from the

    figure that:

    f fh x

    xstif stif 2 1=-

    -__ ii ...(3)The total stiffening force is:

    Ff f

    bh2

    stifst if stif 1 2

    =+e o ...(4)

    The tensile stiffening forces in the two

    reinforcement layers are:

    F f A

    F f A

    stif s s

    stif s s

    1 1 1

    2 2 2

    =

    =

    l

    l...(5)

    From horizontal equilibrium:

    F f A f Astif s s s s1 1 2 2= +l l ...(6)

    Sincex is negative,it follows from the

    figure that:

    h x a

    fa x

    fs s

    1

    1

    2

    2

    - -=

    -

    l l...(7)

    Therefore

    fh x a

    f a xs

    s

    21

    1 2

    =- -

    -l

    l _ i...(8)

    Substituting equation (8) in equation (6)

    and re-arranging, it follows that:

    fA

    h x aa x

    A

    Fs

    s s

    stif1

    11

    22

    =+

    - --

    l ...(9)

    Similarly:

    f

    a xh x a

    A A

    Fs

    s s

    stif

    2

    11 2

    2 =

    -- -

    +

    l ...(10)

    But, from the diagram:

    a xh x a

    f

    f

    s

    s

    2

    1

    2

    1

    -- -

    = ...(11)

    Substituting equation (11) in equations

    (9) and (10):

    ff A f A

    fFs

    s s s s

    sstif1

    1 1 2 2

    1=

    +l ...(12)

    ff A f A

    fFs

    s s s s

    sstif2

    1 1 2 2

    2=

    +l ...(13)

    Fstifcan be determined from equations

    (2) to (4).

    When the neutral axis position is atx

    h (Fig 3):

    .

    .

    /

    /

    f w

    f w

    N mm for mm

    and N mm for mm

    23

    0 2

    1 0 1

    stif

    stif

    22

    22

    = =

    = =

    ...(14)

    As previously, equations (12) and (13)

    can be used to determine the tensile stiff-

    ening stress in the two layers of reinforce-

    ment.

    Determining the average strain: By

    dividing both sides of equations (12) and

    (13) by Youngs modulus for steel,Es, the

    effective reduction in strain in the rein-forcement due to the stiffening effect of

    concrete is:

    f A f AFs

    s s s s

    sstif1

    1 1 2 2

    1=

    +f fD ...(15)

    f A f A Fs s s s ss

    stif1 1 2 22

    2

    = +f

    f

    D ...(16)

    These equations differ from those in the

    previous method (equations (24) and (25)).

    Equations (26) to (33) in Kruger2 can still

    be used to eventually calculate the design

    crack widths.

    Case 2:Section partially in compression

    Determining the neutral axis position:

    Strictly speaking, two cases have to be

    considered, i.e.

    x < a2wherefs2 0 (i.e.compression)

    x a2wherefs2 > 0 (i.e. tension)

    Whenx a2:

    The equations previously given by the

    author2 apply to this case.The positionx of

    the neutral axis is given by equation 17

    (originally eqn 34)2 : (see panel 1)

    where nhx

    1 = andeT

    M= .The concrete

    stress,fc and steel stresses,fs1 andfs2, can

    be determined from equations (35) to (37)

    in Kruger2.

    When:x < a2:

    By settingnh

    a1

    2= in equation (17), the

    value of the eccentricity,e, can be deter-

    mined for whichx a2 i.e.(See Eq 18,

    panel 1).

    For this casefs1 andfs2 are both tensile.

    If these are defined as positive,andfc as

    negative,and by considering horizontal

    and moment equilibrium, the position of

    the neutral axis,x can be determined from

    the equation (19) (see panel 1):

    where nhx

    1 = andeT

    M= .

    The concrete stress,fc, can be deter-

    mined from Eq (20) (see panel 1)

    The equations for steel stresses are

    again given by equations (36) and (37)

    previously presented in Kruger2.

    It should be noted that both equa-tions (17) and (19) are cubic,and therefore

    the solution ofn1 can also be found

    directly as described by Tuma4 or on the

    web page:

    http://mathforum.org/dr.math/faq/faq.cubi

    c.equations2.html.

    Proportioning the stiffening force:As

    shown in Fig 4 and Fig 5, the maximum

    stiffening tensile stress in the concrete is

    again given by Eq (2).

    When 0

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    20|The Structural Engineer 17 May 2005

    technical note: bs 8007

    .

    .

    ,

    F f h x b

    b h xw

    b h xw

    for mm and

    for mm

    21

    30 2

    20 1

    stif stif1= -

    =-

    =

    =-

    =

    ___

    iii

    ...(21)

    The values offs1 andfs2 can again be

    determined from equations (12) and (13)

    respectively.

    When a2 x < hAs previously explained by the author2

    and from Fig 5, it is clear that the

    complete stiffening force acts on the rein-

    forcement in face 1 as in the case of flexure

    only and equation (43) from Kruger2 still

    applies.

    Determining the average strain: When

    0