A New Design Equation for Predicting the Joint Shear Strength of Mono Tonic Ally Loaded Exterior Beam-column Joints

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  • 8/3/2019 A New Design Equation for Predicting the Joint Shear Strength of Mono Tonic Ally Loaded Exterior Beam-column Joints

    1/13

    Engineering Structures 24 (2002) 11051117

    www.elsevier.com/locate/engstruct

    A new design equation for predicting the joint shear strength ofmonotonically loaded exterior beam-column joints

    P.G. Bakir ab,, H.M. Boduroglu a

    a Istanbul Technical University, Civil Engineering Department, Maslak 80626, Istanbul, Turkeyb Postal address: Yazmaci Tahir sok, Derya apt. no 11/4, Catalcesme, Suadiye, Istanbul, Turkey

    Received 11 June 2001; received in revised form 8 March 2002; accepted 8 March 2002

    Abstract

    In this study a new design equation for predicting the shear strength of monotonically loaded exterior beam column joints isproposed. For this purpose, the influence of several key variables on the behaviour of beam-column joints are inspected usingresults of parametric studies on an experimental database compiled from a large number of exterior joint tests. The design equationsuggested has three differences from the previously proposed equations. First, the equation proposed considers the influence ofbeam longitudinal reinforcement ratio, which was not taken into account in previously suggested design equations. Second, as theinfluence of this parameter is taken into account, a more realistic estimate of the influence of joint aspect ratio is obtained. Third,the influence of stirrups is considered differently for joints with low, medium and high amount of stirrup ratios, in a way, whichwas not considered in previously suggested equations. The results showed that the proposed design equation predicts the joint shearstrength of exterior beam column connections accurately with minimal standard deviation and is more reliable than the previouslysuggested equations. 2002 Elsevier Science Ltd. All rights reserved.

    Keywords: Reinforced concrete; Shear strength; Monotonically loaded exterior beam-column connections

    1. Introduction

    It is now generally believed that beam-column jointscan be critical regions in reinforced concrete framesunder severe seismic effects. Beam-column joint failureshave been observed in the 1980 El Asnam [1], 1985Mexico [2], 1986 San Salvador [3], 1989 Lome Prieta[4] and 1999 Kocaeli earthquakes [5]. During the pastforty years, significant amount of research has been car-ried out on seismic behaviour of beam-column joints allover the world. However, compared to cyclically loaded

    joints, little information exists in literature for predictingthe shear strength of monotonically loaded exterior

    joints.Remarkable differences exist in the design of joints

    for seismic loading or monotonic loading. Parameterssuch as column axial load, concrete cylinder strength,stirrup ratio, stirrup index, joint aspect ratio, beam

    Corresponding author. Fax: +90-216-386-9742.

    E-mail address: [email protected] (P.G. Bakir).

    0141-0296/02/$ - see front matter 2002 Elsevier Science Ltd. All rights reserved.

    PII: S0 1 4 1 - 0 2 9 6 ( 0 2 ) 0 0 0 3 8 - X

    reinforcement detailing, the ratio of beam longitudinalreinforcement etc influence the joint shear strength dif-ferently for interior or exterior and monotonically loadedor cyclically loaded joints. This investigation wasplanned with the objective of adding useful data to theunderstanding of the influences of the above-mentionedparameters on the joint shear strength of monotonicallyloaded exterior beam-column joints. Surprisingly, noneof the previously suggested design equations for mono-tonically loaded exterior joints consider the factors thatinfluence joint shear strength such as beam longitudinalreinforcement ratio, joint aspect ratio and concrete cylin-der strength together.

    2. Previously suggested design equations for

    exterior beam column joints

    In this section, the existing empirical design equationsfor predicting the shear strength of the monotonicallyloaded exterior beam-column joints are reviewed.

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    1106 P.G. Bakir, H.M. Boduroglu / Engineering Structures 24 (2002) 11051117

    2.1. The design equation of Sarsam and Phillips

    Sarsam and Phillips [6] have proposed the followingequation for the design of monotonically loaded exterior

    beam column connections.

    Vcol 5.08fcurc0.33dc

    db1.33bcdc1 0.29

    NuAg (1)

    where Vcol is the column shear force at the column-joint

    interface (N); fcu is the concrete cube strength (MPa); rcis the column longitudinal reinforcement ratio

    rc Aso/bcdc (2)

    where Aso is the area of the layer of steel furthest from

    the maximum compression face in a column (mm2); Agis the gross cross-sectional area of the column at the joint

    (mm2); Nu is the axial column load (N);dc is the effectivedepth of the layer of steel furthest away from the

    maximum compression face in a column (mm); db is theeffective depth of beam tension reinforcement (mm); bcis the width of column section at the joint (mm).

    The shear force resisted by the links is taken as:

    Vsd 0.87Ajsfyv (3)

    Vud Vcd Vsd (4)

    where Ajs is the total area of horizontal link reinforce-

    ment crossing the diagonal plane from corner to comer

    of the joint between the beam compression and tensionreinforcement (mm2); fyv is the tensile strength of the

    link reinforcement (MPa); Vsd

    is the design link shear

    force resistance (N); Vcd is the design shear force resist-

    ance of concrete in a joint (N); Vud is the design ultimate

    shear capacity of joint (N)

    All the joint stirrups are considered to be effective in

    increasing the joint shear capacity.

    2.2. The design equation of Vollum

    Vollum [7] proposed the following equation on the

    design of exterior beam column connections:

    Vc

    0.642b1

    0.555(2

    hb

    hc)beffhcfc (5)

    Vj Vc (Asjefyabeffhcfc) (6)

    a is taken as 0.2 for low, medium and high amount ofstirrups. b is 0.9 for U detail beam reinforcement and1 for L bent down. The joint shear strength should be

    limited to:

    Vj0.97beffhcfc1 0.555(2hbhc

    ) (7)1.33beffhcfc (8)

    where Asje is the cross-sectional area of the joint stirrups

    within the top five eighths of the beam depth below themain beam reinforcement (mm2); a is a coefficient thatdepends on factors including column load, concrete

    strength, stirrup index, and joint aspect ratio, which isconservatively taken as 0.2 in Vollums equation. Vc is

    the joint shear strength without stirrups (N); Vj is thetotal joint shear strength (N); hb is the section depth of

    the beam (mm); hc is the section depth of the column

    (mm); fc is the concrete cylinder strength (MPa); beff is

    the average of the beam and column widths (mm); fy is

    the yield strength of stirrups (MPa).

    2.3. Present design guidelines

    The ACI-ASCE Committee 352 [8], and EC8 [9] rec-

    ommend the following design equations for the shearstrength of monotonically loaded joints.

    Vjd 1.058fcbeffhc (ACI (9) ASCE Committee 352)

    Vjd 0.525f2/3c beffhc (EC8 ductility class DCL) (10)

    In order to investigate the reliability of the above

    design equations, the authors carried out several para-

    metric studies on monotonically loaded exterior beam-

    column joints. The parametric studies are explained in

    the next section followed by a comparison of the above

    design equations with the parametric studies of authors.

    3. Parametric studies on joint shear strength

    The authors carried out a parametric investigation of

    exterior beam-column joint behaviour based on 58 tests

    conducted in Europe. The loading in all the tests was

    monotonic. The authors realised that there might be

    important interactions between variables that at firstwere supposed to act independently and this necessitated

    viewing the entire population of results as a single para-

    meter. For this purpose, monotonically loaded exteriorbeam column joints are investigated through test results

    assembled and reconsidered as a unified whole. Examin-ing a large number of individual series of tests as a single

    database has the advantage of observing which variables

    have a significant influence on joint shear strength in alltests and which variables interact with each other. A newdesign equation is proposed based on the parametric

    studies carried out on the experimental database. Table

    1 shows the experimental database used in this study.

    The database comprises of the tests of Ortiz [10], Kord-

    ina [11], Scott [12], Scott & Hamill [13], Taylor [14],and Parker & Bullman [15]. The specimen forms

    included in the database are shown in Fig. 1(a). Fig. 1(b)

    shows the notations used in this study.

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    1107P.G. Bakir, H.M. Boduroglu / Engineering Structures 24 (2002) 11051117

    Table1

    Experimentaldatabase

    Investigator

    Specimen

    Detail

    H(mm)

    L(mm)

    hb/h

    c

    bc/bb

    Beam

    Columnrein.

    fc(MPa)

    Columnaxial

    SI(MPa)0.5

    Vjpredicted/Vjactual

    Failure

    rein.ratio

    ratio

    load

    modes

    Ortiz

    BCJ1

    Lbar

    2000

    1050

    1.33

    1.00

    1.1

    2.19

    34

    0

    0

    0.68

    is

    BCJ2

    Lbar

    2000

    1100

    1.33

    1.00

    1.1

    2.19

    38

    0

    0.16

    0.77

    is

    BCJ3

    Lbar

    2000

    1100

    1.33

    1.00

    1.1

    2.92

    33

    0

    0

    0.64

    is

    BCJ4

    Lbar

    2000

    1100

    1.33

    1.00

    1.1

    3.65

    34

    0

    0.33

    0.78

    is

    BCJ5

    Lbar

    2000

    1100

    1.33

    1.00

    1.1

    3.65

    38

    300

    0

    0.72

    Is

    BCJ6

    Lbar

    2000

    1100

    1.33

    1.00

    1.1

    3.65

    35

    300

    0

    0.68

    is

    BCJ7

    Lbar

    2000

    1100

    1.33

    1.00

    1.1

    3.65

    35

    300

    0.76

    0.68

    b

    Kordina

    RE2

    Lbar

    3000

    1000

    2.00

    1.00

    0.9

    2.41

    25

    240

    0

    0.66

    is

    RE3

    Lbar

    3000

    1000

    1.50

    1.00

    1.8

    2.41

    40

    400

    0.26

    0.96

    is

    RE4

    Lbar

    3000

    1000

    1.50

    1.00

    1.2

    2.41

    32

    51

    0.19

    0.83

    is

    RE6

    Lbar

    3000

    1000

    1.50

    1.00

    1.2

    2.41

    32

    213

    0.38

    0.91

    is

    RE7

    Lbar

    3000

    975

    1.40

    1.00

    1.3

    1.61

    26

    650

    0.43

    0.87

    is

    RE8

    Ubar

    3000

    975

    1.40

    1.00

    1.3

    1.61

    28

    525

    0.42

    0.90

    is

    RE9

    Ubar

    3000

    975

    1.40

    1.00

    1.3

    1.61

    28

    770

    0.41

    0.86

    is

    RE10

    Ubar

    3000

    975

    1.56

    1.00

    1.2

    1.61

    24

    551

    0.45

    0.94

    is

    Taylor

    P1/41/24

    Lbar

    1290

    470

    1.43

    1.40

    2.4

    4.10

    33

    240

    0.3

    0.97

    is

    P2/41/24

    Lbar

    1290

    470

    1.43

    1.40

    2.4

    4.10

    29

    240

    0.3

    0.94

    is

    P2/41/24A

    Lbar

    1290

    470

    1.43

    1.40

    2.4

    4.10

    47

    240

    0.26

    0.92

    is

    A3/41/24A

    Lbar

    1290

    470

    1.43

    1.40

    2.4

    4.10

    27

    240

    0.3

    0.88

    is

    D3/41/24

    Lbar

    1290

    470

    1.43

    1.40

    2.4

    4.10

    53

    60

    0.24

    0.89

    is

    B3/41/24

    Lbar

    1290

    470

    1.43

    1.40

    2.4

    4.10

    22

    240

    0.75

    0.92

    is

    C3/41/24BY

    Ubar

    1290

    470

    1.43

    1.40

    2.4

    4.10

    32

    240

    0.31

    1.04

    is

    C3/41/13Y

    Ubar

    1290

    470

    1.43

    1.40

    1.4

    4.10

    28

    240

    0.33

    0.95

    is

    Scott

    C1AL

    Lbar

    1700

    750

    1.40

    1.36

    1.1

    4.29

    33

    50

    0.188

    0.87

    is

    C4

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    41

    275

    0.203

    0.89

    is

    C4A

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    44

    275

    0.196

    0.86

    is

    C4AL

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    36

    50

    0.218

    0.86

    is

    C7

    Lbar

    1700

    750

    2.00

    1.36

    1.4

    4.29

    35

    275

    0.22

    0.90

    is

    C3L

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    35

    50

    0.22

    1.03

    is

    C6

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    40

    275

    0.21

    1.05

    is

    C6L

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    46

    50

    0.19

    0.94

    is

    C9

    Ubar

    1700

    750

    2.00

    1.36

    1.4

    4.29

    36

    275

    0.22

    0.93

    is

    (co

    ntinuedonnextpage)

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    1108 P.G. Bakir, H.M. Boduroglu / Engineering Structures 24 (2002) 11051117

    Table1(continued)

    Investigator

    Specimen

    Detail

    H(mm)

    L(mm)

    hb/h

    c

    bc/bb

    Beam

    Columnrein.

    fc(MPa)

    Columnaxial

    SI(MPa)0.5

    Vjpredicted/Vjactual

    Failure

    rein.ratio

    ratio

    load

    modes

    Scott

    &C4ALN0

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    42

    50

    0

    0.88

    p

    Hamil

    C4ALN1

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    46

    50

    0.229

    0.85

    js

    C4ALN3

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    42

    50

    0.478

    0.78

    js

    C4ALN5

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    50

    50

    0.718

    0.85

    js

    C4ALH0

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    104

    100

    0

    0.86

    p

    C6LN0

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    51

    50

    0

    0.92

    js

    C6LN1

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    51

    100

    0.19

    0.96

    js

    C4ALH1

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    95.2

    100

    0.159

    0.93

    b

    C4ALH3

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    105.6

    100

    0.302

    0.97

    b

    C4ALH5

    Lbar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    98.4

    100

    0.469

    1.00

    b

    C6LN3

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    49

    50

    0.44

    0.92

    js

    C6LN5

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    37

    50

    0.765

    0.74

    js

    C6LH0

    Ubar

    1700

    750

    1.40

    1.3

    2.1

    4.29

    101

    100

    0

    0.72

    js

    C6LH1

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    102

    100

    0.153

    0.98

    js

    C6LH3

    Ubar

    1700

    750

    1.40

    1.36

    2.1

    4.29

    97

    100

    0.472

    0.93

    js

    Parker

    4a

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    1.09

    39

    0

    0

    -

    c

    4b

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    1.09

    39

    300

    0

    1.05

    js

    4c

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    1.09

    37

    600

    0

    0.83

    js

    4d

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    4.38

    39

    0

    0

    0.97

    js

    4e

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    4.38

    40

    300

    0

    0.92

    js

    4f

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    4.38

    38

    600

    0

    0.78

    js

    5a

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    2.67

    42

    0

    0.404

    -

    c

    5b

    Lbar

    2000

    850

    1.67

    1.20

    0.9

    2.67

    43

    300

    0.4

    1.08

    js

    5d

    Lbar

    2000

    850

    1.67

    1.20

    1.4

    2.67

    43

    0

    0.6

    -

    c

    5e

    Lbar

    2000

    850

    1.67

    1.20

    1.4

    2.67

    45

    300

    0.589

    -

    c

    5f

    Lbar

    2000

    850

    1.67

    1.20

    1.4

    2.67

    43

    600

    0.6

    0.86

    js

    Average

    0.88

    Standarddevi-0.10

    ation

    Note:Ciscolumnfailure;bisbeamfailure;jsisjointshearfailure;pisconnection

    zonereinforcementpulloutfailure.

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    1109P.G. Bakir, H.M. Boduroglu / Engineering Structures 24 (2002) 11051117

    Fig. 1. (a) Typical specimen shape in the experimental database. (b)

    Typlical elevation and notations used for exterior beam colum joints.

    (c) The strut and truss mechanisms.

    It is commonly accepted that beam column joints

    resist shear by the strut and truss mechanisms as sug-

    gested first by Paulay [16] as shown in Fig. 1(c). Thestrut mechanism accounts for the contribution of the con-

    crete, whereas the truss mechanism represents the contri-

    bution of stirrups to joint shear strength. In this study,

    the resistance of the concrete to the joint shear will be

    determined first and then the influence of the stirrupswill be added.

    4. Influence of concrete cylinder strength

    The relation between maximum joint shear stress atthe instant of joint failure and the uni-axial compressive

    stress of concrete fc is shown in Fig. 2. The authors car-

    ried out a regression analysis and found that concrete

    Fig. 2. The influence of concrete cylinder strength on joint shear

    strength.

    cylinder strength is related to the joint shear strength by

    the following equation.

    nj0.9155fc (11)where f

    c

    is the uniaxial concrete cylinder strength with-

    out any factors of safety and vj is in MPa.

    C4ALHO and C4ALNO of Scott have been investi-

    gated in order to find the possible influences of the inter-action of other parameters with the concrete cylinder

    strength. These specimens were deliberately chosen so

    as to eliminate other factors such as stirrups, columnaxial load and joint aspect ratio. Because they had no

    stirrups, they had similar joint aspect ratios and they

    belonged to the same group of tests.

    The analysis confirmed the above relationshipbetween the concrete cylinder strength and the joint

    shear strength. Hamill has also suggested that the joint

    shear strength is proportional to the square root of theconcrete cylinder strength.

    5. Determining the joint shear strength

    The joint shear is calculated using the following pro-

    cedure:

    Mb P(L d1) (12)

    where P is the failure load (N); L is the distance fromthe point of application of the load to the face of the

    column (mm); d1 is the cover (mm).

    A value is assumed for the strain in the beam tensile

    reinforcement. The force in the beam tensile reinforce-

    ment and the moment produced by it are calculated and

    if this is equal to the moment calculated in Eq. (2), theprocedure is stopped. If not, the strain assumed is

    increased in small increments up until, the moment is

    equal to the moment given in Eq. (2). The reinforcement

    was assumed to have an elastic modulus of 200 GPa.

    The joint shear strength is calculated as below:

    Vj TbVcol (13)

    where Vj is the joint shear force (N); Tb is the tensile

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    1110 P.G. Bakir, H.M. Boduroglu / Engineering Structures 24 (2002) 11051117

    force in the beam longitudinal reinforcement (N); Vcol is

    the shear force in the upper column (N).

    The normalised joint shear strength is determined as:

    nj Vj

    beffhcfc(14)

    where beff is the average of the beam and the column

    width; fc is the concrete cylinder strength; hc is the height

    of the column.The unit of v j is (MPa)

    0.5.

    6. Influence of column reinforcement ratio

    The authors made a parametric study on the specimensin the experimental database which failed by joint shear,

    which had low amount of stirrups and which weredetailed by L bars bent down detail. Parker and

    Bullmann specimens were deliberately excluded fromthis parametric study because they have high joint aspect

    ratios and low beam reinforcement ratio. Furthermore

    due to low column longitudinal reinforcement ratio and

    low column axial stress, some of them have failed due

    to column failure. The Kordina specimens were also

    excluded as they are provided by inclined reinforcement

    in their joints which significantly increased their jointshear strength. The parametric study in Fig. 3 clearly

    shows that joint shear strength is independent of the col-

    umn longitudinal reinforcement ratio in joints that fail

    by joint shear failure.

    The authors also analysed the joints of Parker andBullman. The analysis of specimens 4a and 4d of Parker

    and Bullman showed that these two specimens were

    identical except for their column longitudinal reinforce-

    ment ratios. The provision of 75% less column reinforce-ment than specimen 4d, did not only decrease the joint

    shear strength of specimen 4a, but also caused the speci-men 4a to fail by column failure instead of joint shear

    failure. It can be concluded that, the joints that have low

    column longitudinal reinforcement ratios and column

    axial stresses are more likely to fail by column hinging

    Fig. 3. The influence of the column longitudinal reinforcement ratio

    on the normalised joint shear strength.

    and consequently have lower joint shear strengths with

    respect to joints that fail by joint shear failure.

    7. Influence of beam longitudinal reinforcement

    ratio

    The authors having investigated the specimens of

    Parker and Bullman decided that the possible low

    strength of Parker and Bullman specimens apart fromdetailing and high joint aspect ratio as well as low radius

    of bend could be the very low beam longitudinal

    reinforcement ratio. The relation between the beam

    longitudinal reinforcement ratio and the normalised joint

    shear strength is demonstrated in Fig. 4. Fig. 4 shows

    that the ratio of the beam longitudinal reinforcement isrelated to the normalised joint shear strength by the fol-

    lowing equation:

    njAsbbbd0.4289

    (15)

    where Asb is the total area of beam reinforcement; bb is

    the breadth of the beam; d is the depth of the beam.

    In order to understand the possible influence of theratio of beam longitudinal reinforcement on the joint

    shear strength, the authors investigated the specimens

    C4AL and C1AL of Scott, which were nearly identicalexcept the beam reinforcement ratios they had. The joint

    shear strength of C1AL that had a beam longitudinal

    reinforcement ratio of 1.1 was nearly 30% lower than

    C4AL that had a beam reinforcement ratio of 2.1. The

    analysis of these two specimens showed that the beamlongitudinal reinforcement is related to the normalisedjoint shear strength by the above equation.

    8. Influence of beam reinforcement detailing

    The beam reinforcement detailing affects both the nor-

    malised joint shear strength and the failure modes of

    joints. The authors analysis of two identical specimensof Kordina with different beam reinforcement detailing

    Fig. 4. The influence of the beam longitudinal reinforcement ratio on

    the normalised joint shear strength.

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    showed that the joint shear strengths of monotonically

    loaded exterior beam column connections decrease by

    15% if detailed by U bars rather than L bars. This is

    shown in Fig. 5. Inspection of Scott and Hamill speci-

    mens C4ALH3 (L bars bent down detail) and C6ALH3(U bars detail) which were identical except for their

    beam reinforcement detailing shows that providing Lbars bent down detail reinforcement can change the fail-

    ure modes of monotonically loaded exterior beam col-

    umn connections from joint shear to beam failure.Further inspection of Kordina specimens with that of

    Ortiz or Scott shows that the normalised joint shear

    strengths of Kordina specimens are significantly higherthan that of other researchers specimens. The authorsare of the opinion that there are two important reasons

    for this. First, the specimens of Kordina except for RE4are detailed by inclined reinforcement, which signifi-cantly increases the normalised joint shear strength.

    Second, the concrete cylinder strengths of Kordinasspecimens have been underestimated because they are

    based on the minimum rather than the average cube

    strengths. The consequence of this is that the normalised

    joint shear strengths may have been overestimated.

    9. Influence of the vertical anchorage length and

    the radius of bend

    The analysis of BCJ3 of Ortiz showed that the joint

    shear strength of BCJ3 was considerably increased com-pared to other specimens of Ortiz with low amount ofstirrups. The authors are of the opinion that this increase

    is due to higher vertical anchorage length and higherradius of bend of beam reinforcement of Ortiz specimen

    BCJ3. Thus, it can be concluded that there is evidence

    from Ortiz tests that the shear strength of joints can be

    increased if the vertical anchorage length is higher than

    26db (db is the diameter of beam reinforcement) and the

    radius of bend is higher than 8db.

    Fig. 5. The normalised joint shear strength of identical specimens

    with different beam reinforcement detailing.

    10. Influence of joint aspect ratio

    The authors have carried out a parametric study toinvestigate the influence of the joint aspect ratio on thenormalized joint shear strength. The specimens whichfail by failure modes other than joint shear failure, the

    U bar specimens, the specimens with inclined bars, allof Parker and Bullmann specimens, all specimens with

    medium and high amount of stirrups are excluded from

    this study. In order to minimise the possible interaction

    of parameters such as the concrete cylinder strength and

    the beam longitudinal reinforcement ratio, the joint shear

    strength is normalised by the square root of the concrete

    cylinder strength and the 0.4289 power of the beamlongitudinal reinforcement ratio. Fig. 6 shows the

    relation between the joint aspect ratio and the normalised

    joint shear strength. It is evident that the joint aspect

    ratio is related to the normalised shear strength as shown

    in Eq. (16).

    Vj

    beffhcfchb

    hc0.61 (16)

    where hb is the cross-sectional height of the beam; hc is

    the cross-sectional height of the column.In order to investigate the possible interactions of dif-

    ferent parameters, the authors also inspected C7 and

    C4AL of Scott, which were the only test data available

    that investigates the joint aspect ratio. The notable differ-

    ence between C7 and C4AL was that they had got differ-

    ent beam reinforcement ratios as well as different jointaspect ratios. Analysis of the test data confirmed the

    reliability of Eq. (16).

    11. Influence of Joint Stirrups

    Without the influence of transverse reinforcement, theauthors design equation takes the following form:

    Vc

    0.71bg100Asbbbd

    0.4289

    hbhc0.61

    bc bb2

    hcfc (17)

    Fig. 6. The influence of the joint aspect ratio on the joint shear

    strength normalised by the concrete sylinder strength and the beam

    reinforcement ratio.

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    where b 0.85 for joints detailed by U bars and b 1 for joints detailed by L bars. and g 1.37 for inclined

    bars in the joint and g 1 for others.The constant 0.71 is a capacity reduction factor

    determined empirically. The authors have plotted the

    joint shear strengths of the specimens in the experi-

    mental database and their stirrup ratios in Fig. 7. It isvery apparent from the figure that the relation betweenthe stirrup ratio and the normalised joint shear strength

    is tri-linear. Up to stirrup ratios of 0.003, the joints are

    named as joints with low amount of stirrups. Joints with

    joint stirrup ratios between 0.003 and 0.0055 are named

    as joints with medium amount of stirrups. All the stirrups

    yield within this region. When the stirrup ratio is higher

    than 0.0055, not all the stirrups yield as evident from

    the analysis of specimen BCJ7 of Ortiz and C4ALN3 ofScott and Hamill and the contribution of stirrups to joint

    shear strength substantially reduces under the yield

    capacity of stirrups.

    The stirrups that are considered effective in this study

    are those that are situated above beam compressive

    chord and below the top beam reinforcement. This is

    because, the reported stirrup strains of Ortiz specimen

    BCJ7 and BCJ4 both showed that the stirrup strains sub-

    stantially reduce if positioned between the beam tensile

    reinforcement and the beam compressive chord. Fig. 1

    shows this.It is commonly assumed in the literature [16] that joint

    shear strength is given by the addition of concrete resist-

    ance to shear, symbolising the resistance of the concrete

    strut mechanism and stirrup yield capacity, symbolising

    the resistance of the truss mechanism:

    Vj Vc Asjefy (18)

    where Vc is the joint shear strength of the concrete

    (without stirrups); Asje is the area of the stirrups; fy is

    the stirrup yield strength.

    As mentioned above, the analysis of tests showed that

    when the joints have a stirrup ratio higher than 0.0055,

    not all the stirrups yield within the joint. The authors are

    of the opinion that Eq. (18) should be corrected as:

    Fig. 7. The influence of stirrup ratio on the joint shear strength.

    Vj

    beffhcfc vc

    aAsjefy

    behcfc(19)

    Therefore the final equation can be formulated as:

    Vj

    0.71bg

    100

    Asb

    bbdb

    0.4289

    bc bb

    2 hcfc

    hbhc0.61

    (20)

    aAsjefy

    where a 0.664 for joints with low amount of stirrups;a 0.6 for joints with medium amount of stirrups;a 0.37 for joints with high amount of stirrups

    The stirrups not only affect the normalised joint shearstrength but also the failure modes of joints. The authorsinspection of joints C4ALNO (no stirrup in joint) and

    C4ALN1 (single stirrup in joint) of Scott and Hamill has

    shown that provision of a single stirrup in joints whichhave hc/db ratios less than 10 changes the failure mode

    from connection zone reinforcement pull out to jointshear failure. Furthermore, it is apparent from the datab-

    ase that anchorage failures are not anticipated in joints

    which have medium or high amount of stirrups.

    12. Influence of column axial stress

    The authors have depicted the relation between the

    normalised joint shear strength and the column axial

    stress in Fig. 8. There is considerable scatter in the

    experimental data. The results show that the columnaxial load certainly does not influence the joint shearstrength of monotonically loaded exterior beam column

    connections. Vollum reaches a similar conclusion.

    Nevertheless, the authors investigation of the speci-mens of Parker and Bullman showed that column axial

    load influences the behaviour of joints by changing theirfailure modes. The authors comparison of Parker andBullmann specimen 4a with specimens 4b, 4c showed

    that the former failed by column failure while the lattertwo specimens all failed by joint shear failure. The

    Fig. 8. The influence of the column axial stress on the normalised

    joint shear strength.

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    experimental data indicates that high column axial

    stresses and high column longitudinal reinforcement

    ratios are necessary in order to avoid column failures.

    13. Critique of previously suggested design

    equations for exterior beam column joints

    In this section, the previously suggested empirical

    equations are discussed and compared with the designequation of authors. Because the influence of beamlongitudinal reinforcement ratio is not taken into

    account, previous researchers estimates of the influenceof the joint aspect ratio on the joint shear strength are

    flawed. None of the previously suggested design equa-tions take account of the influence of the stirrups realisti-cally. Using the authors new proposal, a more realisticestimate of joint shear strength was obtained.

    13.1. Remark on Sarsam and Phillips equation

    The authors as well as Vollums analysis showed thatthe column axial load does not influence the joint shearstrength. Contrary to the experimental evidence, Sarsam

    and Phillips equation suggests that column axial loadinfluences the joint shear strength.

    Furthermore, all stirrups are considered as effective in

    Sarsam and Phillips equation while the tests of Ortiz

    showed that the effective stirrups are those that are situ-

    ated above the beam compressive chord and below the

    beam reinforcement. Sarsam and Phillips equation pre-

    dicts that all the transverse reinforcement yield. How-ever, inspection of BCJ7 of Ortiz demonstrates clearlythat not all the stirrups yield in some joints.

    Sarsam and Phillips equation predicts that column

    longitudinal reinforcement ratio affects the joint shear

    strength. However, the parametric study of authors inFig. 6 showed that there is no apparent relationship

    between the column longitudinal reinforcement ratio and

    the normalised shear strength of joints that fail by joint

    shear failure.

    The equation predicts that there is a linear relationshipbetween the concrete cube strength and the normalised

    joint shear strength. The authors parametric study inFig. 3 showed that the normalised joint shear strength is

    proportional to the square root of the concrete cylinder

    strength. The equation of Sarsam and Phillips overesti-

    mates the influence of the concrete cylinder strength onthe normalised joint shear strength.

    13.2. Remark on the design equation of Vollum

    As mentioned in the above paragraphs, beamreinforcement ratio significantly influences the jointshear strength of exterior joints. Vollums equation neg-lects the influence of beam longitudinal reinforcement

    Fig. 9. The influence of the beam reinforcement ratio on the predicted

    normalised joint shear strength of the Vollum equation.

    ratio on the joint shear strength. Because the effect ofbeam longitudinal reinforcement ratio is disregarded, the

    equation incorrectly predicts a linear relationship

    between the joint aspect ratio and the joint shear

    strength. If the above parameters are taken into account,

    joint shear strength is predicted as proportional with the

    0.61 power of the joint aspect ratio as given by the sug-

    gested equation in this paper.

    Vollum has not given the basis of the upper limits

    chosen. It is not clear what the basis of the constant 0.97is. Moreover, the author suggests that the other limit

    1.33fcbeffhc is chosen because it is the highest shearstrength of the database used by the author. So the accu-

    racy of the above constraint is limited by the experi-

    mental database used. The authors are of the opinion that

    more experiments are needed to propose upper limits for

    joint shear strength.The authors plotted Vjpredicted/Vjactual values for both

    Vollum and the authors equation against beamreinforcement ratio, joint aspect ratio, stirrup ratio and

    the stirrup index in Fig. 916. The figures clearly showthat the authors model is an improvement on the designequation of Vollum. The suggested design equation is

    more conservative than Vollum equation under varying

    beam reinforcement ratio, joint aspect ratio, stirrup ratio

    and the stirrup index.

    Fig. 10. The influence of the beam reinforcement ratio on the pre-

    dicted joint shear strength of authors equation.

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    Fig. 11. The influence of the joint aspect ratio on the normalised joint

    shear strength predicted by Vollum.

    Fig. 12. The influence of the joint aspect ratio on the predicted shear

    strength of the authors equation.

    Fig. 13. The influence of the stirrup ratio on the predicted joint shear

    strength of the Vollum equation.

    Fig. 14. The influence of the stirrup ratio on the predicted joint shear

    strength of the authors equation.

    Fig. 15. The influence of the stirrup index on the predicted joint shear

    strength of Vollums equation.

    Fig. 16. The influence of the stirrup index on the predicted joint shear

    strength of the authors equation/

    14. Present design guidelines

    Both the ACI-ASCE Committee 352 [8], and EC8 [9]

    methods calculate the joint shear strength on the assump-tion that the tensile reinforcement yield and for bothequations factors of safety are included. The above

    methods are considered to be inadequate by the authors

    because they neglect the influence of the stirrups, beamlongitudinal reinforcement ratio, and joint aspect ratio

    on the joint shear strength.

    14.1. Comparison of the parametric studies with the

    established principles of joint mechanics

    In order to investigate the reliability of the parametric

    studies in Fig. 29, the authors investigated the estab-lished equations on the basic mechanics of reinforced

    concrete beam-column joints. This has been also pre-

    viously discussed by Paulay [17] and by Bonacci & Pan-

    tazopoulou for interior joints [18] who have also takeninto account the joint deformations. Both of the authors

    use the average stresses for equilibrium as shown in Fig.

    18. The typical loading system considered in analysis of

    exterior beam-column joints is shown in Fig. 17. Fig. 18

    depicts the equilibrium of vertical and horizontal forces.Fig. 18 shows that equilibrium of forces in the horizontal

    direction require the average transverse compressive

    stress in the joint sx defined as:

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    Fig. 18. Stress equilibrium.

    Fig. 17. Joint geometry.

    sx Asb

    beffhbfs

    Asje

    beffhbfw (21)

    where fs is the average stress in the beam reinforcement;

    fw is the average stress in the transverse reinforcement.

    Consequently, the average normal concrete stress in

    the y direction sy can be expressed as :

    sy Ascol

    beffhcfscol

    N

    beffhc(22)

    where fscol is the average stress in the column reinforce-

    ment; N is the column axial loadDefining the average joint shear stress in the joint as

    tav, the maximum principal stress associated with thestress tensor is given as;

    s sx tav 0

    tav sy 0

    0 0 sz (23)where sz is the confining stress provided by stirrups inthe z direction.

    s3 I1s2 I2sI3 0 (24a)

    In order to determine the principal stresses, Eq. (24a)

    has to be solved; where I1 sx sy sz

    I2 sxsy sysz sxszt2av (24b)

    I3 sxsyszszt2av (24c)

    The tensile stress in the concrete is negligible and

    therefore s1 0, which consequently gives:

    sy t

    2

    av

    sx(25)

    From the Mohrs circle,

    tan2q 2tav

    sxsy(26)

    If Eq. (25) is substituted into Eq. (26), the following

    quadratic equation ensues:

    t2av 1tanq

    tanqsxtavs2x 0 (27)which gives:

    tav sx

    tanq(28)

    Using Eq. (25), we have:

    sy tav

    tanq(29)

    Collins and Mitchell [19] suggest the following equation

    for the maximum stress in concrete panels:

    f2max fc

    0.8 170e1fc (30)

    The principal compressive stress is given by:

    s2 2 e20.002

    e20.002

    2f2max (31)s2 is also given from Mohrs circle as:

    s2 sx sy tavtanq 1tanq (32)

    Thus the average joint shear stress can be expresses as:

    tav s2

    tanq 1tanq(33)

    Eq. (30)(33) show very clearly that as the principaltensile strain increases, the average joint shear stress

    decreases. Thus it is necessary to express the principaltensile strain in terms of the strains in the x and y direc-

    tions in order to investigate the factors that influence the joint shear strength. From Mohrs circle, it is knownthat:

    tan2q g

    exey(34)

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    From Mohrs circle, the principal tensile strain will be:

    e1 (ex ey)

    2(exey)2

    2

    g22 (35)

    If Eq. (34) is substituted into Eq. (35) and appropriate

    trigonometric transformations are carried out, Eq. (36)given by Bonacci and Pantazopoulou is obtained.

    e1 exeytan2q1tan2q (36)

    The next step will be to express the strains in the x

    and y directions in terms of the stresses.

    sx tavtanq Asbfs

    beffhb

    Asjefw

    beffhb Asb

    beffhbm (37)

    Asje

    beffhbfw

    where

    m fs/fw (38)

    The strain in the x direction can therefore be

    expressed as:

    ex fw

    Es

    tavtanq

    EsAsbmbeffhb

    Asje

    beffhb

    (39)

    The strain in the y direction can similarly be

    expressed as:

    ey fscol

    Es tav

    tanq

    N

    beffhc beffhcAscolEs

    (40)

    If Eq. (39) and (40) are substituted into Eq. (36):

    e1 1

    Es(1tan2q)tavtanq 1Asb

    beffhbm

    Asje

    beffhb

    (41)

    1

    Ascol

    beffhc Ntan2q

    beffhcAscol

    beffhcIt is evident from the inspection of experiments that

    cracks extend throughout the diagonal of the joint. So

    the angle of principal stresses can be expressed as:

    tanq hb

    hc(42)

    If Eq. (42) is substituted into Eq. (41),

    e1 1

    Es1hbhc2tavhbhc 1Asbmbeffhb Asjebeffhb (43)

    1

    Ascol

    beffhc Nhbhc

    2

    Ascol The above equation shows that the principal tensile

    strain is increased by the joint aspect ratio and column

    longitudinal reinforcement ratio and the axial load on

    the column whereas it is decreased by increasing beam

    longitudinal reinforcement ratio and the stirrup ratio. The

    shear stress in the joint is dependent on the principal

    tensile strain as evident from Equations 30 and 33. It is

    therefore evident from Eq. (28)(29) and (43) that the

    joint shear strength increases as the beam longitudinalreinforcement ratio and the transverse reinforcement

    ratio increases. Eq. (29) shows that the joint shear

    strength increases as the column load and the column

    longitudinal reinforcement increases but Eq. (43) shows

    that as the longitudinal column reinforcement and the

    column load increases, the principal tensile stresses

    increase which consequently decreases the normalised

    joint shear strength. Therefore the increase in the joint

    shear strength due to Eq. (29) is offset by the increasein the principal tensile strain. The above conclusions are

    totally in accordance with the predictions of theauthors equation.

    15. Conclusions

    The purpose of this investigation was to study the

    effect of the parameters influencing the behaviour ofbeam to column connections and to determine if the

    present design guidelines are unconservative. From the

    analysis of the tests and results of the parametric studies,the following design recommendations can be made.

    1. All the experimental evidence points to the fact that

    the U bar details should not be used in monotonically

    loaded exterior beam column joints. As mentioned in

    the upper paragraphs, providing L bars bent downdetail beam reinforcement can change the failure

    modes of monotonically loaded exterior beam-column

    joints from joint shear to beam failure. Furthermore,

    the joint shear strength of joints is increased by 15%

    if detailed by L bars bent down detail beam reinforce-ment.

    2. Experimental evidence shows that anchorage failures

    are not anticipated in joints with stirrups in monoton-

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    ically loaded exterior beam column joints. In joints

    without stirrups on the other hand, hc/db values should

    be larger than 10 in order to avoid anchorage failures.

    3. Column axial load has no influence on ultimate shearcapacity of the joint but high column axial load and

    high column longitudinal reinforcement ratios are

    necessary in the joint to avoid column failures.4. Transverse reinforcement in the joint improves the

    joint shear capacity but not in the same ratio as indi-

    cated by the addition rule Vc+Vs. The authors plottedthe stirrup ratio against the joint shear strength. The

    results showed that the diagram is trilinear. Based on

    this parametric study, the authors classified the stir-rups into three in increasing the joint shear strength.

    Up to stirrup ratios of 0.003, the joints are named as

    joints with low amount of stirrups. Joints with joint

    stirrup ratios between 0.003 and 0.0055 are named as

    joints with medium amount of stirrups. All the stir-

    rups yield within this region. When the stirrup ratiois higher than 0.0055, not all the stirrups yield as evi-

    dent from the analysis of specimen BCJ7 of Ortiz and

    C4ALN3 of Scott and Hamill and the contribution of

    stirrups to joint shear strength substantially reduces

    under the yield capacity of stirrups. Parametric studies

    further carried out on the experimental database in

    Table 1 showed that the addition rule Vc+Vs, shouldbe corrected as (Vc aVs)beffhcfc where is 0.664for low amount of stirrups, 0.6 for medium amount

    of stirrups, 0.37 for high amount of stirrups.

    5. Increasing the beam longitudinal reinforcement ratio

    increases the joint shear strength. Because the influ-ence of beam longitudinal reinforcement ratio is taken

    into account, the proposed equation predicts that the

    joint shear strength is proportional to (hb/hc)0.61.

    6. The present guidelines, design equations and code

    recommendations for predicting the shear strength of

    monotonically loaded exterior beam column joints are

    unconservative. The suggested design equation gives

    more conservative and reliable results for predicting

    the joint shear strength under varying beam longitudi-

    nal reinforcement ratio, joint aspect ratio, stirrup ratio

    as well as stirrup index.

    7. The analysis of BCJ3 of Ortiz shows that the joint

    shear strength will further increase if the verticalanchorage length is higher than 26db and the radius

    of bend of beam bars are higher than 8db. The authors

    are of the opinion that these figures can be used aslower limits for the radius of bend and vertical

    anchorage length.

    8. The authors applied their equation on the experi-

    mental database in Table 1. The results showed that

    the average Vjpredicted Vjtest values for the authors equ-

    ation applied on all the experiments in the experi-

    mental database is 0.88 and the standard deviation is

    0.1. The results show that the equation suggested

    gives realistic and conservative estimates of the joint

    shear strength.9. The extremely good results of the proposed design

    equation on the experimental database confirmed andsupported the value of the parametric studies.

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