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Support CenterKnowledge Base Articles5.3 Strength verifications in Detail 3D
ConcreteKnowledge baseDetail 2DEN (Eurocode)Cracks

5.3 Strength verifications in Detail 3D

This article is also available in
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The different verifications required by ACI 318-19 are assessed based on the direct results provided by the model. Verifications are carried out for concrete strength, reinforcement strength, and anchorage (bond shear stresses).

Strength - Concrete

The concrete strength in compression is evaluated as the ratio between the maximum Equivalent principal stress fc,eq (also σc,eq in previous text) obtained from FE analysis and the limit value f'c,lim.

Equivalent Principal Stress expresses the equivalent uni-axial stress for a general tri-axial stress state.

fc,eq=σc3−σc1f_{c,eq} = \sigma_{c3} - \sigma_{c1}fc,eq​=σc3​−σc1​

The fc,eq value can, therefore, be directly compared with uniaxial strength limits. This expression is derived from the implementation of the Mohr-Coulomb plasticity theory, conservatively assuming the angle of internal friction φ = 0°.

Strength - Reinforcement

The strength of the reinforcement is evaluated in both tension and compression as the ratio between the stress in the reinforcement at the cracks fs and the specified limit value fy,lim.

fy,lim=ϕs⋅fyf_{y,lim} = \phi_{s} \cdot f_{y}fy,lim​=ϕs​⋅fy​

Strength - Anchors

Anchors are checked for normal stresses in a similar way to reinforcement, where the limit value fy,lim is determined. 

To make it easier to navigate the following text, we will first divide anchoring into three groups in terms of code-checking according to ACI or AISC.

Group 1

  • Anchorage Types
    • Cast-in plate
    • Base plate - Stand-off = direct 
    • Base plate - Stand-off = Mortar joint - thickness of mortar less than 0.5 times the anchor diameter
    • Single anchor with projected length less than 0.5 times anchor diameter
  • Anchor code-checks (ACI / AISC)
    • Tension/compression
      • All anchor types in tension – ACI 318-19 chap. 17.6.1.2  
      • All anchor types in compression – AISC 360-16 chap. E
    • Shear without lever arm
      • Bolt material – ACI 318-19 chap. 17.7.1.2 (b)
      • Headed studs – ACI 318-19 chap. 17.7.1.2 (a)
      • Reinforcement – ACI 318-19 chap. 17.7.1.2 (b)
    • Interaction of tension and shear - ACI 318-19 chap. 17.8

Group 2

  • Anchorage Types
    • Base plate - Stand-off = Mortar joint - thickness of mortar more than 0.5 times the anchor diameter
  • Anchor code-checks (ACI / AISC)
    • Tension/compression
      • All anchor types in tension – ACI 318-19 chap. 17.6.1.2  
      • All anchor types in compression – AISC 360-16 chap. E
    • Shear with lever arm
      • Bolt material – ACI 318-19 chap. 17.7.1.2 (b) + chap. 17.7.1.2.1.
      • Headed studs – ACI 318-19 chap. 17.7.1.2 (a) + chap. 17.7.1.2.1.
      • Reinforcement – ACI 318-19 chap. 17.7.1.2 (b) + chap. 17.7.1.2.1.
    • Interaction of tension and shear - ACI 318-19 chap. 17.8

Group 3

  • Anchorage types
    • Base plate - Stand-off = gap
    • Single anchor with projected length more than 0.5 times the anchor diameter
  • Anchor code-checks (ACI / AISC)
    • Tension/compression (with buckling)
      • All anchor types in tension – ACI 318-19 chap. 17.6.1.2
      • All anchor types in compression – AISC 360-16 chap. E3
    • Bending
      • For all anchor types – AISC 360-16 chap. F11
    • Shear
      • For all anchor types – AISC 360-16 chap. G
    • Interaction of axial force and bending
      • NPn+MMn≤1\dfrac{N}{P_n}+\dfrac{M}{M_n}\le 1Pn​N​+Mn​M​≤1 

Tensile resistance of anchor according to ACI 318-19 chap. 17.6.1.2

ϕNsa=ϕa,t Ase,N futa\phi N_{sa}=\phi_{a,t}\,A_{se,N}\,f_{uta}ϕNsa​=ϕa,t​Ase,N​futa​

where:

  • ϕa,t  – strength reduction factor for anchors in tension according to ACI 318-19 chap. 17.5.3 (a)
  • Ase,N – tensile stress area (reduced by thread)
  • futa – specified tensile strength of anchor steel and shall not be greater than 1.9 fya and 860 MPa

Shear resistance of anchor according to ACI 318-19 chap. 17.7.1.2 (a)

The steel strength in shear for headed studs is determined as:

ϕVsa=ϕa,V Ase,V futa\phi V_{sa}=\phi_{a,V}\,A_{se,V}\,f_{uta}ϕVsa​=ϕa,V​Ase,V​futa​

where:
ϕa,v – strength reduction factor for anchors in tension according to ACI 318-19 chap. 17.5.3 (a)
Ase,V – tensile stress area (reduced by thread)
futa – specified tensile strength of anchor steel and shall not be greater than 1.9 fya and 860 MPa

Shear resistance of anchor according to ACI 318-19 chap. 17.7.1.2 (b)

The steel strength in shear for anchors from bolt material and reinforcement is determined as:

ϕVsa=ϕa,V 0.6 Ase,V futa\phi V_{sa}=\phi_{a,V}\,0.6\,A_{se,V}\,f_{uta}ϕVsa​=ϕa,V​0.6Ase,V​futa​

where:

  • ϕa,v  – strength reduction factor for anchors in tension according to ACI 318-19 chap. 17.5.3 (a)
  • Ase,V – tensile stress area (reduced by thread)
  • futa – specified tensile strength of anchor steel and shall not be greater than 1.9 fya and 860 MPa

Shear resistance of anchor connected to a base with mortar - ACI 318-19 chap. 17.7.1.2.1

If anchors are used with built-up grout pads (Group 2), the design strength calculated in accordance with 17.7.1.2 shall be multiplied by 0.80.

Interaction in tension and shear according to ACI 318-19 chap. 17.8

It shall be permitted to neglect the interaction between tension and shear if (a) or (b) is satisfied.
(a) Nua/(ϕNn) ≤ 0.2
(b) Vua/(ϕVn) ≤ 0.2 

If Nua/(ϕNn) > 0.2 for the governing strength in tension and Vua/(ϕVn) > 0.2 for the governing strength in shear, then Eq. (17.8.3) shall be satisfied.

NuaϕNn+VuaϕVn≤1.2\frac{N_{ua}}{\phi N_n}+\frac{V_{ua}}{\phi V_n}\le 1.2ϕNn​Nua​​+ϕVn​Vua​​≤1.2

Compressive resistance of anchor according to AISC 360-16 chap. E3

Pn=ϕa,c Fcr AgP_n =\phi_{a,c}\, F_{cr}\, A_{g}Pn​=ϕa,c​Fcr​Ag​

where:

  • ϕa,t  – the strength reduction factor for anchors in compression according to AISC 360-16 chap. E1
  • (a) When: Lcr≤4.71EFy\dfrac{L_c}{r} \le 4.71\sqrt{\dfrac{E}{F_y}}\quadrLc​​≤4.71Fy​E​​  or     FyFe≤2.25\dfrac{F_y}{F_e}\le 2.25Fe​Fy​​≤2.25
    • Fcr=(0.658 Fy/Fe)FyF_{cr}=\left(0.658^{\,F_y/F_e}\right)F_yFcr​=(0.658Fy​/Fe​)Fy​
  • (b) When: Lcr>4.71EFy\dfrac{L_c}{r} > 4.71\sqrt{\dfrac{E}{F_y}}\quadrLc​​>4.71Fy​E​​  or     FyFe>2.25\dfrac{F_y}{F_e}> 2.25Fe​Fy​​>2.25
    • Fcr=0.877FeF_{cr}=0.877F_eFcr​=0.877Fe​
  • Ag​ – gross cross-sectional area of member
  • E – modulus of elasticity of steel
  • Fe=π2E(Lcr)2F_e=\dfrac{\pi^2 E}{\left(\dfrac{L_c}{r}\right)^2}Fe​=(rLc​​)2π2E​ - elastic buckling stress
  • Fy – specified minimum yield stress of the type of steel being used
  • r=IAsr=\sqrt{\dfrac{I}{A_s}}r=As​I​​ – radius of gyration
  • I=πds464I=\dfrac{\pi d_s^4}{64}I=64πds4​​ – moment of inertia of the bolt 

Bending resistance of anchor according to AISC 360-16 chap. F11

Mn=ϕa,b Z Fy ≤1.6 ϕa,b Sx FyM_n=\phi_{a,b}\, Z\, F_y\, \le 1.6\,\phi_{a,b}\, S_x\, F_yMn​=ϕa,b​ZFy​≤1.6ϕa,b​Sx​Fy​

where:

  • Z=ds36Z=\dfrac{d_s^{3}}{6}Z=6ds3​​ – plastic section modulus of the bolt
  • Sx=2IdsS_x=\dfrac{2I}{d_s}Sx​=ds​2I​ – elastic section modulus of the bolt

Shear resistance of anchor according to AISC 360-16 chap. G

Vn=ϕa,v 0.6 Av FyV_n=\phi_{a,v}\,0.6\,A_v\,F_yVn​=ϕa,v​0.6Av​Fy​

where:

  • AV = 0.844As – the shear area
  • As – the bolt area reduced by threads

Concrete crushing at the anchor–concrete interface

The anchor shear resistance is also limited from the point of view of concrete crushing at the anchor–concrete interface. The limit values and the method for determining them are described in detail in the article - Shear behaviour of anchors in reinforced concrete. Once the contact force reaches this limit, the stop criterion is triggered, and the analysis is terminated before the resistance is exceeded.​ 

Pull-out check for headed anchors (Washer plates and Headed studs)

For headed anchors, an additional stop criterion is implemented to check the concrete bearing (crushing) above the anchor head - pull-out. During the analysis, the compressive force transferred through the head-to-concrete contact is monitored and compared with the limit value given by ACI 318-19, Clause 17.6.3.2.2a (pull-out failure of headed fastenings).

Npn=Φ⋅Ψc,p⋅8⋅Abrg⋅fc′N_{pn} = \Phi \cdot \Psi_{c,p} \cdot 8 \cdot A_{brg} \cdot f'_cNpn​=Φ⋅Ψc,p​⋅8⋅Abrg​⋅fc′​
​

where:

  • Φ\PhiΦ is the strength reduction factor - Table 17.5.3(c)
  • Abrg net bearing area of the head of stud, anchor bolt, or headed deformed bar (without the shank area). 
  • f'c is the specified compressive strength of concrete
  • Ψc,p\Psi_{c,p}Ψc,p​ is the pullout cracking factor according to 17.6.3.3, and is always taken as 1.0, i.e. the value for cracked concrete. This is consistent with the CSFM approach used in Detail, where the tensile strength of concrete is neglected and the concrete is assumed to be cracked in tension.

Once the contact force reaches this code-based limit, the stop criterion is triggered, and the analysis is terminated before the pull-out resistance is exceeded.​ 

Anchorage -  Bond stress

The bond shear stress is evaluated independently as the ratio between the bond stress τb calculated by FE analysis and the bond strength fbu.

Although the bond strength is not explicitly defined in ACI 318-19, the calculation of the development length can be found in Section 25.4.2. However, since the bond strength is the basic input for determining the development length, see R25.4.1.1 and ACI Committee 408 1966, the bond strength can be calculated as follows:

Let us assume that if we anchor the reinforcement bar into a concrete block to the development length ld or greater, pulling out the reinforcement will lead to rupture of the reinforcement and not to pulling out of the concrete. This can be written with the following formula.

π⋅db⋅ld⋅fbu=fy⋅As\pi\cdot d_{b} \cdot l_{d} \cdot f_{bu}=f_{y}\cdot A_{s}π⋅db​⋅ld​⋅fbu​=fy​⋅As​

where:

db is the diameter of the reinforcement bar, ld is the development length, fbu is the bond strength, fy is the yield strength of the reinforcement, and As is the area of the reinforcement rebar.

From the preceding, the formula for calculating bond strength can be easily derived:

fbu=fy⋅Asπ⋅db⋅ldf_{bu}=\frac{f_{y}\cdot A_{s}}{\pi\cdot d_{b} \cdot l_{d} }fbu​=π⋅db​⋅ld​fy​⋅As​​

The development length ld is then determined according to ACI 318-19 Table 25.4.2.3 as follows:

ld=(fy⋅ψt⋅ψe⋅ψgC⋅λfc′)⋅dbl_{d}=\left( \frac{f_{y}\cdot\psi_{t}\cdot\psi_{e}\cdot\psi_{g}}{C\cdot\lambda\sqrt{f'_{c}}} \right)\cdot d_{b}ld​=(C⋅λfc′​​fy​⋅ψt​⋅ψe​⋅ψg​​)⋅db​

where:

C = 25 (2.1 for metric) for no. 6 and smaller bars and deformed wires, C = 20 (1.7 for metric) for no. 7 and larger bars, λ = 1.0 for normal weight concrete, ψt, ψe, ψg are determined according to ACI 318-19 Table 25.4.2.3. 

Only uncoated or zinc-coated (galvanized) reinforcement is supported, so ψe = 1.0. ψg is automatically determined from the reinforcement grade, and ψt is automatically derived from the position of the reinforcement in the model and from the direction of concreting that can be set in the application for each project item as follows.

Fig. 5.3.1Direction of concreting\textsf{\textit{\footnotesize{Fig. 5.3.1\qquad Direction of concreting}}}Fig. 5.3.1Direction of concreting

These verifications are carried out with respect to the appropriate limit values for the respective parts of the structure (i.e., in spite of having a single grade both for concrete and reinforcement material, the final stress-strain diagrams will differ in each part of the structure due to tension stiffening and compression softening effects).

Anchorage -  Total force

Total force Ftot and limit force Flim

The total force Ftot is a result of the finite element analysis and can be defined in two ways.

Ftot=As⋅fsF_{tot}=A_{s} \cdot f_{s}Ftot​=As​⋅fs​

where As is the area of the reinforcement bar and fs is the stress in the bar.

Or as a sum of the anchorage force Fa and the bond force Fbond.

Ftot=Fa+FbondF_{tot}=F_{a}+F_{bond}Ftot​=Fa​+Fbond​

where Fa is the actual force in the anchorage spring and Fbond is the bond force that can be obtained by integrating the bond stress τb along the length of reinforcement bar l.

Fbond=Cs⋅∫0lτb(x)dxF_{bond}=C_{s} \cdot \int_{0}^{l}\tau_{b}\left( x \right)dxFbond​=Cs​⋅∫0l​τb​(x)dx

Cs is the circumference of the reinforcement bar.

The limit force Flim is the maximum force in the element of the rebar considering the strength of the rebar and also anchoring conditions (bond between concrete and reinforcement and anchorage hooks, loops, etc.).

Flim=min(Flim,bond+Fau,Fu)F_{lim}=min\left( F_{lim,bond}+F_{au},F_{u} \right)Flim​=min(Flim,bond​+Fau​,Fu​)

Fu=fy,lim⋅AsF_{u}=f_{y,lim}\cdot A_{s}Fu​=fy,lim​⋅As​

Fau=β⋅fy,lim⋅AsF_{au}=\beta\cdot f_{y,lim}\cdot A_{s}Fau​=β⋅fy,lim​⋅As​

Flim,bond=Cs⋅l⋅fbuF_{lim,bond}=C_{s}\cdot l \cdot f_{bu}Flim,bond​=Cs​⋅l⋅fbu​

where Cs is the circumference of the reinforcement bar, and l is the length from the beginning of the rebar to the point of interest.

Fig. 5.3.2Definition of the limit force Flim\textsf{\textit{\footnotesize{Fig. 5.3.2\qquad Definition of the limit force Flim}}}Fig. 5.3.2Definition of the limit force Flim

Flim,2=Flim,1+Flim,addF_{lim,2}=F_{lim,1}+F_{lim,add}Flim,2​=Flim,1​+Flim,add​

where Flim,add is the additional force calculated from the magnitude of the angle between neighboring elements. Flim,2 must be always lower than Fu.

The available anchorage types in CSFM include a straight bar (i.e., no anchor end reduction), 90-degree hook, 180-degree hook, perfect bond, and continuous bar. All these types, along with the respective anchorage coefficients β, are shown in Fig. 5.3.3 for longitudinal reinforcement. The values of the adopted anchorage coefficients are derived from the comparison of the equation from section ACI 318-19 25.4.3.1 and equations taken from section ACI 318-19 25.4.2.3. It should be noted that, in spite of the different available options, CSFM distinguishes three types of anchorage ends: (i) no reduction in the anchorage length, (ii) a reduction of 30% of the anchorage length in the case of a normalized anchorage, and (iii) perfect bond.

Fig. 5.3.3 Available anchorage types and respective anchorage coefficients for longitudinal reinforcing bars in CSFM:\textsf{\textit{\footnotesize{Fig. 5.3.3\qquad  Available anchorage types and respective anchorage coefficients for longitudinal reinforcing bars in CSFM:}}}Fig. 5.3.3 Available anchorage types and respective anchorage coefficients for longitudinal reinforcing bars in CSFM:

(a) straight bar; (b) 90-degree hook; (c) 180-degree hook; (d) perfect bond; (e) continuous bar\textsf{\textit{\footnotesize{(a) straight bar; (b) 90-degree hook; (c) 180-degree hook; (d) perfect bond; (e) continuous bar}}}(a) straight bar; (b) 90-degree hook; (c) 180-degree hook; (d) perfect bond; (e) continuous bar

The anchorage coefficient for stirrups is always - β = 1.0.

In order to comply with ACI, the anchorage spring should be used in the calculation, the anchorage spring is modified by the β coefficient so the user must use one of the available anchorage types when defining the reinforcement start and end conditions. 

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