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This calculator allows the user to assess the structural integrity of concrete columns to ensure compliance with the Australian Standard AS 3600. The calculation will identify the design capacities of concrete columns to meet axial, flexural and shear design requirements to Ultimate Limit State (ULS) methods.
❗ This calculation has been written in accordance with AS3600:2018.
Column cross-section with symbols used in this calculator


📃 List of symbols used in this calculator

Calculation

Technical notes

  1. The calculator does not calculate second order effects of slender columns, it assumes the input design bending moment (M*) takes into account any second order effects.
  1. Currently you can only input rectangular sections in the calculator.

Inputs

Material Properties



γc
:24kN/m3



f'c
:40MPa



Ec
:32800MPa



Es
:200000MPa



fsy
:500MPa



Loads

Section and Reinforcement Geometry



Lu
:6000mm



D
:600mm



b
:600mm


Tensile Reinforcement, Ast:


Tensile reinforcement diameter
:32mm



Number of tensile reinforcement bars
:4


Compressive Reinforcement, Asc:


Compressive reinforcement diameter
:32mm



Number of compressive reinforcement bars
:4


Shear Reinforcement:


Stirrup diameter
:12mm



Spacing of legs
:200



Number of legs
:2

Cover:


Exposure classification
:A2



Formwork and compaction method (1)
:Self-compacting concrete



Design life (years)
:60

Using a design life of 120 years requires additional 5mm cover


cst
:30mm



csc
:30mm

This cover distance is to the surface of the first steel reinforcement, either longitudinal or shear, from top and bottom concrete fibres.


Column Restraints

AS 3600:2018 Figure 10.5.3(A) - effective length factor (k) for columns with simplified end restraints

End #1


Rotation - #1
:Fixed



Translation - #1
:Fixed

End #2


Rotation - #2
:Fixed



Translation - #2
:Fixed





Output

Section Properties



Ag
:360000mm2



Zx
:36000000mm3



Zy
:36000000mm3



Ixx
:10800000000mm4



Iyy
:10800000000mm4




Ast
:3217mm2



Asc
:3217mm2



Area of shear reinforcement, Asv
:226mm2



Total minimum cover
:20mm



dst
:542mm



dsc
:58mm



Distance to centroid of shear reinforcement, dsv
:564mm



Column and Slenderness Properties



k
:0.7



Le
:4200mm



r
:180mm



sr
:23.33



Column classification
:Braced, Short


Column Strength Checks

Interaction Curve (combined flexural and axial check)



(M*, N*) < Interaction curve
:FAIL

Squash Load


SL - ϕ
:0.65



SL - φNuo
:9905kN

Decompression Point


DP - ku
:1



DP - ϕ
:0.6



DP - ϕNu
:6398.4kN



DP - ϕMu
:594.8kN m

Balanced Point


BP - ku
:0.54545



BP - ϕ
:0.6



BP - ϕNu
:2892kN



BP - ϕMu
:960kN m

Pure Bending


PB - kuo
:0.135



PB - ϕ
:0.85



PB - ϕMu
:689kN m





Flexural Checks



ϕMu / M*
:0.36



ϕMu > M*
:PASS


Minimum moment check:


Mu,min
:163.93kN m



M* > Mu,min
:PASS


Longitudinal reinf. check:


As,min
:3600.0mm2



As,max
:14400.0mm2



As > As,min
:PASS



As ≤ As,max
:PASS

As,min = 1% of Ag
As,max = 4% of Ag
Ductility check:


kuo
:0.1347



kuo < 0.36
:PASS




Shear Checks



θ
:36degree



bv
:600mm



dv
:432mm



kv
:0.15



Vuc
:245.9kN



Vus
:336.2kN



ϕVu
:436.6kN



V*/ϕVu
:0.11



ϕVu > V*
:PASS

Minimum shear reinf. check:


Minimum Asv/s
:0.607mm2/mm



Asv/s
:1.131mm2/mm



Asv/s > Asv/s,min
:PASS




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Explanation

Columns are typically subject to combined compression and bending load and should be checked using an interaction curve, as per Cl 10.6.2 of AS3600:2018. An interaction curve is a graphical representation of the ultimate strength of a column's cross-section. It is defined by four key points (A, B, C and D on the adjacent figure) which are design capacities that form the boundary of failure modes for a section subject to combined bending and axial load. See the toggle blocks below for further information on the failure modes.
If the design forces N* and M* are within the region bound by the interaction curve, then the column is deemed to be safe.
Interaction curve


Four key points on the Interaction Curve

Note the design capacities are calculated using strain compatibility across the section. The maximum (ultimate) strain of concrete, εcu is 0.003 and the strain at yield for class 500N reinforcing bars is 0.0025.

A - Squash Load

The squash load, Nuo, is the point where a column fails in pure compression. The concrete is at ultimate strain of 0.003 and, due to strain compatibility, the steel therefore has exceeded its yield strain and will be at yield strength.


Nuo=Cc+CswhereCc=α1fc(AgAsc)Cs=Cs1+Cs2=fsyAscN_{uo} = C_c + C_s \\ \text{where}\\ C_c = \alpha_1f'_c(A_g-A_{sc}) \\ C_s = C_{s_{1}}+C_{s_{2}} \\ \hspace{0.5cm} = f_{sy}A_{sc}

B - Decompression Point

The decompression point is where a column fails under combined bending and compression while providing no tensile capacity in the section. At this point, the strain in the tension reinforcement is zero and the extreme compressive fibre of the concrete is at its ultimate strain of 0.003. The concrete section in tension is assumed to provide no resistance against tension.


Nu=Cc+CswhereCc=α2fcγkudbCs=εsEsAscN_u = C_c + C_s \\ \text{where}\\ C_c = \alpha_2f'_c \cdot \gamma k_ud \cdot b\\C_s = \varepsilon_sE_sA_{sc}

C - Balanced Failure

The balanced failure point is where a column fails under combined bending and compression by simultaneous crushing of the concrete and yielding of the reinforcement. At this point, the concrete is at ultimate strain, 0.003 and the outer steel strain reaches yield, 0.0025 and hence ku is fixed at 0.545. The balanced failure point represents the maximum bending capacity of a column.


Nu=Cc+CsTswhereCc=α2fcγkudbCs=εs1EsAscTs=fsyAstandku=0.545N_u = C_c + C_s - T_s\\ \text{where}\\ C_c = \alpha_2f'_c \cdot \gamma k_ud \cdot b\\C_s = \varepsilon_{s1}E_sA_{sc}\\T_s = f_{sy}A_{st}\\ \text{and}\\k_u=0.545

D - Pure Bending

The pure bending point is where the column fails in bending without an external axial load. The column capacity is calculated in the same way as a doubly reinforced beam, taking moments about any point.


Mu=Cc(γkud2)+Cs(dsc)Ts(d)whereCc=α2fcγkudbCs=εs1EsAscTs=fsyAstM_u = C_c(\frac{\gamma k_ud}{2})+C_s(d_{sc})-T_s(d)\\\text{where}\\ C_c = \alpha_2f'_c \cdot \gamma k_ud \cdot b\\C_s = \varepsilon_{s1}E_sA_{sc}\\T_s = f_{sy}A_{st}

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