StrucLab
LabKitModelling & AnalysisWall Stiffness Modifier

Wall Stiffness Modifier

AS 3600:2018 Cl 6.2.4.2 · Cracked-section Ieff for wall elements · ULS elastic analysis

Method & Equations

AS 3600:2018 Cl 6.2.4.2 specifies the moment of inertia to use for walls in elastic analysis of lateral force-resisting systems at the ultimate limit state. The clause distinguishes between uncracked and cracked behaviour:

  • Cl 6.2.4.2(a) — Uncracked sections: use the full gross uncracked section (Ieff = Ig, i.e. modifier = 1.0).
  • Cl 6.2.4.2(b) — Cracked sections: apply the modifier from Table 6.2.4, which varies with the axial load ratio N*/(Ag·f'c).
Cracking criterion — Cl 3.1.1.3

A wall is taken as cracked when the peak in-plane tensile membrane stress S22 (from elastic shell analysis) reaches the characteristic uniaxial tensile strength of concrete:

$$f'_{ct} = 0.36 \sqrt{f'_c}$$

Direct (uniaxial) tensile strength is used rather than flexural f'ct.f = 0.6·√f'c because S22 from a shell element represents a membrane stress with no strain gradient through the wall thickness. The flexural value would non-conservatively delay the cracked classification.

Table 6.2.4 — wall modifiers (cracked)
$$\begin{array}{ll} N^*/(A_g f'_c) \geq 0.2 : & I_{\text{eff}} = 0.40\, I_g \\ N^*/(A_g f'_c) = 0.1 : & I_{\text{eff}} = 0.30\, I_g \\ N^*/(A_g f'_c) = 0.0 : & I_{\text{eff}} = 0.25\, I_g \end{array}$$

For intermediate values of the axial ratio, linear interpolation is permitted (Table 6.2.4 footnote). Net tension (N* < 0) is outside the table's range and is conservatively clamped at the ratio = 0 row (Ieff = 0.25·Ig); engineers expecting significant net tension in a wall should consider a separate detailed assessment.

0.00.10.2≥0.2N* / (Ag · f'c)0.250.300.401.00Ieff / IgUncracked: Ieff = 1.0·Ig — Cl 6.2.4.2(a)Cracked — Table 6.2.4
Limitations & Assumptions
  • For ULS elastic analysis only (lateral force distribution, period, inter-storey drift). Serviceability deflection of slabs/beams uses Cl 8.5/9.5 Branson-based Ief — a different method not implemented here.
  • S22 is taken as the peak in-plane membrane stress from shell-element output. The engineer must judge where to extract S22 (panel average vs. edge peak vs. specific load combo) — the tool does not extract this automatically.
  • Cracking criterion uses direct tensile strength f'ct per Cl 3.1.1.3, on the basis that S22 from a shell is a membrane stress.
  • Net tension (N* < 0) is clamped to ratio = 0; this is outside the explicit range of Table 6.2.4 and engineers should consider whether a more detailed assessment is warranted.
  • Does not address shear-stiffness modifiers, P-delta amplification, or non-linear cracked behaviour — refer to AS 3600 Section 6 and seismic guidance (e.g. AS 1170.4) for those effects.
  • Single wall element only. Coupled walls, walls with openings, and walls connected to slabs above/below may require separate consideration of effective stiffness at the connection.

Analysis Parameters

Derived quantities
Ag
900,000 mm²
Lw × tw
f'ct (direct tension)
2.277 MPa
0.36·√f'c · Cl 3.1.1.3
Axial ratio N*/(Ag·f'c)
0.0556
Within table range
Ieff (absolute)
1.875×10^11 mm⁴
modifier × Ig

Stiffness Modifier

AS 3600 Cl 6.2.4.2
Ieff / Ig — stiffness modifier
0.278
Cracked · Reduced
Linear interpolation per Table 6.2.4Cl 6.2.4.2(b)

Cracking Assessment

AS 3600 Cl 3.1.1.3 & Cl 6.2.4.2
QuantityValueReference
Wall length, Lw3,000 mm
Wall thickness, tw300 mm
Gross area, Ag = Lw·tw900,000 mm²
Characteristic strength, f'c40 MPa
Direct tensile strength, f'ct = 0.36·√f'c2.277 MPaCl 3.1.1.3
Applied stress, |S22|4.500 MPaInput (shell)
Cracking stateCrackedCl 6.2.4.2

Table 6.2.4 Lookup & Interpolation

AS 3600 Table 6.2.4 (walls)
QuantityValueReference
Cracked? (Cl 6.2.4.2)YesCl 6.2.4.2(b)
N* (input)2,000 kN
Axial ratio, N*/(Ag·f'c) raw0.0556
Axial ratio adopted (clamped ≥ 0)0.0556
Table 6.2.4 — walls
N*/(Ag·f'c) ≥ 0.20.40·IgTable 6.2.4
N*/(Ag·f'c) = 0.10.30·IgTable 6.2.4
N*/(Ag·f'c) = 0.00.25·IgTable 6.2.4
Interpolation
Interpolate between (0.0, 0.25) and (0.1, 0.30): Ieff/Ig = 0.25 + (0.0556 − 0)/0.1 · (0.30 − 0.25) = 0.2778Table 6.2.4
Stiffness modifier, Ieff/Ig0.278Table 6.2.4