| Project | — | Job No. | — |
| Calculation | Wall Stiffness Modifier | By | — |
| Reference | AS 3600:2018 Clause 6.2.4.2 & Table 6.2.4 | Date | 23 May 2026 |
Wall Stiffness Modifier
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:
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)
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.
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 quantitiesStiffness Modifier
AS 3600 Cl 6.2.4.2Cracking Assessment
AS 3600 Cl 3.1.1.3 & Cl 6.2.4.2| Quantity | Value | Reference |
|---|---|---|
| Wall length, Lw | 3,000 mm | — |
| Wall thickness, tw | 300 mm | — |
| Gross area, Ag = Lw·tw | 900,000 mm² | — |
| Characteristic strength, f'c | 40 MPa | — |
| Direct tensile strength, f'ct = 0.36·√f'c | 2.277 MPa | Cl 3.1.1.3 |
| Applied stress, |S22| | 4.500 MPa | Input (shell) |
| Cracking state | Cracked | Cl 6.2.4.2 |
Table 6.2.4 Lookup & Interpolation
AS 3600 Table 6.2.4 (walls)| Quantity | Value | Reference |
|---|---|---|
| Cracked? (Cl 6.2.4.2) | Yes | Cl 6.2.4.2(b) |
| N* (input) | 2,000 kN | — |
| Axial ratio, N*/(Ag·f'c) raw | 0.0556 | — |
| Axial ratio adopted (clamped ≥ 0) | 0.0556 | — |
| Table 6.2.4 — walls | ||
| N*/(Ag·f'c) ≥ 0.2 | 0.40·Ig | Table 6.2.4 |
| N*/(Ag·f'c) = 0.1 | 0.30·Ig | Table 6.2.4 |
| N*/(Ag·f'c) = 0.0 | 0.25·Ig | Table 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) = 0.2778 | Table 6.2.4 | |
| Stiffness modifier, Ieff/Ig | 0.278 | Table 6.2.4 |