DESIGN

Cracked Section Analysis

Analysis ignoring concrete in tension below NA. Required for serviceability (deflection, crack width) per IS 456 Annex F.

Also calledcracked sectioncracked moment of inertiaieff
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CODES
Definition

Cracked-section analysis (also called cracked-section moment of inertia, Ieff) accounts for the reality that concrete cracks under flexural tension at service load — and the cracked region contributes minimal stiffness to the section. Per IS 456:2000 Annex C, cracked section is used to compute deflection and crack width at serviceability limit state (SLS). The cracked Ieff is significantly less than the gross section moment of inertia Ig (typically 30-60% of Ig for normally-reinforced beams), causing larger deflections than uncracked analysis predicts.

The Bischoff equation (used in IS 456 Annex C and ACI 318) computes Ieff from a transition between Ig (gross uncracked) and Ie (cracked transformed): Ieff = Ig × (Mcr/Ma)³ + Icr × (1 − (Mcr/Ma)³), where Mcr is the cracking moment and Ma is the actual applied moment. For a typical beam at service load with Ma ≈ 1.5 × Mcr: Ieff ≈ 0.3 × Ig + 0.7 × Icr ≈ 50-65% of Ig depending on reinforcement percentage.

Applications: (1) Beam and slab deflection check per IS 456 Cl. 23.2 — using Ieff in standard deflection formulas (e.g., for simply-supported beam with UDL: δ = 5wL⁴/(384EIeff)). (2) Long-term deflection multiplier — short-term elastic × creep multiplier × shrinkage curvature factor. (3) Crack width estimation per IS 456 Cl. 35.3.2. (4) Pre-stressed concrete losses estimation per IS 1343. (5) Building drift check under service loads. The most-overlooked aspect: many designers use gross section moment of inertia (Ig) in deflection calculations, which underestimates deflection by 30-50%. Software (ETABS, SAFE, STAAD) defaults to cracked-section analysis for deflection; users sometimes switch to gross section for 'simpler' analysis without realising the consequence. Always use cracked Ieff for deflection and crack width SLS checks.

Typical values
Ieff / Ig (typical residential beam)0.50-0.65
Ieff / Ig (lightly reinforced 0.5%)0.40-0.55
Ieff / Ig (heavily reinforced 2%)0.65-0.80
Cracking moment Mcr (M25 beam)0.7 × √fck × Z / 1000 kNm
Modular ratio (Fe500 in M25)8.0
Tension reinforcement multiplierPer IS 456 Annex C
Where used
  • Beam and slab deflection check (IS 456 Cl. 23.2)
  • Crack width estimation at service load (IS 456 Cl. 35.3.2)
  • Pre-stress losses calculation (IS 1343 Cl. 18)
  • Long-term deflection projection
  • Tall-building drift analysis under service loads
Acceptance / threshold
Per IS 456 Annex C: Ieff via Bischoff equation accounting for Mcr/Ma; long-term deflection ≤ span/250 (general) or span/350 (sensitive partitions); crack width ≤ 0.3 mm (moderate exposure) or 0.2 mm (water-tank).
Site example
Site reality: a Pune commercial 6 m simply-supported beam was designed for span/depth = 22 (= 273 mm depth). Deflection check used Ig instead of Ieff — predicted deflection 12 mm, actual measured 35 mm at 2 years (creep + shrinkage). Forensic review found Ieff at service load was 0.45 × Ig, doubling the elastic deflection prediction; with creep + shrinkage multiplier, total long-term was 35 mm — confirmed by measurement. Always use cracked-section analysis for deflection; gross section underestimates by 30-50%.
Frequently asked
What is cracked-section analysis?
Cracked-section analysis accounts for concrete cracking under flexural tension at service load — the cracked region contributes minimal stiffness. Cracked Ieff is significantly less than gross Ig (typically 30-65% of Ig). Used for deflection and crack-width estimation at service limit state (SLS). Per IS 456:2000 Annex C.
When should cracked-section moment of inertia be used?
For all serviceability checks: deflection (Cl. 23.2), crack width (Cl. 35.3.2), pre-stress losses, long-term deflection. Use Ieff (cracked) NOT Ig (gross). Software defaults to cracked-section analysis; designers must verify the option is enabled. For ultimate limit state (strength), gross-section analysis is acceptable; for SLS, cracked-section is mandatory.
How is cracked moment of inertia calculated?
Per IS 456 Annex C using Bischoff transition: Ieff = Ig × (Mcr/Ma)³ + Icr × (1 − (Mcr/Ma)³), where Mcr is the cracking moment, Ma is the applied moment, and Icr is the fully cracked transformed moment of inertia. For a typical beam at service load: Mcr/Ma ≈ 0.6-0.8, giving Ieff ≈ 50-65% of Ig. Software (ETABS, SAFE, STAAD) computes automatically; manual calculation per Annex C tables.
Related design terms