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Limit State Method — Principles, Loads & Partial Safety Factors

Limit state philosophy, limit states of collapse and serviceability, characteristic loads and strengths, partial safety factors for loads and materials (IS 456 Table 18), design loads, assumptions for flexure, the stress block, limiting depth of neutral axis and balanced, under- and over-reinforced sections — with solved numericals.

📑 Contents (10 sections)

Last reviewed 16 Sept 2026 · 6 min read

What a limit state is

A limit state is a condition beyond which a structure (or part of it) no longer fulfils its design purpose. Limit state design makes the structure safe against all relevant limit states with an acceptable probability, instead of only keeping elastic stresses below permissible values (as working stress design does).

Group Limit states
Limit state of collapse (strength, safety) Flexure, compression, shear, torsion, bond; overall stability (overturning, sliding); buckling
Limit state of serviceability (fitness for use) Deflection, cracking, vibration, durability, fire resistance

The structure is designed for the collapse limit states and checked for serviceability.

Characteristic values

  • Characteristic strength of a material — the value below which not more than 5% of test results are expected to fall ( for concrete, for steel).
  • Characteristic load — the load that has only a 95% probability of not being exceeded during the life of the structure. In practice, loads from IS 875 (dead, imposed, wind) and IS 1893 (earthquake) are used as characteristic loads.

Partial safety factors

For materials ()

Material Limit state of collapse Limit state of serviceability
Concrete 1.5 1.0
Steel 1.15 1.0

Concrete gets the larger factor because its strength is more variable (site mixing, compaction, curing).

For loads ()

Code ProvisionIS 456 Table 18 — partial safety factors for loads
Load combination Collapse: DL Collapse: IL Collapse: WL/EL Serviceability: DL Serviceability: IL Serviceability: WL/EL
DL + IL 1.5 1.5 — 1.0 1.0 —
DL + WL (or EL) 1.5 or 0.9* — 1.5 1.0 — 1.0
DL + IL + WL (or EL) 1.2 1.2 1.2 1.0 0.8 0.8

*0.9 is used for dead load where it helps stability (overturning, uplift, stress reversal).

Assumptions for flexure (limit state of collapse)

  1. Plane sections remain plane — strain varies linearly with depth.
  2. Maximum strain in concrete at the outermost compression fibre is 0.0035 in bending.
  3. The design stress–strain curve of concrete is parabolic–rectangular, with maximum design stress .
  4. Tensile strength of concrete is ignored.
  5. Stresses in reinforcement follow the design stress–strain curve of steel, with = 1.15 (design yield ).
  6. The maximum strain in the tension steel at failure must not be less than (that is, ), so that steel yields before concrete crushes (ductile failure).

The stress block

Integrating the parabolic–rectangular stress diagram over the compression depth of a rectangular section of width :

FormulaCompressive force and its position

Tension: (when steel yields).

Lever arm ; moment of resistance .

Where the numbers come from: the average stress of the block is , and its centroid lies at .

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