Beam Design

Flexural design, flexural capacity, and torsion design for rectangular RC beams.

Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
Compression Reinforcement (optional)
Resistance Factor
ACI 318-25 §21.2.2: φ = 0.90 for tension-controlled sections (εt ≥ 0.005)
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kN·m
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Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
Partial Safety Factors
Recommended: 1.50 (persistent)
Recommended: 1.15
Compression Reinforcement (optional)
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kN·m
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Input Parameters

kN-m · m

Section Geometry

m
m
m
mm
Material Properties
Loading
kN·m
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Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
Resistance Factor
Tension Reinforcement
mm
bars
Compression Reinforcement (optional)
mm
bars
Loading (optional — for D/C)
kN·m
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Enter values and click Calculate.

Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
Partial Safety Factors
Tension Reinforcement
mm
bars
Compression Reinforcement (optional)
mm
bars
Loading (optional — for D/C)
kN·m
📋
Enter values and click Calculate.

Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
Tension Reinforcement
mm
bars
Loading (optional — for D/C)
kN·m
📋
Enter values and click Calculate.

Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
MPa
ACI 318-25: φ = 0.75 for shear/torsion
Design Actions
kN
kN·m
Transverse Reinforcement (Stirrups)
mm
m
Longitudinal Torsion Bars
mm
bars
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Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
Design Actions
kN
kN·m
Transverse Reinforcement (Stirrups)
mm
m
Longitudinal Torsion Bars
mm
bars
ℹ️
Equilibrium vs Compatibility Torsion (EC2 §6.3.1): If this is equilibrium torsion (statically determinate — cannot be redistributed), full design is required. If this is compatibility torsion (statically indeterminate — can be redistributed), EC2 §6.3.1 permits neglecting torsion in ULS design provided cracking is acceptable and minimum reinforcement is provided. Do not neglect equilibrium torsion.
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Input Parameters

kN-m · m

Section Geometry

m
m
m
mm
Material Properties
Design Actions
kN
kN·m
kN·m
Required for equivalent moment Me per IS 456 Cl 41.3
Transverse Reinforcement (Stirrups)
mm
m
Longitudinal Torsion Bars
mm
bars
ℹ️
IS 456:2000 Cl 41 — Equivalent Shear/Moment Method: Combined torsion, bending, and shear are handled by designing for equivalent shear Ve = Vu + 1.6Tu/b and equivalent moments Me1 (bottom), Me2 (top). Stirrups are designed for the equivalent nominal shear stress τve.
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Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
φ = 0.75 (ACI 318-25 §21.2.1). λ = 1.0 NW · 0.85 sand-LW · 0.75 all-LW (§19.2.4).
Longitudinal Steel
mm²
ρw = Asl/(bw·d) · ACI 318-25 §22.5.5.1
Stirrup Layout
mm
m
Applied Load
kN
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Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
MPa
MPa
Recommended: 1.50
Recommended: 1.15
Longitudinal Steel
mm²
ρl = Asl/(bw·d) · EN 1992-1-1 §6.2.2
Stirrup Layout
mm
m
Applied Load
kN
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Input Parameters

kN-m · m

Section Geometry

m
m
m
Material Properties
Longitudinal Steel
mm²
Used to compute pt = 100·Ast/(b·d) for τc (Table 19)
Stirrup Layout
mm
m
Applied Load
kN
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📚 Design Background & Code References

Shear Behaviour of Reinforced Concrete Beams

An uncracked reinforced concrete beam resists shear through a combination of concrete tensile and compressive stresses acting on inclined planes. Once diagonal (inclined) cracks form, the internal force path changes fundamentally — and the beam transitions from beam action to a more complex arch-and-truss mechanism.

Mechanisms of Shear Transfer

  • Compression zone contribution: The uncracked concrete above the neutral axis carries significant shear directly.
  • Aggregate interlock: The rough crack faces interlock and transfer shear across diagonal cracks; this is sensitive to crack width.
  • Dowel action: The longitudinal tension bars crossing a crack resist shear by bending — typically a minor contribution but not negligible.
  • Stirrup contribution: Vertical stirrups cross diagonal cracks and carry the remaining shear demand after the concrete mechanisms are exhausted.

Truss Analogy

The classical design model treats the cracked beam as a parallel-chord truss: the longitudinal steel acts as the tension chord, the concrete compression zone as the compression chord, inclined concrete struts carry compression, and stirrups act as vertical tension members. This model, due to Ritter (1899) and Mörsch (1902), underpins all three codes.

Eurocode 2 extends this to the variable-angle strut model — the strut angle θ is chosen by the designer between 21.8° and 45°, trading a shallower angle (fewer stirrups, more horizontal force in the chord) against a steeper one (more stirrups, less chord force).

Size Effect

Shear capacity per unit area decreases as beam depth increases — a phenomenon not captured by simple √f'c scaling. ACI 318-19 onward addresses this through the size effect factor λs in §22.5.5.1; EC2 captures it via the k = 1 + √(200/d) term in VRd,c.

Design Approach

General Design Requirement
φVn ≥ Vu   (ACI)    VRd ≥ VEd   (EC2)    Vu ≤ Vc + Vus   (IS 456)
All three codes use the same additive model: concrete contribution + stirrup contribution ≥ factored shear demand. When Vu exceeds the concrete capacity alone, stirrups are required to carry the excess. When Vu exceeds the maximum strut capacity, the section must be enlarged.

Why Minimum Stirrups Are Required

Even when the applied shear is below the concrete's capacity (Vu < φVc), all three codes mandate a minimum quantity of shear reinforcement in beams. This is because:

  • Diagonal cracking can occur suddenly; minimum stirrups prevent brittle failure after cracking.
  • Shear demand is often uncertain — construction loads, load redistribution, and dynamic effects can produce higher-than-designed shear.
  • Stirrups also confine the core concrete and hold the main bars in place against dowel splitting.

📚 Design Background & Code References

Flexural Behaviour of Reinforced Concrete Beams

A reinforced concrete beam resists bending through an internal force couple: compression carried by concrete in the compression zone, and tension carried by the steel reinforcement. At the ultimate limit state (ULS), the concrete is assumed to have reached its limiting compressive strain while the tension steel has yielded.

Both ACI 318 and Eurocode 2 are based on the Bernoulli-Euler hypothesis — plane sections remain plane after bending — with full strain compatibility between concrete and steel at every load level.

Three Stages of Beam Behaviour

A reinforced concrete beam passes through three behavioural stages as the applied moment increases from zero to failure:

  1. Uncracked elastic stage: The full concrete section — above and below the neutral axis — resists tension and compression. Both materials behave elastically. This stage ends when the extreme tension fibre stress reaches the modulus of rupture fr ≈ 0.62√f'c (ACI, MPa units). The corresponding moment is the cracking moment Mcr.
  2. Cracked elastic stage: Flexural cracks form at the tension face. Below the neutral axis, only the transformed steel area resists tension. Above the neutral axis, concrete carries compression elastically. This regime governs serviceability limit states — deflection and crack width checks.
  3. Ultimate limit state (ULS): The extreme compression fibre concrete reaches its crushing strain εcu. In a properly designed under-reinforced section, the tension steel has already yielded (εs ≫ εy), providing large deflections and visible cracking as warning before failure. This is the regime that controls strength design.

Whitney Equivalent Rectangular Stress Block

The actual parabolic-rectangular concrete stress distribution in the compression zone is replaced by an idealised rectangular stress block for calculation convenience. The block is calibrated so that its resultant force Cc equals that of the real distribution, and acts at the same centroid location.

ACI 318-25 Rectangular Block — §22.2.2
Block depth:   a = β₁ · c
Block stress:   0.85 f'c
Compression resultant:   Cc = 0.85 f'c · a · b
Tension resultant:   T = As · fy (at yield)
Moment capacity:   φMn = φ · As · fy · (d − a/2)
β₁ accounts for the shape of the actual distribution; it equals 0.85 for f'c ≤ 28 MPa and decreases linearly to a minimum of 0.65 for higher-strength concrete. EC2 uses λ = 0.8 and η = 1.0 for fck ≤ 50 MPa with analogous meaning.

Balanced Reinforcement Ratio ρbal

The balanced failure condition occurs when the extreme concrete fibre reaches εcu at the same instant that the outermost tension steel reaches its yield strain εy = fy/Es. At balanced failure, both concrete crushing and steel yielding occur simultaneously — a brittle failure with no ductile warning. All codes prohibit design at or above the balanced steel ratio.

Balanced Steel Ratio — ACI (SI)
ρbal = (0.85 β₁ f'c / fy) · [εcu / (εcu + εy)]
εcu = 0.003 ·   εy = fy / 200 000 (fy in MPa)
Example (f'c = 28 MPa, fy = 420 MPa): ρbal ≈ 0.0285
EC2 expresses the equivalent limit as x/d ≤ 0.45; IS 456 tabulates xu,max/d by steel grade. All three restrict the section to the under-reinforced side of balanced failure.

Ductility and the Tension-Controlled Requirement

Codes mandate ductile, under-reinforced failure to ensure large deflections and wide cracks occur before collapse — giving occupants warning and allowing load redistribution in indeterminate structures.

CodeDuctility RequirementImplication
ACI 318-25Net tensile strain εt ≥ 0.004 at ULS (φ = 0.90 when εt ≥ 0.005)ρ ≤ ≈ 0.75 ρbal
Eurocode 2Neutral axis x/d ≤ 0.45 (for δ ≥ 0.7 redistribution)K ≤ K' = 0.167
IS 456:2000xu/d ≤ xu,max/d (by grade: Fe 415 → 0.48)Mu ≤ Mu,lim

Key Assumptions at ULS

  • Tensile strength of concrete is neglected — only steel resists tension.
  • Concrete reaches its limiting compressive strain: εcu = 0.003 (ACI) or 0.0035 (EC2 for fck ≤ 50 MPa).
  • Stress distribution idealised as a rectangular (Whitney) stress block.
  • Steel has yielded: σs = fy (ACI) or fyd = fyks (EC2).
  • Section is singly-reinforced — compression steel neglected.

Effective Depth

Effective Depth
d = h − cclear − dbar/2
h = total depth · c = clear cover to main bar face · dbar = main bar diameter (assumed 20 mm / 0.75 in). Stirrup thickness is conservatively included in the clear cover input.
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