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)
Loading
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)
Loading
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

SI · kN-m · m

Section Geometry

m
m
m
mm
Material Properties
Loading
kN·m
📋
Enter values — results update automatically.

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
📋
Enter values — results update automatically.

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 — results update automatically.

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 — results update automatically.

Input Parameters

SI · kN-m · m

Section Geometry

m
m
m
Material Properties
Tension Reinforcement
mm
bars
Loading (optional D/C check)
kN·m
📋
Enter values — results update automatically.

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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Enter values — results update automatically.

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

SI · kN-m · m

Section Geometry

m
m
m
mm
Material Properties
Design Actions
kN
kN·m
Stirrups (closed, 2-leg)
mm
m
Longitudinal Torsion Bars
mm
bars
ℹ️
TS 500:2000 §9 — Thin-Wall Space Truss: Equivalent thin-wall tube analogy (tef, Ak). Stirrups resist torsion shear flow; longitudinal bars balance the diagonal force. Section adequacy: Vd/(b·d) + Td/(2·Ak·tef) ≤ 0.22·fcd.
📋
Enter values — results update automatically.

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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Enter values — results update automatically.

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
📊
Enter values — results update automatically.

📚 Design Background & Code References

Theory↑ Top

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.
ACI 318-25↑ Top

ACI 318-25 §22.5 Shear Strength

The nominal shear strength of a section is Vn = Vc + Vs. The design requirement is φVn ≥ Vu, where φ = 0.75 for shear.

Concrete Contribution — §22.5.5.1 (SI)
Vc = 0.66 λ ρw1/3 f'c1/3 · bw · d   [N, MPa, mm]
ρw = Asl / (bw · d)   (longitudinal tension reinforcement ratio)
Stirrup Contribution — §22.5.8.5
Vs = Av · fyt · d / s   (vertical stirrups)
Vs,max = 0.66 √f'c · bw · d   (§22.5.1.2 — if exceeded, increase section)
Maximum Spacing — §9.7.6.2.2
If Vs ≤ 0.33√f'c · bw · d:   smax = min(d/2, 600 mm)
If Vs > 0.33√f'c · bw · d:   smax = min(d/4, 300 mm)
Minimum Shear Reinforcement — §26.6.3.1
Av/s ≥ max(0.062√f'c · bw/fyt,   0.35 · bw/fyt)
Eurocode 2↑ Top

EN 1992-1-1 §6.2 Shear Resistance

Members without shear reinforcement rely on concrete tensile resistance (VRd,c). When VEd > VRd,c, vertical stirrups must carry the full design shear via the variable strut inclination method.

Concrete Resistance — §6.2.2
VRd,c = [CRd,c · k · (100ρlfck)1/3] · bw · d
CRd,c = 0.18/γc  ·   k = 1 + √(200/d) ≤ 2.0  ·   ρl = Asl/(bw·d) ≤ 0.02
VRd,c,min = 0.035 · k3/2 · √fck · bw · d
Stirrup Resistance — §6.2.3 (θ = 45°)
VRd,s = (Asw/s) · z · fywd   z = 0.9d, fywd = fywk/γs
VRd,max = 0.5 · bw · z · ν · fcd   (ν = 0.6(1−fck/250), fcd = fck/γc)
Maximum Spacing — §9.2.2
sl,max = 0.75 · d   (vertical stirrups, θ = 45°)
ρw,min = 0.08 √fck / fywk
IS 456:2000↑ Top

IS 456:2000 Cl. 40 Shear Design

The nominal shear stress τv is checked against the design shear strength τc (Table 19) and maximum shear stress τc,max (Table 20). Stirrups carry the shear in excess of τc.

Nominal Shear Stress — Cl. 40.1
τv = Vu / (b · d)   [N/mm²]
Design Shear Strength — Table 19
τc depends on pt = 100·Ast/(b·d) and fck
τc,max from Table 20: M20 → 2.8, M25 → 3.1, M30 → 3.5, M35 → 3.7, M40+ → 4.0 N/mm²
Stirrup Contribution — Cl. 40.4
Vus = 0.87·fy·Asv·d / sv
Required Asv/sv = (Vu − τc·b·d) / (0.87·fy·d)
Minimum Shear Reinforcement — Cl. 26.5.1.6
Asv / (b·sv) ≥ 0.4 / (0.87·fy)
Max spacing: sv,max = min(0.75d, 300 mm) — Cl. 26.5.1.5
TS 500:2000↑ Top

TS 500:2000 §8.1 Shear Capacity

TS 500 adopts the same additive model as EC2 and IS 456: the design shear resistance Vr is the sum of the concrete contribution Vcr and the stirrup contribution Vw. Axial compression enhances Vcr.

Design shear resistance — §8.1.1
Vr = Vcr + Vw ≥ Vd
Vcr = 0.65 · fctd · bw · d
fctd = fctk/γc;   fctk = 0.35√fck (TS 500 Table 2.3);   γc = 1.5  →   fctd ≈ 0.233√fck
Stirrup contribution — §8.3.2
Vw = (Asv/sv) · fywd · d
Vr,max = 0.22 · fcd · bw · d   (§8.1.3 — compression strut limit)
Minimum stirrups — §8.2.3 & §8.2.5
Asv,min/(bw·sv) ≥ 0.3 · fctd/fywd
sv,max = min(d/2, 300 mm)
Worked Example↑ Top

Example — ACI 318-25 Shear Design (Rectangular Beam)

Given: Rectangular beam, b = 300 mm, h = 550 mm, effective depth d = 500 mm. Concrete f'c = 28 MPa, fyt = 420 MPa. Longitudinal tension steel: As = 1,520 mm² (4Ø22 from flexural design). Factored shear: Vu = 180 kN. Normal-weight concrete, λ = 1.0.

  1. Longitudinal reinforcement ratio
    ρw = As/(bw·d) = 1,520/(300×500) = 0.01013
  2. Concrete shear resistance — §22.5.5.1
    Vc = 0.66·λ·ρw1/3·f'c1/3·bw·d
    = 0.66 × 1.0 × 0.010131/3 × 281/3 × 300 × 500
    = 0.66 × 0.2163 × 3.037 × 150,000 = 65,100 N = 65.1 kN
    φVc = 0.75 × 65.1 = 48.8 kN
  3. Shear reinforcement required?
    Vu = 180 kN > φVc = 48.8 kN → Stirrups required
  4. Required stirrup contribution
    φVs,req = Vu − φVc = 180 − 48.8 = 131.2 kN
    Vs,req = 131.2/0.75 = 174.9 kN
  5. Section adequacy check — §22.5.1.2
    Vs,max = 0.66√f'c·bw·d = 0.66×5.292×150,000 = 523,900 N = 523.9 kN
    Vs,req = 174.9 kN << Vs,max → Section is adequate ✓
  6. Select stirrup size and spacing
    Try Ø10 closed stirrups, 2 legs: Av = 2×78.5 = 157 mm²
    sreq = Av·fyt·d / Vs,req = 157×420×500/174,900 = 188 mm
  7. Maximum spacing limit — §9.7.6.2.2
    Vs,req = 174.9 kN ≤ 0.33√f'c·bw·d = 0.33×5.292×150,000/1000 = 261.8 kN
    → smax = min(d/2, 600) = min(250, 600) = 250 mm
  8. Minimum shear reinforcement — §26.6.3.1
    Av/s ≥ max(0.062√28×300/420, 0.35×300/420) = max(0.234, 0.250) = 0.250 mm²/mm
    Use s = 175 mm: Av,prov/s = 157/175 = 0.897 mm²/mm > 0.250 ✓
Result: Ø10 @ 175 mm (2 legs, Av = 157 mm²/set).
Vs,prov = 157×420×500/175 = 188,400 N = 188.4 kN
φVn = 0.75×(65.1 + 188.4) = 190.1 kN ≥ Vu = 180 kN ✓
References↑ Top

References

  • [1]
    ACI 318-25 — Building Code Requirements for Structural Concrete. American Concrete Institute, 2025. §22.5 (Shear strength), §9.7.6.2 (Maximum stirrup spacing), §26.6.3 (Minimum shear reinforcement).
  • [2]
    EN 1992-1-1:2004 — Eurocode 2: Design of Concrete Structures. CEN, Brussels. §6.2 (Shear), §9.2.2 (Shear reinforcement in beams). Variable-angle strut inclination method.
  • [3]
    IS 456:2000 — Plain and Reinforced Concrete — Code of Practice, 4th Rev. Bureau of Indian Standards. Cl. 40 (Shear), Table 19 (Design shear strength τc), Table 20 (Maximum τc,max), Cl. 26.5.1 (Stirrup spacing limits).
  • [4]
    Ritter, W. — Die Bauweise Hennebique. Schweizerische Bauzeitung, Vol. 33, 1899. (Original truss analogy model for shear in RC beams.)
  • [5]
    Collins, M.P. & Mitchell, D. — Prestressed Concrete Structures. Prentice-Hall, 1991. Chapter 7 (Compression Field Theory — basis of EC2 variable-angle truss method).
  • [6]
    Wight, J.K. & MacGregor, J.G. — Reinforced Concrete: Mechanics and Design, 7th Ed. Pearson, 2016. Chapter 6 (Shear in Beams).
  • [7]
    Kani, G.N.J. — The Riddle of Shear Failure and Its Solution. ACI Journal, Vol. 61, No. 4, 1964. (Landmark study on size effect and shear span ratio influence.)
  • [8]
    TS 500:2000 — Requirements for Design and Construction of Reinforced Concrete Structures. Turkish Standards Institution, Ankara. §8.1 (Shear resistance), §8.2.3 (Minimum stirrup), §8.2.5 (Maximum stirrup spacing), §8.3.2 (Stirrup contribution).
Disclaimer: For educational and preliminary design only. Verify all results with a licensed structural engineer.

Input Parameters

SI · kN-m · m

Section Geometry

m
m
m
Material Properties
Stirrup Layout
mm
m
Applied Load
kN
📊
Enter values — results update automatically.

📚 Design Background & Code References

Theory↑ Top

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 = fyk/γs (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.
ACI 318-25↑ Top

ACI 318-25 Strength Design Method

ACI 318-25 uses Load and Resistance Factor Design (LRFD). The design requirement is φMn ≥ Mu, where φ is the strength reduction factor and Mn is the nominal moment capacity.

Strength Reduction Factor φ — ACI 318-25 Table 21.2.2
φ = 0.90    tension-controlled (εt ≥ 0.005)
φ = 0.65 → 0.90    transition zone (0.002 < εt < 0.005)
φ = 0.65    compression-controlled (εt ≤ 0.002)
For beams under pure flexure, φ = 0.90 applies when ρ ≤ 0.75ρbal.

ACI 318-25 §22.2 Stress Block & Reinforcement

Stress Block Factor β₁
β₁ = 0.85   (f'c ≤ 28 MPa)    β₁ ≥ 0.65 (minimum)
β₁ = 0.85 − 0.05·(f'c − 28)/7   (f'c > 28 MPa)
Required Steel Area
Rn = Mu/(φ·b·d²)
ρ = (0.85f'c/fy)·[1−√(1−2Rn/0.85f'c)]
As = ρ·b·d

ACI 318-25 §9.6.1.2 Minimum & Maximum Reinforcement

Reinforcement Limits
ρmin = max(0.25√f'c/fy , 1.4/fy)   [MPa]
ρmax = 0.75·ρbal   (ensures εt ≥ 0.005)

ACI 318-25 Material Limits

ParameterMinimumMaximumReference
Concrete f'c17 MPa (2500 psi)70 MPa (10000 psi)*§19.2.1
Rebar fy280 MPa (40 ksi)550 MPa (80 ksi)§20.2.2
Strength factor φ0.650.90Table 21.2.2

* Higher f'c permitted with special provisions per §19.2.1.3

ACI 318-25 §25.2 Minimum Bar Spacing

Clear Spacing Between Bars — §25.2.1
sclear ≥ max(db, 25 mm, 4/3 · aggregate size)
For bars in multiple layers: vertical clear spacing ≥ 25 mm
Adequate clear spacing allows concrete to flow around bars during placement and consolidation. Insufficient spacing leads to honeycombing and reduced bond strength.

ACI 318-25 §24.3 Crack Control — Maximum Bar Spacing

Even when flexural strength is adequate, bar spacing in the tension zone is limited to control crack widths under service loads. Wider crack widths accelerate corrosion and are visually alarming to occupants.

Maximum Spacing in Tension Zone — §24.3.2
s ≤ 380 · (280/fs) − 2.5·cc   [mm]
s ≤ 300 · (280/fs)   (interior exposure limit)
fs = 2/3 · fy   (approximate service bar stress, MPa)
cc = clear cover to flexural tension reinforcement
For fy = 420 MPa with cc = 40 mm: smax ≈ 213 mm. This is often the governing spacing limit in slabs and wide beams.

ACI 318-25 §22.2 Design Summary

The complete ACI flexural design procedure for a singly reinforced rectangular section:

  1. Compute Rn = Mu / (φ · b · d²)
  2. Solve ρ = (0.85f'c / fy) · [1 − √(1 − 2Rn / 0.85f'c)]
  3. Check ρmin ≤ ρ ≤ ρmax (= 0.75 ρbal)
  4. As = ρ · b · d
  5. Check εt ≥ 0.004; confirm φ = 0.90
  6. Verify bar spacing ≥ sclear,min and ≤ scrack,max
Eurocode 2↑ Top

EN 1992-1-1 Partial Factor Method

Eurocode 2 uses a partial factor method rather than a single capacity reduction factor φ. Safety is achieved by factoring the material strengths directly, rather than the resulting capacity. This produces design strengths fcd and fyd that are used throughout all capacity calculations.

Design Material Strengths
fcd = αcc·fck/γc    [αcc=1.0 recommended; γc=1.5]
fyd = fyk/γs              [γs=1.15]
γc and γs are Nationally Defined Parameters (NDPs) and may be modified by National Annexes. The recommended values are γc = 1.5 (persistent/transient) and γs = 1.15. For accidental design situations both reduce to 1.0.

EN 1992-1-1 §6.1 Flexural Design

Design Procedure — Lever Arm Method
K = MEd/(b·d²·fcd)
K' = 0.167   [limiting K for δ=1.0, no redistribution]
z = d·[0.5+√(0.25−K/1.134)] ≤ 0.95d   (lever arm)
As = MEd/(fyd·z)

If K > K': compression steel required or section must be enlarged
The factor 1.134 = 2·0.567 where 0.567 = λ·η/(2) = 0.8·1.0/2·(1/0.8) — derived from the rectangular stress block parameters for fck ≤ 50 MPa. The lever arm formula is equivalent to solving the force equilibrium and moment equations directly.

EN 1992-1-1 §9.2.1.1 Minimum Reinforcement

Minimum As (§9.2.1.1)
As,min = max(0.26·fctm/fyk, 0.0013) · b·d
fctm = 0.30·fck2/3   (fck ≤ 50 MPa)
Example (C25/30, fyk=500): fctm=2.56 MPa → ρmin=0.0013
Minimum reinforcement ensures the section does not fail immediately upon cracking. The formula links the minimum steel to the tensile capacity of the concrete, ensuring the steel can carry the tension released at cracking without yielding immediately. At minimum steel, the cracking moment Mcr ≈ Mn.

EN 1992-1-1 Table 7.4N Span-to-Depth Ratios (Deflection)

EC2 allows deflection to be checked implicitly by limiting the span-to-effective-depth ratio l/d rather than computing deflections explicitly. The limiting ratios are:

SystemLightly loaded (ρ = 0.5%)Normally loaded (ρ = 1.5%)
Simply supported beam/slab2014
End span of continuous2618
Interior span of continuous3020
Cantilever86

Values from EC2 Table 7.4N for simply supported beams with fyk = 500 MPa. Multiply by 0.8 for flanged beams (beff/bw > 3) and by 1.5 for flat slabs.

EN 1992-1-1 Material Limits

ParameterMinimumMaximumReference
Concrete fck12 MPa (C12/15)90 MPa (C90/105)Table 3.1
Rebar fyk400 MPa600 MPa§3.2.2
Partial factor γc1.0 (accidental)1.5 (persistent)Table 2.1N
Partial factor γs1.0 (accidental)1.15 (persistent)Table 2.1N
IS 456:2000↑ Top

IS 456:2000 Code Overview

IS 456:2000 is the Indian Standard for Plain and Reinforced Concrete — Code of Practice. It covers the design of concrete structures for flexure, shear, torsion, and serviceability. Limit state design (Cl. 18) is the primary design method, targeting both the Limit State of Collapse and the Limit State of Serviceability.

IS 456 Cl. 38 Flexural Design (Limit State)

The limiting neutral axis depth ratio xu,lim/d depends on the steel grade (Fe 250 → 0.53, Fe 415 → 0.48, Fe 500 → 0.46, Fe 550 → 0.44). The design moment capacity is:

Singly Reinforced Beam — Cl. 38.1
Mu = 0.87 fy Ast d [1 − (Ast fy) / (b d fck)]
Mu,lim = 0.36 fck b xu,lim (d − 0.42 xu,lim)
Minimum / Maximum Steel — Cl. 26.5.1.1
Ast,min = 0.85 b d / fy
Ast,max = 0.04 b D   (D = total depth)

IS 456 Cl. 40 Shear Design

Nominal shear stress τv = Vu/(b·d) is compared with design shear strength τc (Table 19, function of pt and fck) and maximum τc,max (Table 20). Vertical stirrups carry excess shear.

Stirrup Capacity — Cl. 40.4 (b)
Vus = 0.87 fy Asv d / sv
sv,max = min(0.75d, 300 mm) — Cl. 26.5.1.5

IS 456 Cl. 41 Torsion Design

IS 456 converts torsion to equivalent shear (Ve) and equivalent bending moment (Mt) using the equivalent moment method. Both are checked against the section capacity.

Equivalent Shear — Cl. 41.3.1
Ve = Vu + 1.6 Tu / b
τve = Ve / (b · d) ≤ τc,max
Equivalent Moment — Cl. 41.4.2
Mt = Tu (1 + D/b) / 1.7
Design for Mu1 = Mu + Mt (tension side) and Mu2 = Mt − Mu (if positive, compression side)

IS 456 Table 2 Concrete Grades

Standard grades: M15, M20, M25, M30, M35, M40, M45, M50, M55. The number denotes the characteristic compressive strength fck (cylinder) in MPa at 28 days. M25 (25 MPa) is the minimum grade for reinforced concrete in moderate exposure.

IS 456 Table 1 Steel Grades

Fe 250 (mild steel, fy = 250 MPa), Fe 415 (HYSD, most common), Fe 500, Fe 550. Design yield stress = 0.87 fy in the limit state method.

TS 500:2000↑ Top

TS 500:2000 §7 Flexural Design

TS 500 uses the equivalent rectangular stress block — the same conceptual model as ACI 318 — but applies Turkish material factors (γc = 1.5, γs = 1.15) and its own ductility limit for the neutral axis depth.

Equivalent rectangular stress block — §7.4
a = Ast·fyd / (0.85·fcd·b)
Mrd = Ast·fyd·(d − a/2)
fcd = fck/γc = fck/1.5  ·  fyd = fyk/γs = fyk/1.15
Ductility limit — §7.5.4
xu/d ≤ 0.45   (for fyk ≤ 500 MPa)
Ensures yielding of tension steel before concrete crushing — the fundamental ductility requirement for RC beams under TS 500.
Minimum / Maximum reinforcement — §7.1.2 & §7.1.3
Ast,min = max(0.8·fctd·b·d/fyd,   0.002·b·d)
Ast,max = 0.04·b·h

TS 500:2000 §3.3 Material Factors

PropertyExpressionNote
Concrete design strength fcdfck/1.5§3.3.1
Tensile strength fctk0.35·√fckTable 2.3
Design tensile strength fctdfctk/1.5§3.3.1
Steel design yield fydfyk/1.15§3.3.2
Partial factor for concrete γc1.5—
Partial factor for steel γs1.15—
Limits & Comparison↑ Top

Design Limits Comparison — ACI 318-25 vs. Eurocode 2 vs. IS 456:2000

ParameterACI 318-25Eurocode 2IS 456:2000
Concrete strain at ULSεcu = 0.003εcu = 0.0035εcu = 0.0035
Resistance / partial factorφ = 0.90 (flexure)γc=1.5 · γs=1.15γc=1.5 · γs=1.15 (implicit)
Stress block depth factorβ₁ = 0.85 → 0.65λ = 0.8 (fck ≤ 50 MPa)0.36·fck·b·xu (parabolic-rect.)
Stress block intensity0.85·f'cη·fcd, η=1.00.36·fck (equiv. rect. block)
Minimum reinforcementmax(0.25√f'c/fy, 1.4/fy)·b·dmax(0.26fctm/fyk, 0.0013)·b·d0.85·b·d / fy (Cl. 26.5.1.1a)
Maximum reinforcementρ ≤ 0.75·ρbalK ≤ K' = 0.1670.04·b·D (Cl. 26.5.1.1b)
Neutral axis limit (xu/d)Not directly (εt ≥ 0.004)x/d ≤ 0.45Fe415: 0.48 · Fe500: 0.46 · Fe250: 0.53
Maximum lever armNot explicitly limitedz ≤ 0.95dNot explicitly limited
Worked Example↑ Top

Example — ACI 318-25 Flexural Design (Singly Reinforced Rectangular Beam)

Given: Rectangular section, b = 300 mm, h = 550 mm, effective depth d = 500 mm (cover = 40 mm + Ø10 stirrup + Ø22/2). Concrete f'c = 28 MPa, steel fy = 420 MPa. Factored moment: Mu = 250 kN·m.

  1. Stress block factor β₁ — §22.2.2.4.3
    f'c = 28 MPa → β₁ = 0.85 (no reduction needed; limit applies for f'c > 28 MPa)
  2. Design resistance coefficient Rn
    Rn = Mu/(φ·b·d²) = 250×106/(0.90×300×500²) = 3.704 MPa
  3. Required reinforcement ratio ρ
    ρ = (0.85f'c/fy)·[1−√(1−2Rn/(0.85f'c))]
    = (0.85×28/420)·[1−√(1−2×3.704/23.80)]
    = 0.05667·[1−√0.6888] = 0.05667×0.1700 = 0.00963
  4. Reinforcement limits — §9.6.1.2
    ρmin = max(0.25√28/420, 1.4/420) = max(0.00315, 0.00333) = 0.00333
    ρbal = (0.85×0.85×28/420)·(0.003/0.00510) = 0.04817×0.5882 = 0.02833
    ρmax = 0.75×0.02833 = 0.02125
    0.00333 ≤ ρ = 0.00963 ≤ 0.02125 ✓
  5. Required steel area and bar selection
    As,req = ρ·b·d = 0.00963×300×500 = 1,445 mm²
    Select: 4Ø22 → As,prov = 4×380 = 1,520 mm²
  6. Tension-controlled check — confirm φ = 0.90
    a = As·fy/(0.85·f'c·b) = 1,520×420/(0.85×28×300) = 89.4 mm
    c = a/β₁ = 89.4/0.85 = 105.2 mm
    εt = (d/c − 1)·εcu = (500/105.2 − 1)×0.003 = 0.01126 ≫ 0.005
    → Tension-controlled failure ✓ → φ = 0.90 applies
  7. Moment capacity verification
    φMn = φ·As·fy·(d − a/2)
    = 0.90×1,520×420×(500 − 44.7)/106 = 261.5 kN·m ≥ Mu = 250 kN·m ✓
Result: Use 4Ø22 (As = 1,520 mm²) in a single layer. The section is tension-controlled (εt = 0.0113 ≫ 0.005), confirming ductile failure with large post-yield deformations before collapse. φMn = 261.5 kN·m ≥ Mu = 250 kN·m ✓
References↑ Top

References

  • [1]
    ACI 318-25 — Building Code Requirements for Structural Concrete and Commentary. American Concrete Institute, 2025. §9.6, §21.2.2, §22.2.
  • [2]
    EN 1992-1-1:2004 — Eurocode 2: Design of Concrete Structures. CEN, Brussels. §6.1, §9.2.1.
  • [3]
    IS 456:2000 — Plain and Reinforced Concrete — Code of Practice, 4th Rev. Bureau of Indian Standards (BIS), New Delhi. Cl. 38 (Flexure), Cl. 40 (Shear), Cl. 41 (Torsion).
  • [4]
    MacGregor, J.G. & Wight, J.K. — Reinforced Concrete: Mechanics and Design, 7th Ed. Pearson, 2016.
  • [5]
    Mosley, Bungey & Hulse — Reinforced Concrete Design to Eurocode 2, 7th Ed. Palgrave Macmillan, 2012.
  • [6]
    Whitney, C.S. — Plastic Theory of Reinforced Concrete Design. Trans. ASCE, Vol. 107, 1942.
  • [7]
    Pillai, S.U. & Menon, D. — Reinforced Concrete Design, 3rd Ed. Tata McGraw-Hill, 2009. (IS 456-based reference text)
  • [8]
    TS 500:2000 — Requirements for Design and Construction of Reinforced Concrete Structures. Turkish Standards Institution, Ankara. §7 (Flexure, bond, and reinforcement detailing), §7.1.2 (Ast,min), §7.1.3 (Ast,max), §7.4 (Stress block), §7.5.4 (xu/d ≤ 0.45 ductility limit).
Disclaimer: For educational and preliminary design only. All results must be verified by a licensed structural engineer. Always refer to the current edition of the applicable code.

📚 Design Background & Code References — Torsion

Theory↑ Top

Nature of Torsion in Reinforced Concrete

Torsion arises when an applied load acts eccentrically relative to the shear centre of a member, or when the structural system requires a beam to act as a support for perpendicular members. Unlike flexure and shear, torsion twists the cross-section about its own axis, producing a complex three-dimensional state of stress.

Two fundamentally different types of torsion arise in structural frames, and they must be treated differently in design:

  • Equilibrium (Primary) Torsion: The torsional moment is required for static equilibrium — it cannot be redistributed without collapse of the structure. A cantilevering spandrel beam loaded off-axis is a classic example. Full torsional design is mandatory.
  • Compatibility (Secondary) Torsion: The torsional moment arises from compatibility of deformations in a statically indeterminate structure. After cracking, the torsional stiffness drops sharply and the moment redistributes to adjacent members. EC2 §6.3.1 and ACI commentary permit neglecting compatibility torsion provided the structure can accommodate cracking and the member is detailed with minimum reinforcement.

Thin-Walled Tube (Bredt) Analogy

Solid rectangular sections under torsion are analysed using the thin-walled closed-section analogy. Once torsional cracks form, the uncracked core becomes ineffective and the section behaves as a thin-walled tube. A constant shear flow q circulates around the perimeter of the enclosed area Ao:

Bredt Shear Flow
q = T / (2·Ao)   [N/mm]
τ = q / tef = T / (2·Ao·tef)   [MPa]
q is constant around the perimeter regardless of wall thickness variation. The enclosed area Ao is taken to the centreline of the equivalent wall. All three codes use this model as the basis for torsional reinforcement design, differing only in how Ao and tef are defined.

Space Truss Model

The design model for torsional reinforcement is the space truss analogy: diagonal concrete compression struts form on the faces of the section, resisted by transverse tension in closed stirrups and longitudinal tension in corner bars. This truss must be closed — open stirrups cannot carry torsion. The strut angle θ (measured from the member axis) may be taken as 45° (ACI, IS 456) or optimised between 21.8° and 45° (EC2 variable-angle method).

Combined Torsion and Shear

Torsion and shear co-exist in most real beams. Both produce shear stresses on the section walls, but their directions differ: on two opposite faces they add, and on the other two they subtract. Design codes therefore require checking the combined demand against the section's maximum capacity, typically through a circular or linear interaction equation. The reinforcement contributions add directly — stirrups from both shear and torsion sum.

ACI 318-25↑ Top

ACI 318-25 §22.7 Torsional Strength

ACI 318-25 uses the thin-walled tube space-truss model at θ = 45°. The design shear flow area Ao = 0.85·Aoh, where Aoh is the area enclosed by the centreline of the outermost closed transverse reinforcement.

Torsional Section Geometry
Aoh = x1 · y1   (area enclosed by stirrup centreline, mm²)
Ph = 2(x1 + y1)   (stirrup centreline perimeter, mm)
Ao = 0.85·Aoh ·   Acp = b·h ·   Pcp = 2(b+h)
x1 = b − 2(ccover + dstirrup/2),   y1 = h − 2(ccover + dstirrup/2)
Threshold Torsion — §22.7.4 (below this, torsion may be neglected)
Tth = 0.083·λ·√f'c·(Acp²/Pcp)   [N·mm, MPa, mm]
If Tu ≤ φTth (φ = 0.75): torsion effects may be neglected
If Tu > φTth: full torsional design required
The threshold is the torsion at which diagonal cracking begins. Below this level, the uncracked section can carry torsion through concrete tensile resistance alone, and reinforcement is not needed for torsion specifically.
Required Transverse Reinforcement — §22.7.6.1 (per stirrup leg)
At/s = Tu / (φ·2·Ao·fyt·cot θ)   θ = 45° → cot θ = 1.0
At/s is the torsion contribution per stirrup leg. Add to the shear contribution Av/(2s) per leg to get the total closed stirrup requirement.
Required Longitudinal Reinforcement — §22.7.6.1
Al = (At/s)·Ph·(fyt/fy)·cot²θ   [mm²]
Al,min = 0.42√f'c·Acp/fy − (At/s)·Ph·(fyt/fy)   (§9.7.5.1)
Spacing of longitudinal bars ≤ 300 mm; at least one bar per corner
Longitudinal bars carry the horizontal component of the inclined strut forces. They are distributed around the perimeter of the section — not concentrated at the corners alone — to maintain the space truss geometry.
Section Adequacy — Combined V + T Interaction (§22.7.7.2, solid sections)
√[(Vu/(bw·d))² + (Tu·Ph/(1.7·Aoh²))²] ≤ φ·(Vc/(bw·d) + 0.66√f'c)
This check limits concrete strut compression. If exceeded, the section dimensions must be increased — additional reinforcement alone cannot solve a strut crushing failure.

ACI 318-25 §9.7.5 Detailing Rules

  • Stirrups must be closed (hooks at both ends engaging longitudinal bars)
  • Maximum stirrup spacing: Ph/8 ≤ 300 mm
  • Longitudinal bars: ≥ 1 bar per corner, spacing ≤ 300 mm around perimeter
  • Longitudinal bars must have fy ≥ 420 MPa; db ≥ sstirrup/24 (§9.7.5.3)
Eurocode 2↑ Top

EN 1992-1-1 §6.3 Torsional Resistance

EC2 models solid sections as thin-walled closed sections. No concrete contribution to torsional resistance is assumed — once cracked, all torsion is carried entirely by reinforcement (unlike shear, where VRd,c exists).

Effective Wall Thickness and Enclosed Area — §6.3.2
tef = A/u   but ≥ 2·c   (A = cross-section area, u = outer perimeter, c = cover to longitudinal bar)
Ak = (b − tef)·(h − tef)   (area enclosed by wall centreline)
uk = 2·[(b − tef) + (h − tef)]   (perimeter of Ak)
For a rectangular section 350×600 mm with c = 40 mm: A = 210,000 mm², u = 1,900 mm → tef = 210,000/1,900 = 110 mm; check 2c = 80 mm → tef = 110 mm governs.
Required Stirrup Area (per leg) — §6.3.2(2)
Asw/s = TEd / (2·Ak·fywd·cot θ)
θ = 45° (recommended): Asw/s = TEd / (2·Ak·fywd)
fywd = fywk/γs = fywk/1.15
Required Longitudinal Steel — §6.3.2(3)
Asl = (Asw/s)·uk·(fywd/fyd)·cot²θ
For θ = 45°: cot²θ = 1. Distributed uniformly around the perimeter at spacing ≤ uk/8 ≤ 350 mm; one bar per corner required (§9.2.3).
Maximum Torsional Resistance — §6.3.2(4)
TRd,max = 2·ν·fcd·Ak·tef·sin θ·cos θ   (θ = 45°: TRd,max = ν·fcd·Ak·tef)
ν = 0.6·(1 − fck/250)   (concrete strut strength reduction factor)
Shear + Torsion Interaction — §6.3.2(4)
TEd/TRd,max + VEd/VRd,max ≤ 1.0
VRd,max = 0.5·bw·z·ν·fcd   (same as pure shear maximum; §6.2.3)
If this interaction is not satisfied, increase the section dimensions or concrete strength. Unlike ACI's circular interaction, EC2 uses a linear interaction equation, which is more conservative near the corners of the design space.

EN 1992-1-1 §9.2.3 Torsion Detailing

  • Stirrups must be fully closed loops with 135° hooks or welded
  • At least one longitudinal bar at each corner of the stirrup
  • Stirrup spacing ≤ uk/8 and ≤ min(b, h, 350 mm)
  • Longitudinal bar spacing ≤ 350 mm
IS 456:2000↑ Top

IS 456:2000 Cl. 41 Equivalent Shear-Moment Method

IS 456 does not use the space-truss or thin-walled tube model. Instead, torsion is converted into equivalent shear and equivalent bending moment, which are then added to the actual shear and bending moment for design. This simplified method is applicable to beams of compact cross-section under moderate combined loading.

Equivalent Shear — Cl. 41.3.1
Ve = Vu + 1.6·Tu/b
τve = Ve/(b·d)   (equivalent nominal shear stress)
Check: τve ≤ τc,max (Table 20: 3.1 MPa for M25, 3.5 MPa for M30)
If τve exceeds τc,max, the section must be redesigned — increase b or fck.
Equivalent Bending Moments — Cl. 41.4.2
Mt = Tu·(1 + D/b)/1.7   (torsion equivalent moment, kN·m)
Me1 = Mu + Mt   → design longitudinal steel on tension face (bottom bars)
Me2 = Mt − Mu   → if Me2 > 0: design longitudinal steel on compression face (top bars)
The factor (1 + D/b)/1.7 accounts for the aspect ratio of the cross-section. For a square section (D = b), Mt = Tu×2/1.7 = 1.18Tu. For deeper sections (D > b), the equivalent moment is larger.
Transverse Reinforcement for Combined V + T — Cl. 41.3.2
Asv/sv = (τve − τc)·b / (0.87·fy)   (design τc from Table 19)
Minimum Asv/sv = 0.4·b / (0.87·fy) — Cl. 26.5.1.6
sv,max = min(x1, y1/4, 300 mm) — Cl. 26.5.1.7
x1 and y1 are the shorter and longer centre-to-centre dimensions of the closed stirrup, respectively.

Comparison of the Three Approaches

FeatureACI 318-25Eurocode 2IS 456:2000
Design modelSpace truss (θ = 45°)Thin-walled tube (θ = 21.8–45°)Equivalent shear + moment
Concrete contributionNone (T carried by steel)None (T carried by steel)τc contributes to Ve
Compatibility torsionMay neglect if Tu ≤ φTthMay neglect per §6.3.1Full design required
Stirrup type requiredClosed, hooked at both endsFully closed loopsTwo-legged closed links
Longitudinal steelAdditional Al distributed around perimeterAdditional Asl distributed around perimeterIncluded via Me1 / Me2
TS 500:2000↑ Top

TS 500:2000 §9 Torsion Design

TS 500 §9 uses the thin-walled space-truss (Bredt) analogy — the same physical model as ACI 318 and EC2, but with a fixed strut angle of 45°. The section is replaced by an equivalent thin-walled tube, and shear flow is balanced by stirrups and longitudinal bars.

Equivalent thin-wall geometry — §9.1
Ak = area enclosed by centreline of closed stirrup
uk = perimeter of Ak
tef = Ak / uk   (effective wall thickness)
Section adequacy check — §9.3.4
Vd/(bw·d) + Td/(2·Ak·tef) ≤ 0.22·fcd
Combined shear + torsion stress must not exceed the compression strut limit. If exceeded, increase section dimensions or concrete grade.
Stirrup requirement for torsion — §9.3.2
Tr = 2·Ak·(Asv/sv)·fywd   (at θ = 45°, cot θ = 1)
Required: Asv/sv ≥ Td / (2·Ak·fywd)
Stirrups must be closed links; max spacing: sv ≤ min(uk/8, 300 mm)
Longitudinal reinforcement for torsion — §9.3.3
Al = (Asv/sv) · uk · fywd/fyd
Additional longitudinal bars are distributed uniformly around the section perimeter to balance the diagonal torsion force.
Worked Example↑ Top

Example — ACI 318-25 Torsion Design (Rectangular Beam)

Given: Rectangular section b = 350 mm, h = 600 mm. Concrete f'c = 28 MPa, steel fy = fyt = 420 MPa. Clear cover = 40 mm to stirrup face, stirrup Ø10. Factored torsion: Tu = 60 kN·m. (Shear design handled separately; focus on torsion here.)

  1. Section geometry
    Acp = 350×600 = 210,000 mm² · Pcp = 2(350+600) = 1,900 mm
    x1 = 350 − 2(40+5) = 260 mm · y1 = 600 − 2(40+5) = 510 mm
    Aoh = 260×510 = 132,600 mm² · Ph = 2(260+510) = 1,540 mm
    Ao = 0.85×132,600 = 112,710 mm²
  2. Threshold torsion — §22.7.4
    Tth = 0.083×1.0×√28×(210,000²/1,900) / 106 = 0.083×5.292×23,210,526/106 = 10.19 kN·m
    φTth = 0.75×10.19 = 7.64 kN·m
    Tu = 60 kN·m >> φTth → Torsion design required
  3. Required transverse reinforcement — §22.7.6.1
    At/s = Tu/(φ·2·Ao·fyt·cot θ) = 60×106/(0.75×2×112,710×420×1.0)
    = 60×106/71,007,300 = 0.845 mm²/mm per stirrup leg
    For Ø10 closed stirrups: At = 78.5 mm² per leg
    Required s ≤ 78.5/0.845 = 92.9 mm → Use s = 90 mm
    At,prov/s = 78.5/90 = 0.872 mm²/mm > 0.845 ✓
    Check max spacing: Ph/8 = 1,540/8 = 192 mm → 90 mm < 192 mm ✓
  4. Required longitudinal torsion steel — §22.7.6.1
    Al = (At/s)·Ph·(fyt/fy)·cot²θ
    = 0.845×1,540×(420/420)×1.0² = 1,301 mm²
    Minimum Al (§9.7.5.1): 0.42×5.292×210,000/420 − 0.845×1,540 = 1,112 − 1,301 < 0 → not governing
    Al = 1,301 mm² governs
  5. Distribute longitudinal bars
    Spacing ≤ 300 mm around perimeter; one bar per corner required
    Perimeter ≈ Ph = 1,540 mm → need ≥ 1,540/300 ≈ 6 bars
    Use 8Ø16 (8×201 = 1,608 mm² ≥ 1,301 mm²) evenly spaced at ~193 mm ✓
Result: Ø10 closed stirrups @ 90 mm (torsion governs spacing; add shear contribution to get total stirrup area if combined V+T). 8Ø16 longitudinal bars distributed evenly around the section perimeter (one per corner + one at mid-face of each side).
Note: A section adequacy check for combined V+T per §22.7.7.2 must also be performed using the actual factored shear Vu.
References↑ Top

References

  • [1]
    ACI 318-25 — Building Code Requirements for Structural Concrete. American Concrete Institute, 2025. §22.7 (Torsional strength), §9.7.5 (Longitudinal torsional reinforcement), §9.7.6.3 (Torsional reinforcement detailing).
  • [2]
    EN 1992-1-1:2004 — Eurocode 2: Design of Concrete Structures. CEN, Brussels. §6.3 (Torsion), §9.2.3 (Torsion reinforcement detailing). Variable-angle truss method.
  • [3]
    IS 456:2000 — Plain and Reinforced Concrete — Code of Practice, 4th Rev. Bureau of Indian Standards. Cl. 41 (Torsion — equivalent shear and bending moment method), Cl. 26.5.1.7 (Stirrup spacing for torsion).
  • [4]
    Hsu, T.T.C. — Unified Theory of Reinforced Concrete. CRC Press, 1993. Chapter 4 (Torsion — softened truss model and space-truss analogy).
  • [5]
    Collins, M.P. & Mitchell, D. — Prestressed Concrete Structures. Prentice-Hall, 1991. Chapter 6 (Combined flexure, shear and torsion).
  • [6]
    MacGregor, J.G. & Wight, J.K. — Reinforced Concrete: Mechanics and Design, 7th Ed. Pearson, 2016. Chapter 7 (Torsion in Beams — derivation of ACI design equations).
  • [7]
    TS 500:2000 — Requirements for Design and Construction of Reinforced Concrete Structures. Turkish Standards Institution, Ankara. §9 (Torsion — thin-walled tube analogy), §9.3.2 (Stirrup requirement), §9.3.3 (Longitudinal reinforcement), §9.3.4 (Section adequacy — 0.22fcd limit).
Disclaimer: For educational and preliminary design only. All results must be verified by a licensed structural engineer. Always refer to the current edition of the applicable code.
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