Beam Design
Flexural design, flexural capacity, and torsion design for rectangular RC beams.
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
SI · kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
SI · kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
SI · kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
Input Parameters
kN-m · mSection Geometry
📚 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
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 §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.
ρw = Asl / (bw · d) (longitudinal tension reinforcement ratio)
Vs,max = 0.66 √f'c · bw · d (§22.5.1.2 — if exceeded, increase section)
If Vs > 0.33√f'c · bw · d: smax = min(d/4, 300 mm)
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.
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
VRd,max = 0.5 · bw · z · ν · fcd (ν = 0.6(1−fck/250), fcd = fck/γc)
ρw,min = 0.08 √fck / fywk
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.
τc,max from Table 20: M20 → 2.8, M25 → 3.1, M30 → 3.5, M35 → 3.7, M40+ → 4.0 N/mm²
Required Asv/sv = (Vu − τc·b·d) / (0.87·fy·d)
Max spacing: sv,max = min(0.75d, 300 mm) — Cl. 26.5.1.5
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.
Vcr = 0.65 · fctd · bw · d
Vr,max = 0.22 · fcd · bw · d (§8.1.3 — compression strut limit)
sv,max = min(d/2, 300 mm)
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.
- Longitudinal reinforcement ratio
ρw = As/(bw·d) = 1,520/(300×500) = 0.01013 - 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 - Shear reinforcement required?
Vu = 180 kN > φVc = 48.8 kN → Stirrups required - Required stirrup contribution
φVs,req = Vu − φVc = 180 − 48.8 = 131.2 kN
Vs,req = 131.2/0.75 = 174.9 kN - 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 ✓ - 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 - 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 - 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 ✓
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
- [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).
Input Parameters
SI · kN-m · mSection Geometry
📚 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:
- 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.
- 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.
- 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.
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)
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.
εcu = 0.003 · εy = fy / 200 000 (fy in MPa)
Example (f'c = 28 MPa, fy = 420 MPa): ρbal ≈ 0.0285
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.
| Code | Ductility Requirement | Implication |
|---|---|---|
| ACI 318-25 | Net tensile strain εt ≥ 0.004 at ULS (φ = 0.90 when εt ≥ 0.005) | ρ ≤ ≈ 0.75 ρbal |
| Eurocode 2 | Neutral axis x/d ≤ 0.45 (for δ ≥ 0.7 redistribution) | K ≤ K' = 0.167 |
| IS 456:2000 | xu/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
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.
φ = 0.65 → 0.90 transition zone (0.002 < εt < 0.005)
φ = 0.65 compression-controlled (εt ≤ 0.002)
ACI 318-25 §22.2 Stress Block & Reinforcement
β₁ = 0.85 − 0.05·(f'c − 28)/7 (f'c > 28 MPa)
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
ρmax = 0.75·ρbal (ensures εt ≥ 0.005)
ACI 318-25 Material Limits
| Parameter | Minimum | Maximum | Reference |
|---|---|---|---|
| Concrete f'c | 17 MPa (2500 psi) | 70 MPa (10000 psi)* | §19.2.1 |
| Rebar fy | 280 MPa (40 ksi) | 550 MPa (80 ksi) | §20.2.2 |
| Strength factor φ | 0.65 | 0.90 | Table 21.2.2 |
* Higher f'c permitted with special provisions per §19.2.1.3
ACI 318-25 §25.2 Minimum Bar Spacing
For bars in multiple layers: vertical clear spacing ≥ 25 mm
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.
s ≤ 300 · (280/fs) (interior exposure limit)
fs = 2/3 · fy (approximate service bar stress, MPa)
cc = clear cover to flexural tension reinforcement
ACI 318-25 §22.2 Design Summary
The complete ACI flexural design procedure for a singly reinforced rectangular section:
- Compute Rn = Mu / (φ · b · d²)
- Solve ρ = (0.85f'c / fy) · [1 − √(1 − 2Rn / 0.85f'c)]
- Check ρmin ≤ ρ ≤ ρmax (= 0.75 ρbal)
- As = ρ · b · d
- Check εt ≥ 0.004; confirm φ = 0.90
- Verify bar spacing ≥ sclear,min and ≤ scrack,max
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.
fyd = fyk/γs [γs=1.15]
EN 1992-1-1 §6.1 Flexural Design
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
EN 1992-1-1 §9.2.1.1 Minimum Reinforcement
fctm = 0.30·fck2/3 (fck ≤ 50 MPa)
Example (C25/30, fyk=500): fctm=2.56 MPa → ρmin=0.0013
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:
| System | Lightly loaded (ρ = 0.5%) | Normally loaded (ρ = 1.5%) |
|---|---|---|
| Simply supported beam/slab | 20 | 14 |
| End span of continuous | 26 | 18 |
| Interior span of continuous | 30 | 20 |
| Cantilever | 8 | 6 |
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
| Parameter | Minimum | Maximum | Reference |
|---|---|---|---|
| Concrete fck | 12 MPa (C12/15) | 90 MPa (C90/105) | Table 3.1 |
| Rebar fyk | 400 MPa | 600 MPa | §3.2.2 |
| Partial factor γc | 1.0 (accidental) | 1.5 (persistent) | Table 2.1N |
| Partial factor γs | 1.0 (accidental) | 1.15 (persistent) | Table 2.1N |
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:
Mu,lim = 0.36 fck b xu,lim (d − 0.42 xu,lim)
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.
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.
τve = Ve / (b · d) ≤ τc,max
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 §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.
Mrd = Ast·fyd·(d − a/2)
Ast,max = 0.04·b·h
TS 500:2000 §3.3 Material Factors
| Property | Expression | Note |
|---|---|---|
| Concrete design strength fcd | fck/1.5 | §3.3.1 |
| Tensile strength fctk | 0.35·√fck | Table 2.3 |
| Design tensile strength fctd | fctk/1.5 | §3.3.1 |
| Steel design yield fyd | fyk/1.15 | §3.3.2 |
| Partial factor for concrete γc | 1.5 | — |
| Partial factor for steel γs | 1.15 | — |
Design Limits Comparison — ACI 318-25 vs. Eurocode 2 vs. IS 456:2000
| Parameter | ACI 318-25 | Eurocode 2 | IS 456:2000 |
|---|---|---|---|
| Concrete strain at ULS | εcu = 0.003 | εcu = 0.0035 | εcu = 0.0035 |
| Resistance / partial factor | φ = 0.90 (flexure) | γc=1.5 · γs=1.15 | γc=1.5 · γs=1.15 (implicit) |
| Stress block depth factor | β₁ = 0.85 → 0.65 | λ = 0.8 (fck ≤ 50 MPa) | 0.36·fck·b·xu (parabolic-rect.) |
| Stress block intensity | 0.85·f'c | η·fcd, η=1.0 | 0.36·fck (equiv. rect. block) |
| Minimum reinforcement | max(0.25√f'c/fy, 1.4/fy)·b·d | max(0.26fctm/fyk, 0.0013)·b·d | 0.85·b·d / fy (Cl. 26.5.1.1a) |
| Maximum reinforcement | ρ ≤ 0.75·ρbal | K ≤ K' = 0.167 | 0.04·b·D (Cl. 26.5.1.1b) |
| Neutral axis limit (xu/d) | Not directly (εt ≥ 0.004) | x/d ≤ 0.45 | Fe415: 0.48 · Fe500: 0.46 · Fe250: 0.53 |
| Maximum lever arm | Not explicitly limited | z ≤ 0.95d | Not explicitly limited |
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.
- 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) - Design resistance coefficient Rn
Rn = Mu/(φ·b·d²) = 250×106/(0.90×300×500²) = 3.704 MPa
- 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 - 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 ✓ - 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 - 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 - 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 ✓
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).
📚 Design Background & Code References — Torsion
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:
τ = q / tef = T / (2·Ao·tef) [MPa]
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 §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.
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)
If Tu ≤ φTth (φ = 0.75): torsion effects may be neglected
If Tu > φTth: full torsional design required
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
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)
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).
Ak = (b − tef)·(h − tef) (area enclosed by wall centreline)
uk = 2·[(b − tef) + (h − tef)] (perimeter of Ak)
θ = 45° (recommended): Asw/s = TEd / (2·Ak·fywd)
fywd = fywk/γs = fywk/1.15
ν = 0.6·(1 − fck/250) (concrete strut strength reduction factor)
VRd,max = 0.5·bw·z·ν·fcd (same as pure shear maximum; §6.2.3)
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 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.
τve = Ve/(b·d) (equivalent nominal shear stress)
Check: τve ≤ τc,max (Table 20: 3.1 MPa for M25, 3.5 MPa for M30)
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)
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
Comparison of the Three Approaches
| Feature | ACI 318-25 | Eurocode 2 | IS 456:2000 |
|---|---|---|---|
| Design model | Space truss (θ = 45°) | Thin-walled tube (θ = 21.8–45°) | Equivalent shear + moment |
| Concrete contribution | None (T carried by steel) | None (T carried by steel) | τc contributes to Ve |
| Compatibility torsion | May neglect if Tu ≤ φTth | May neglect per §6.3.1 | Full design required |
| Stirrup type required | Closed, hooked at both ends | Fully closed loops | Two-legged closed links |
| Longitudinal steel | Additional Al distributed around perimeter | Additional Asl distributed around perimeter | Included via Me1 / Me2 |
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.
uk = perimeter of Ak
tef = Ak / uk (effective wall thickness)
Required: Asv/sv ≥ Td / (2·Ak·fywd)
Stirrups must be closed links; max spacing: sv ≤ min(uk/8, 300 mm)
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.)
- 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 - 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 - 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)For Ø10 closed stirrups: At = 78.5 mm² per leg
= 60×106/71,007,300 = 0.845 mm²/mm per stirrup 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 ✓ - Required longitudinal torsion steel — §22.7.6.1
Al = (At/s)·Ph·(fyt/fy)·cot²θMinimum Al (§9.7.5.1): 0.42×5.292×210,000/420 − 0.845×1,540 = 1,112 − 1,301 < 0 → not governing
= 0.845×1,540×(420/420)×1.0² = 1,301 mm²
Al = 1,301 mm² governs - 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 ✓
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
- [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).