RC Beam Design Step-by-Step: Flexure, Shear, and Deflection

A complete walkthrough of reinforced concrete rectangular beam design per ACI 318-25, covering preliminary sizing, flexural reinforcement, shear stirrup design, minimum steel requirements, and deflection control — illustrated with a fully worked numerical example.

For preliminary sizing (ACI Table 9.3.1.1), flexural design formulas, and minimum/maximum steel limits, see US Standards Design Guide — Part 6: RC Design (ACI 318-25).

2. Factored Loads and Design Moment

Using ASCE 7-22 / ACI 318-25 load combinations:

wu = 1.2 D + 1.6 L  (governing gravity combination) Mu = wu · L² / 8  (simply supported) Vu = wu · L / 2  (simply supported, at face of support)

For continuous beams, use ACI moment coefficients (Table 6.5.2) or an elastic frame analysis. Moment redistribution of up to 20% is permitted at supports (ACI §6.6.5).

5. Shear Design — Stirrups

ACI 318-25 §22.5 (detailed method):

Vc = [8λ(ρw)1/3(f'c)1/3 + Nu/(6Ag)] × bwd / 6  (SI units, MPa) φVc + φVs ≥ Vu  (φ=0.75) Vs = Avfytd / s

Rearranging for required stirrup spacing: s = Avfytd / Vs

ZoneConditionMax spacing
No stirrups requiredVu ≤ 0.5φVc—
Min stirrups only0.5φVc < Vu ≤ φVcd/2 ≤ 600 mm
Standard shear zoneVu ≤ φ(Vc+4Vc)d/2 ≤ 600 mm
High shear zoneVs > 4Vcd/4 ≤ 300 mm

Minimum stirrup area: Av,min/s = max(0.062√f'c/fyt, 0.35/fyt) × bw

Critical section for shear: located at d from the face of support (not at the support itself). The shear force at d from the support governs stirrup design in most cases.

6. Deflection Control

If h ≥ hmin from Table 9.3.1.1, no deflection calculation is needed. Otherwise, compute:

Δimmediate = 5wL⁴ / (384EcIe)  (simply supported, uniform load) Ie = Ig·(Mcr/Ma)³ + Icr[1−(Mcr/Ma)³] ≤ Ig  (ACI §24.2.3.5) Mcr = fr·Ig/yt   fr = 0.62√f'c (MPa)

Long-term deflection multiplier per ACI §24.2.4:

Δlong-term = λΔ · Δimmediate,sustained λΔ = ξ / (1 + 50ρ')  [ξ=2.0 for 5+ years, 1.4 for 12 months, 1.2 for 6 months]
Span ConditionDeflection Limit (ACI Table 24.2.2)
Immediate live load, flat roofsL/180
Immediate live load, floorsL/360
Total (creep+shrinkage+LL), non-structural elements attachedL/480
Total (creep+shrinkage+LL), no non-structural elementsL/240

7. Worked Example — 6 m Simply-Supported Beam

Given: L=6.0 m, Dead load D=20 kN/m (includes self-weight), Live load L=25 kN/m. f'c=28 MPa, fy=420 MPa. Try b=300 mm, h=550 mm (hmin=6000/16=375 mm ✓).

Step 1 — Factored loads:

wu = 1.2×20 + 1.6×25 = 24 + 40 = 64 kN/m

Mu = 64×6²/8 = 288 kN·m  |  Vu,face = 64×6/2 = 192 kN

Step 2 — Effective depth: d = 550 − 40 − 10 − 12 = 488 mm (Ø24 main bar)

Step 3 — Flexural design:

a = 488 − √(488² − 2×288×10⁶/(0.90×0.85×28×300)) = 488 − √(238,144 − 90,240) = 488 − √147,904 = 488 − 384.6 = 103.4 mm

As = 288×10⁶ / (0.90×420×(488−51.7)) = 288×10⁶ / (0.90×420×436.3) = 288×10⁶/164,890 = 1,746 mm²

Use 4Ø25 (As,prov=1,963 mm²) arranged in one row. Check spacing: (300−2×40−2×10−4×25)/(3) = 46.7 mm > 25 mm ✓

Step 4 — Minimum steel: As,min = 0.00333×300×488 = 488 mm² < 1,746 mm² ✓

Step 5 — Shear at d from support: Vu,d = 192 − 64×0.488 = 192 − 31.2 = 160.8 kN

ρw = 1963/(300×488) = 0.01342

Vc = [8×1.0×(0.01342)1/3×(28)1/3] × 300×488/6×10⁻³ = [8×0.2389×3.037]×24,400/6×10⁻³ = 5.809×4,067×10⁻³ = 128.4 kN

φVc = 0.75×128.4 = 96.3 kN < Vu,d=160.8 kN → stirrups required

Vs = (160.8−96.3)/0.75 = 86.0 kN

Use Ø10 double-leg stirrups (Av=2×78.5=157 mm²): s = 157×420×488/(86,000) = 374 mm < d/2=244 mm → use s=200 mm

Step 6 — Deflection: h=550 > hmin=375 mm → no calculation required per ACI Table 9.3.1.1 ✓

Summary: 300×550 mm beam, 4Ø25 flexural bars, Ø10@200 stirrups throughout (closer spacing near supports in practice). Use the Beam Design Calculator to automate these calculations.
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