AISC 360-22 Cantilever Beam Design — Worked Example
Complete step-by-step flexural design of a cantilever steel beam per AISC 360-22. Covers section classification, lateral-torsional buckling with bottom flange bracing, shear capacity, deflection (cantilever vs. simple span comparison), and serviceability limits. All calculations in US customary units.
Related pages: AISC Beam Design Guide | Deflection Guide | Beam Capacity Calculator | Lateral Torsional Buckling
Problem Statement
A steel-framed balcony extends 8 ft from the face of the building. The cantilever beams are W16x26 at 6 ft spacing, supporting a 4-1/2 in. normal-weight concrete slab on 2 in. composite steel deck (total 6-1/2 in.). The building is a 3-storey office located in a moderate wind region.
Design data:
- Cantilever span: L = 8 ft
- Beam spacing: s = 6 ft c/c
- Beam: W16x26, ASTM A992 (Fy = 50 ksi, Fu = 65 ksi)
- Deck: 2 in. deep, 20-gauge composite deck with 4-1/2 in. NWC topping
- Loads: Dead = 58 psf (slab + deck + MEP + ceiling), Live = 100 psf (balcony, per ASCE 7-22 Table 4.3-1), Superimposed dead = 15 psf (railing + finishes)
- Deflection limit: L/240 for total load (ASCE 7-22 Appendix C, pedestrian comfort)
- Lateral bracing: Bottom flange unbraced (exposed), tip bracing via perimeter beam at 8 ft
Step 1 — Load Determination
Service loads (per beam):
Tributary width per beam = 6 ft
- w_D = (58 + 15) psf x 6 ft = 438 plf = 0.438 klf (dead + superimposed)
- w_L = 100 psf x 6 ft = 600 plf = 0.600 klf (live)
Factored load combination (ASCE 7-22, LRFD):
wu = 1.2 x 0.438 + 1.6 x 0.600 = 0.526 + 0.960 = 1.486 klf
Step 2 — Design Actions (Cantilever)
For a uniformly loaded cantilever of length L = 8 ft:
Maximum factored moment (at support): Mu = wu x L^2 / 2 = 1.486 x 8.0^2 / 2 = 1.486 x 32.0 = 47.6 kip-ft
Maximum factored shear (at support): Vu = wu x L = 1.486 x 8.0 = 11.9 kips
Step 3 — Section Properties (W16x26, A992)
| Property | Value | Unit |
|---|---|---|
| Depth d | 15.7 | in. |
| Flange width bf | 5.50 | in. |
| Flange thickness tf | 0.345 | in. |
| Web thickness tw | 0.250 | in. |
| Plastic modulus Zx | 44.2 | in^3 |
| Elastic modulus Sx | 38.4 | in^3 |
| Moment of inertia Ix | 301 | in^4 |
| Radius of gyration ry | 1.12 | in. |
| Torsional constant J | 0.262 | in^4 |
| Warping constant Cw | 565 | in^6 |
Section classification per AISC Table B4.1b: flange lambda_f = 7.97 < lambda_pf = 9.15 (Compact). Web lambda_w = 60.0 < lambda_pw = 90.5 (Compact). Section is Compact for flexure.
Step 4 — Flexural Capacity (AISC 360 Chapter F)
Plastic moment (AISC Eq. F2-1): Mp = Fy x Zx = 50 x 44.2 = 184.2 kip-ft, phi_b x Mp = 165.8 kip-ft
Lateral-Torsional Buckling (AISC Section F2.2): The cantilever bottom flange is in compression and unbraced between support and tip brace. Lb = 8 ft = 96 in.
Lp = 1.76 x ry x sqrt(E/Fy) = 1.76 x 1.12 x 24.08 = 47.5 in. = 3.96 ft Lr approximately 12.2 ft for W16x26. Lp < Lb < Lr — inelastic LTB governs.
phi_b x Mn = Cb x [phi_b x Mp - (phi_b x Mp - 0.7 x Fy x Sx) x (Lb - Lp)/(Lr - Lp)]
For cantilever, Cb = 1.0 per AISC Manual Part 3.
phi_b x Mn = 1.0 x [165.8 - (165.8 - 112.0) x (8.0 - 3.96)/(12.2 - 3.96)] = 165.8 - 53.8 x 0.490 = 139.4 kip-ft
Flexural utilisation: Mu / (phi_b x Mn) = 47.6 / 139.4 = 0.341 (34.1%)
Step 5 — Shear Capacity (AISC 360 Section G2)
h/tw = 60.0. 2.24 x sqrt(E/Fy) = 53.9 < 60.0 — check shear buckling. kv = 5.34 for unstiffened web. 1.10 x sqrt(kv x E/Fy) = 61.2 > 60.0 — Cv = 1.0, shear yielding governs.
Aw = d x tw = 3.93 in^2, Vn = 0.6 x Fy x Aw x Cv = 117.9 kips, phi_v x Vn = 106.1 kips
Vu = 11.9 kips << 106.1 kips — OK, utilisation = 11.2%
Step 6 — Deflection Check (Serviceability)
Cantilever deflection: delta = w x L^4 / (8 x E x I)
w_total = 1.038 klf = 0.0865 kips/in. delta_total = 0.105 in. = L/914
Simple span comparison (same length, same load):
delta_simple = 5 x w x L^4 / (384 x E x I) = 0.0110 in. = L/8,760 Ratio: delta_cantilever / delta_simple = 0.105 / 0.0110 = 9.55 — consistent with theoretical 9.6x.
Live load deflection: w_L = 0.600 klf. delta_LL = 0.0608 in. = L/1,579
Deflection limits: L/240 (total) = 0.400 in. — OK (0.105 in.) L/360 (live) = 0.267 in. — OK (0.061 in.)
Step 7 — Lateral Bracing Detail
A perimeter spandrel beam (W12x22) at cantilever tips provides lateral brace points at 8 ft. Bracing force per AISC Appendix 6:
P_brace = 0.02 x Mu x Cd / (h0 x phi) = 0.02 x (47.6 x 12) / (15.4 x 0.75) = 0.99 kips per cantilever
With 10 bays: total bracing force = 9.9 kips. A 2x2x1/4 angle brace is adequate.
Step 8 — Vibration Check
Natural frequency: f_n = (1/(2 x pi)) x sqrt(g/delta_total) = 0.1592 x sqrt(386.4/0.105) = 9.66 Hz > 3 Hz — OK per AISC DG 11.
Summary of Checks
| Limit State | Reference | Capacity | Demand | Utilisation |
|---|---|---|---|---|
| Flexure (LTB) | AISC F2-2 | 139.4 kip-ft | 47.6 kip-ft | 34.1% |
| Shear yielding | AISC G2-1 | 106.1 kips | 11.9 kips | 11.2% |
| Deflection (total) | L/240 | 0.400 in. | 0.105 in. | 26.3% |
| Deflection (live) | L/360 | 0.267 in. | 0.061 in. | 22.8% |
| Vibration | AISC DG 11 | >3 Hz | 9.66 Hz | OK |
Conclusion: The W16x26 cantilever beam at 8 ft span satisfies all AISC 360-22 limit states, with flexure at 34% utilisation being the controlling strength check. The beam is deflection-limited — a shallower section would increase deflections and reduce vibration frequency.