W360x1202 G40.21 350W — Canadian W-Shape Section Properties

Approximate equivalent of W14X808 per AISC A6. Approx. equivalent of W14X808. Verify against CISC Handbook.

Dimensions (Metric)

Property Value Unit
Depth (d) 579.1 mm
Flange Width (bf) 472.4 mm
Flange Thickness (tf) 130.0 mm
Web Thickness (tw) 95.0 mm
Cross-Sectional Area (A) 1535.6 cm²
Mass 1202.3 kg/m

Elastic Section Properties (Metric)

Property Strong Axis (X-X) Weak Axis (Y-Y) Unit
Moment of Inertia (I) 661,806 231,008 cm⁴
Elastic Section Modulus (S) 22,778 9,783 cm³
Plastic Section Modulus (Z) 29,988 15,240 cm³
Radius of Gyration (r) 20.75 12.27 cm

Torsional Properties

Property Value Unit
Torsional Constant (J) 76,586 cm⁴
Warping Constant (Cw) 116,529,000 cm⁶
Distance Between Flange Centroids (ho) 44.96 cm
Effective Radius (rts) 15.09 cm

Imperial Reference

Property Value Unit
Depth (d) 22.80 in
Flange Width (bf) 18.60 in
Area (A) 238.00 in²
Weight 808 lb/ft

Section Profile Summary

Hot-rolled W-shape with Sx = 22,778 cm³. The section is commonly specified for primary framing in multi-storey buildings, crane girders, and bridge stringers.

At 579.1 mm deep and 1202.3 kg/m, this is a heavy section for primary framing — transfer beams, long-span roof girders, and major bridge stringers.

Key Design Checks (CSA S16)

Check Formula This Section
Plastic moment Mp = Zx × Fy 10,496 kN·m
Deflection Δ = 5wL⁴/(384EIx) Use Ix = 661,806 cm⁴
Torsion St. Venant = GJ/L J = 76,586 cm⁴
Column buckling KL/r → Fcr r_x = 20.75 cm

Design Notes

Verification (CSA S16): All designs using this section must be verified by a licensed Professional Engineer. Before finalizing member selection, check beam-column interaction (P-M), lateral-torsional buckling, serviceability deflections, and all connection limit states. See Engineering Disclaimer.

Worked Example: Roof beam (flat roof) — w360x1202

Scenario: Flat roof with services — allowance for mechanical units and drainage. Simply supported wide flange, 9.8 m span, 3.6 m tributary width. Service loads: 2.0 kPa dead + 1.5 kPa live (12.6 kN/m total).

Given:

Step 1 — Live load deflection:

Δ_LL = 5 w_L L⁴ / (384 E Ix)

Δ_LL = 5 × 5.4 × (9845)⁴ / (384 × 200000 × 6,618,060,000)

Δ_LL = 0.5 mm

Step 2 — Deflection limit (L/250):

Δ_limit = L / 250 = 9845 / 250 = 39.4 mm

Step 3 — Dead + live deflection:

Δ_total = 1.2 mm

Step 4 — Design check:

✓ Live load deflection is within the L/250 limit.

Verify the design moment M*_Ed (from factored loads 1.35G + 1.5Q per CSA S16) does not exceed φMn = 9,446 kN·m. Also confirm shear resistance and bearing details at the supports.

Related Resources

Design Resources


Educational reference only. Verify all section properties against the current CSA S16 Manual and mill certificates before design. Results are PRELIMINARY — NOT FOR CONSTRUCTION.