W530x165 G40.21 350W — Canadian W-Shape Section Properties

Approximate equivalent of W21X111 per AISC A6. Approx. equivalent of W21X111. Verify against CISC Handbook.

Dimensions (Metric)

Property Value Unit
Depth (d) 546.1 mm
Flange Width (bf) 312.4 mm
Flange Thickness (tf) 22.2 mm
Web Thickness (tw) 14.0 mm
Cross-Sectional Area (A) 210.3 cm²
Mass 165.2 kg/m

Elastic Section Properties (Metric)

Property Strong Axis (X-X) Weak Axis (Y-Y) Unit
Moment of Inertia (I) 111,133 11,405 cm⁴
Elastic Section Modulus (S) 4,080 729 cm³
Plastic Section Modulus (Z) 4,572 1,118 cm³
Radius of Gyration (r) 22.99 7.37 cm

Torsional Properties

Property Value Unit
Torsional Constant (J) 284 cm⁴
Warping Constant (Cw) 7,840,200 cm⁶
Distance Between Flange Centroids (ho) 52.32 cm
Effective Radius (rts) 8.56 cm

Imperial Reference

Property Value Unit
Depth (d) 21.50 in
Flange Width (bf) 12.30 in
Area (A) 32.60 in²
Weight 111 lb/ft

Section Profile Summary

With Ix = 111,133 cm⁴, this wide flange is commonly specified for long-span floor beams and transfer girders where stiffness controls the design.

At 546.1 mm deep and 165.2 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 1,600 kN·m
Deflection Δ = 5wL⁴/(384EIx) Use Ix = 111,133 cm⁴
Torsion St. Venant = GJ/L J = 284 cm⁴
Column buckling KL/r → Fcr r_x = 22.99 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: School classroom beam — w530x165

Scenario: School building — tighter deflection limit for suspended ceiling integrity. Simply supported wide flange, 10.9 m span, 2.4 m tributary width. Service loads: 3.5 kPa dead + 3.0 kPa live (15.6 kN/m total).

Given:

Step 1 — Live load deflection:

Δ_LL = 5 w_L L⁴ / (384 E Ix)

Δ_LL = 5 × 7.2 × (10922)⁴ / (384 × 200000 × 1,111,330,000)

Δ_LL = 6.0 mm

Step 2 — Deflection limit (L/360):

Δ_limit = L / 360 = 10922 / 360 = 30.3 mm

Step 3 — Dead + live deflection:

Δ_total = 13.0 mm

Step 4 — Design check:

✓ Live load deflection is within the L/360 limit.

Verify the design moment M*_Ed (from factored loads 1.35G + 1.5Q per CSA S16) does not exceed φMn = 1,440 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.