Canadian Cold-Formed Steel Design — CSA S136-19 for Light Gauge Steel

Complete reference for cold-formed steel design per CSA S136-19 (NAS Supplement). Covers effective width method, distortional buckling, local buckling interaction, C-section and Z-section properties, and a worked example for a cold-formed steel purlin in Canadian construction.

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CSA S136 Design Framework

CSA S136-19 (adopting the North American Specification for Cold-Formed Steel) governs the design of cold-formed steel members. Key differences from CSA S16 (hot-rolled):

Parameter CSA S16 (Hot-Rolled) CSA S136 (Cold-Formed)
Thickness t ≥ 4.5 mm typical 0.84-6.0 mm
Fy 350 MPa typical 230-550 MPa
Design approach Plastic/elastic section Effective width method
Buckling modes LTB, LB, FB Local, distortional, global
Resistance factor phi 0.90 (members) 0.90 (members)

Material Grades

CSA Grade Fy (MPa) Fu (MPa) Typical Application
230 MPa 230 310 Light framing, interior studs
275 MPa 275 380 General framing, curtain walls
340 MPa 340 450 Roof purlins, side rails
550 MPa 550 620 High-strength, racking

Grade 340 MPa is the most common for cold-formed structural members in Canada.

Effective Width Method

Per CSA S136 Clause B2, the effective width of a uniformly compressed stiffened element:

b_e = w × (1 - 0.22/lambda_p) / lambda_p when lambda_p > 0.673 b_e = w when lambda_p ≤ 0.673

Where:

Section Types

Section Buckling Mode Effective Width Application
C-section (lipped channel) Local flange, distortional, global Flange + lip, web
Z-section Local flange, distortional, global Flange + lip, web
Hat section Local (stiffened elements) All elements
Track section Local flange, web Flange, web

Distortional Buckling

Per CSA S136 Clause B3.2, distortional buckling is a critical limit state for cold-formed sections with edge stiffeners:

Mn_dist = Sc × Fd (nominal moment capacity for distortional buckling)

Where:

Distortional buckling is unique to cold-formed steel — it occurs when the lip-stiffened flange rotates about the flange-web junction.

Distortional Buckling Stress

Fd = (k_d × pi^2 × E) / (12 × (1 - nu^2)) × (t/b_f)^2

For C-sections, k_d depends on the lip depth to flange width ratio d/b_f:

For most C-sections, distortional buckling governs when the flange width-to-thickness ratio b_f/t > 70/sqrt(Fy/340).

C-Section Properties

Standard C-Section (CS) Dimensions

Designation Depth d (mm) Flange bf (mm) Lip d (mm) t (mm) Mass (kg/m)
CS100×50×15×1.2 100 50 15 1.2 2.11
CS150×50×15×1.5 150 50 15 1.5 3.28
CS200×50×15×1.9 200 50 15 1.9 4.68
CS250×75×18×2.5 250 75 18 2.5 8.02
CS300×75×18×3.0 300 75 18 3.0 10.1

C-Section Flexural Capacity (340 MPa)

Section Sx_eff (×10^3 mm^3) Mr (kN·m) Governing Buckling Mode
CS100×50×15×1.2 8.2 2.5 Local flange
CS150×50×15×1.5 21.5 6.6 Distortional
CS200×50×15×1.9 42.1 12.9 Distortional
CS250×75×18×2.5 88.3 27.0 Local web
CS300×75×18×3.0 131.2 40.1 LTB (global)

Z-Section Properties

Standard Z-Section (ZS) Dimensions

Designation Depth d (mm) Flange bf (mm) Lip d (mm) t (mm) Mass (kg/m)
ZS150×50×15×1.5 150 50 15 1.5 3.28
ZS200×50×15×1.9 200 50 15 1.9 4.68
ZS250×75×18×2.5 250 75 18 2.5 8.02
ZS300×75×18×3.0 300 75 18 3.0 10.1

Z-sections have better bending capacity than C-sections of the same dimensions due to the offset web, which increases the weak-axis section modulus.

Worked Example — Purlin Design

Given: CS200×50×15×1.9 purlin at roof slope 2:12. Span = 6.0 m, continuous over two spans. Purlin spacing = 1.5 m. Loads: dead = 0.5 kPa, snow = 1.0 kPa (NBCC 2020). Grade 340 MPa steel.

Step 1 — Section Properties: CS200×50×15×1.9: mass = 4.68 kg/m, Sx_eff = 42.1 × 10^3 mm^3 Ix_eff = 4.21 × 10^6 mm^4 (approximate — depends on effective width calculation)

Step 2 — Factored Loads: Dead load: 0.5 kPa × 1.5 m = 0.75 kN/m (purlin self-weight: 0.046 kN/m — included) Snow load: 1.0 kPa × 1.5 m = 1.50 kN/m

Load combination (NBCC 2020): 1.25D + 1.5S = 1.25 × 0.80 + 1.5 × 1.50 = 1.0 + 2.25 = 3.25 kN/m

Step 3 — Moment (continuous two-span): Maximum positive moment: M_pos = 0.096 × w × L^2 = 0.096 × 3.25 × 6.0^2 = 11.2 kN·m Maximum negative moment (at interior support): M_neg = 0.063 × w × L^2 = 0.063 × 3.25 × 6.0^2 = 7.4 kN·m

Step 4 — Flexural Capacity: Sx_eff = 42.1 × 10^3 mm^3 (positive bending, compression flange on lip side) Mr = phi × Sx_eff × Fy = 0.90 × 42,100 × 340 / 10^6 = 12.9 kN·m

Step 5 — Check: Mf = 11.2 kN·m ≤ Mr = 12.9 kN·m. Ratio = 0.87. OK.

Step 6 — Deflection (Serviceability): Live load deflection: delta = 0.0069 × w_S × L^4 / (E × Ix_eff) = 0.0069 × 1.50 × 6000^4 / (200,000 × 4.21 × 10^6) = 15.9 mm L/240 = 6000/240 = 25.0 mm. 15.9 < 25.0. OK.

Result: CS200×50×15×1.9 Grade 340 MPa purlin at 1.5 m spacing, spanning 6.0 m continuous over 2 spans. Adequate for factored loads and serviceability.

Connections in Cold-Formed Steel

Per CSA S136 Clause E:

Fastener Type Design Check Resistance per Fastener
Self-drilling screw Shear, pull-out, pull-over 2-8 kN per screw
Power actuated fastener Shear, tension 3-12 kN per fastener
Bolted connection Bearing, shear Per CSA S16 provisions
Welded connection Fusion weld Per CSA W59 provisions

Screw Spacing and Edge Distance

Frequently Asked Questions

What is the difference between CSA S136 and CSA S16 for steel design? CSA S136 (cold-formed steel) is used for light-gauge members (t = 0.84-6.0 mm) that are formed at room temperature. Design uses the effective width method to account for local and distortional buckling. CSA S16 (hot-rolled steel) is used for heavier sections and uses plastic/elastic section properties with section classification (Class 1-4). CSA S136 addresses distortional buckling (unique to cold-formed sections with lip stiffeners), which CSA S16 does not cover.

What is the effective width method in cold-formed steel design? The effective width method accounts for local buckling by reducing the width of compression elements. Per CSA S136 Clause B2, the effective width be = w × (1 - 0.22/lambda_p)/lambda_p when lambda_p > 0.673. This means the centre portion of a slender compression element is assumed to buckle and carry no stress, while the edges near the supports carry stress up to Fy. The reduced section properties are calculated using the effective widths of all compression elements.

What is distortional buckling in cold-formed steel? Distortional buckling is a buckling mode unique to cold-formed sections with edge stiffeners (lips). The compression flange and lip rotate about the flange-web junction, while the web remains straight. Unlike local buckling (where the flange buckles between lip and web), distortional buckling involves the whole flange-lip assembly. CSA S136 Clause B3.2 provides the distortional buckling check, which often governs for intermediate flange slenderness.

What fasteners are used in cold-formed steel construction in Canada? Self-drilling screws are the most common fasteners (Nos. 8-14, with No. 12 being standard for structural connections). Power-actuated fasteners (powder-actuated or gas-actuated) are used for connections to concrete or steel supports. Bolted connections (M6-M12) are used for heavy connections with thicker material. Welding is less common in cold-formed construction due to the thin material but is permitted per CSA W59 for t ≥ 1.5 mm.

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This page is for educational reference. Cold-formed steel design per CSA S136-19. Verify effective width calculations and buckling modes with analysis software. Results are PRELIMINARY — NOT FOR CONSTRUCTION without independent PE/SE verification.

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