EN 1993-1-1 Column Buckling Capacity — Verification Benchmark
Complete hand calculation of a UC 152x152x30 column buckling capacity against the Steel Calculator WASM engine, matched to EN 1993-1-1:2005 Clause 6.3.1.
PRELIMINARY — NOT FOR CONSTRUCTION. All results are for educational and reference use only. Must be independently verified by a licensed Chartered Engineer (CEng) or Professional Engineer (PE/SE) before use in any project.
Problem Statement
Member: UC 152x152x30, steel grade S275 (fy = 275 MPa, fu = 430 MPa) Length: L = 4.0 m, pinned-pinned about both axes (effective length factor k = 1.0) Objective: Determine the design buckling resistance Nb,Rd about the weak (z-z) axis per EN 1993-1-1
Section Properties — UC 152x152x30
| Property | Value | Property | Value |
|---|---|---|---|
| h | 157.6 mm | A | 38.3 cm^2 |
| b | 152.9 mm | iy | 6.76 cm |
| tw | 6.5 mm | iz | 3.83 cm |
| tf | 9.4 mm | Wy,pl | 247 cm^3 |
| r | 7.6 mm | Iz | 562 cm^4 |
| h/b | 1.03 | tf (max) | 9.4 mm |
Hand Calculation — EN 1993-1-1, Clause 6.3.1
Step 1: Material Parameters
Per EN 1993-1-1 Clause 3.2.6:
epsilon = sqrt(235 / fy) = sqrt(235 / 275) = sqrt(0.8545) = 0.9244
lambda_1 = 93.9 * epsilon = 93.9 * 0.9244 = 86.80
Step 2: Effective Length and Slenderness
Lcr = k * L = 1.0 * 4.0 m = 4,000 mm
lambda_bar = (Lcr / iz) / lambda_1
= (4,000 / 38.3) / 86.80
= 104.44 / 86.80
= 1.203
Step 3: Buckling Curve Selection — EN 1993-1-1 Table 6.2
For hot-rolled H-section UC 152x152x30:
- h/b = 1.03 <= 1.2
- tf = 9.4 mm <= 100 mm
- Buckling about z-z axis (minor axis)
Per Table 6.2: Buckling curve c, imperfection factor alpha = 0.49.
Step 4: Reduction Factor chi — EN 1993-1-1 Clause 6.3.1.2
Phi = 0.5 * [1 + alpha * (lambda_bar - 0.2) + lambda_bar^2]
= 0.5 * [1 + 0.49 * (1.203 - 0.2) + (1.203)^2]
= 0.5 * [1 + 0.49 * 1.003 + 1.447]
= 0.5 * [1 + 0.4915 + 1.4472]
= 0.5 * 2.9387
= 1.4694
chi = 1 / (Phi + sqrt(Phi^2 - lambda_bar^2))
= 1 / (1.4694 + sqrt(1.4694^2 - 1.203^2))
= 1 / (1.4694 + sqrt(2.1591 - 1.4472))
= 1 / (1.4694 + sqrt(0.7119))
= 1 / (1.4694 + 0.8437)
= 1 / 2.3131
= 0.4323
Check: chi <= 1.0 âÃÂÃÂ. The reduction accounts for the member imperfection and residual stress captured by the Ayrton-Perry formulation underlying the European buckling curves.
Step 5: Design Buckling Resistance
Per EN 1993-1-1 Clause 6.3.1.1(3):
Nb,Rd = chi * A * fy / gamma_M1
= 0.4323 * 3,830 * 275 / 1.00
= 0.4323 * 1,053,250
= 455,400 N
= 455.4 kN
Step 6: Cross-Section Check — Clause 6.3.1.1(1)
Per Clause 6.3.1.1(1), the design buckling resistance of a compression member:
N_Ed / Nb,Rd <= 1.0
For an applied axial load N_Ed = 300 kN:
Utilization = 300 / 455.4 = 0.659 âÃÂàPASS at 65.9%
WASM Output Comparison
The Steel Calculator WASM engine (EN 1993 region), run with identical inputs:
| Quantity | Hand Calculation | WASM Output | Difference |
|---|---|---|---|
| epsilon | 0.9244 | 0.9244 | 0.00% |
| lambda_1 | 86.80 | 86.80 | 0.00% |
| Lcr (mm) | 4,000 | 4,000 | 0.00% |
| lambda_bar | 1.203 | 1.203 | 0.00% |
| Buckling curve | c | c | Match |
| alpha | 0.49 | 0.49 | Match |
| Phi | 1.469 | 1.469 | 0.00% |
| chi | 0.4323 | 0.4323 | 0.00% |
| Nb,Rd (kN) | 455.4 | 455.4 | 0.00% |
| Utilization (at 300 kN) | 0.659 | 0.659 | 0.00% |
| Verdict | PASS | PASS | Match |
All 10 quantities match within 0.00%. The EN 1993 buckling calculation is exact — there are no rounding-sensitive intermediate values in this example.
Sensitivity Check — What If the Axial Load Exceeds Capacity?
The WASM engine correctly identifies overloaded members. For N_Ed = 500 kN:
| Quantity | Hand Calc (N_Ed=500) | WASM (N_Ed=500) |
|---|---|---|
| Nb,Rd (kN) | 455.4 | 455.4 |
| Utilization | 1.098 | 1.098 |
| Verdict | FAIL | FAIL |
| Failure clause | 6.3.1.1(3) | 6.3.1.1(3) |
Code References — EN 1993-1-1:2005
| Clause | Title | Application |
|---|---|---|
| 3.2.6 | Design values of material coefficients | fy, fu, E for S275 |
| 6.3.1.1(1) | Uniform members in compression | Scope and N_Ed / Nb,Rd <= 1.0 |
| 6.3.1.1(3) | Buckling resistance formula | Nb,Rd = chiAfy/gamma_M1 |
| 6.3.1.2(1) | Reduction factor chi | Ayrton-Perry formulation |
| 6.3.1.2(2) | Phi parameter | 0.5[1+alpha*(lambda_bar-0.2)+lambda_bar^2] |
| 6.3.1.3 | Non-dimensional slenderness | lambda_bar formula |
| Table 6.2 | Buckling curves and imperfection factors | alpha values per curve |
| UK NA.2.4 | National Annex — gamma_M1 | UK NA: gamma_M1 = 1.00 |
How to Reproduce
- Navigate to the Steel Calculator Column Capacity tool
- Select EN 1993-1-1 as the design code
- Enter: UC 152x152x30, S275, L=4.0m, k=1.0 for weak axis
- Enter axial load N_Ed = 300 kN
- Click Calculate — the WASM engine produces the output shown above
The WASM engine also handles the full Eurocode capacity check including cross-section classification to EN 1993-1-1 Clause 5.5, not just buckling alone.
Why Verification Matters
Structural engineering software must produce correct results. Every calculation engine powering Steel Calculator is verified against published textbook examples, SCI (Steel Construction Institute) design guides for Eurocode 3, and independent hand calculations. These verification pages are public, reproducible evidence of accuracy for all supported design codes.
See also: AISC Beam Verification, AS 4100 Bolt Verification, CSA Weld Verification, AISC Base Plate Verification.
Last verified: 2026-05-08. WASM version: core-wasm-v2 stage-4-member-design. Tolerance standard: all quantities within 1.0% of hand calculation or textbook published value. EN 1993 gamma_M values per UK National Annex.
Disclaimer: This content is for educational purposes only. Results must be verified by a licensed professional engineer. Steel Calculator provides preliminary design tools — NOT a substitute for professional engineering judgment.