Guides · EN 1993-1-2

Reduction factors for steel in fire

How much of the strength and stiffness of steel remains at elevated temperatures, and how that shows in buckling.

Properties of carbon steel at elevated temperatures

EN 1993-1-2 (cl. 3.2.1, Table 3.1) expresses the mechanical properties of steel at temperature θa as fractions of their values at 20 °C:

θa [°C]ky,θ (yield)kp,θ (proportional)kE,θ (elastic)
201.0001.0001.000
1001.0001.0001.000
2001.0000.8070.900
3001.0000.6130.800
4001.0000.4200.700
5000.7800.3600.600
6000.4700.1800.310
7000.2300.0750.130
8000.1100.0500.090
9000.0600.03750.0675
10000.0400.02500.0450
11000.0200.01250.0225
12000.0000.00000.0000

Intermediate temperatures are interpolated linearly. The yield strength is fully retained up to 400 °C, then drops from 78% to 23% between 500 and 700 °C. The modulus of elasticity starts dropping from 100 °C and, above 500 °C, falls faster than the yield strength.

The buckling reduction factor in fire χfi

For compression members (cl. 4.2.3.2) and lateral-torsional buckling (cl. 4.2.3.3), EN 1993-1-2 uses a single buckling curve regardless of the section shape:

χfi = 1 / [ φθ + √(φθ² − λ̄θ²) ]    φθ = ½ · [ 1 + α · λ̄θ + λ̄θ² ]    α = 0.65 · √(235 / fy)
λ̄θ = λ̄ · √(ky,θ / kE,θ) non-dimensional slenderness at temperature θa

Values of χfi as a function of λ̄θ:

λ̄θS235S275S355S460
0.20.8810.8890.9010.912
0.40.7710.7840.8050.824
0.60.6610.6770.7020.726
0.80.5540.5690.5940.619
1.00.4560.4690.4910.512
1.20.3730.3830.4000.417
1.40.3060.3140.3270.340
1.60.2530.2590.2690.279
1.80.2120.2160.2240.231
2.00.1790.1830.1890.194

Unlike the normal-temperature design, there is no plateau for low slenderness: even at λ̄θ = 0.2 the resistance drops by about 10%. The factor α depends on the steel grade, so higher-strength steels have slightly higher χfi values at the same slenderness.

Why slenderness increases in fire

The ratio ky,θ / kE,θ is greater than one between 200 and 800 °C. For example, at 600 °C it is 0.47 / 0.31 = 1.52, so the slenderness grows by √1.52 ≈ 1.23. Thus, a column with λ̄ = 0.8 at normal temperature reaches a value of λ̄θ ≈ 0.98 at 600 °C.

Informative material summarising the provisions of EN 1993-1-2. It does not replace the text of the standard, the National Annex or verification by a qualified engineer.

Slenderness and χfi are computed for you, about both axes.

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