The UA 125×75×12 is a steel section with a mass of 17.8 kg/m, an overall depth of 125 mm and width of 75 mm. It has a cross-sectional area of 22.7 cm², a second moment of area Iᵧ of 355 cm⁴, an elastic modulus Wₑₗ,ᵧ of 43.4 cm³, tabulated by CivilAxis from EN 10056 · Continental Steel.
Mass
17.8 kg/m
Depth
125 mm
Width
75 mm
Area
22.7 cm²
Ask about capacity, buckling or detailing for UA 125×75×12.
Dimension symbols for Unequal Angle sections. Not to scale.
UA 125×75×12 section properties to EN 10056 · Continental Steel.
Geometry
Depth of section
h
125
Width of section
b
75
Web thickness
tw
12
Flange thickness
tf
12
Root fillet radius
r
11
Toe radius
r2
4.8
Mass and area
Mass per metre
mass
17.8
Cross-sectional area
A
22.7
Bending about the major axis (y-y)
Area moment of inertia about y-axis
Iy
355
Elastic section modulus about y-axis
Wel,y
43.4
Radius of gyration about y-axis
iy
3.95
Bending about the minor axis (z-z)
Area moment of inertia about z-axis
Iz
96
Elastic section modulus about z-axis
Wel,z
17
Radius of gyration about z-axis
iz
2.06
Principal axes
Area moment of inertia about u-u (major principal) axis
Iu
392
Area moment of inertia about v-v (minor principal) axis
Iv
58.8
Radius of gyration about u-u axis
iu
4.16
Radius of gyration about v-v axis
iv
1.61
Elastic section modulus about u-u axis
Wel,u
43.4
Elastic section modulus about v-v axis
Wel,v
17
Detailing dimensions
Centroid distance from back of leg (y)
cy
4.32
Centroid distance from back of leg (z)
cz
1.84
Common questions about UA 125×75×12
UA 125×75×12 has a mass of 17.8 kg/m, tabulated to EN 10056. A 12 m length therefore weighs about 214 kg, which is the figure to use for a steel take-off or when checking a lift.
UA 125×75×12 has a depth of 125 mm, a width of 75 mm, a web thickness of 12 mm, a flange thickness of 12 mm, with a cross-sectional area of 22.7 cm². These are the nominal dimensions from EN 10056; rolling tolerances apply to the delivered section.
The elastic section modulus about the major axis, Wel,y, is 43.4 cm³. Angles are tabulated about their principal (u-u and v-v) axes rather than a plastic major-axis modulus, so the elastic value is the one to design from unless you are working from the principal-axis properties directly.
The second moment of area about the major axis, Iy, is 355 cm⁴, and about the minor axis Iz is 96 cm⁴. Iy is the value deflection depends on - for a simply supported beam under a uniform load, the midspan deflection is 5wL⁴/384EIy - so on spans where a deflection limit governs rather than strength, this is the number that decides the section.
iy is 3.95 cm about the major axis and iz is 2.06 cm about the minor axis. Column buckling is governed by the SMALLER value: the slenderness is lambda = L_cr / i, so with iz = 2.06 cm a 0.2 m effective length already gives lambda = 100. Minor-axis buckling almost always controls unless the weak axis is restrained.
