The EA 175×175×15 is a steel section with a mass of 39.4 kg/m, an overall depth of 175 mm and width of 175 mm. It has a cross-sectional area of 50.7 cm², a second moment of area Iᵧ of 1474 cm⁴, an elastic modulus Wₑₗ,ᵧ of 117 cm³, tabulated by CivilAxis from EN 10056 · Continental Steel.
Mass
39.4 kg/m
Depth
175 mm
Width
175 mm
Area
50.7 cm²
Ask about capacity, buckling or detailing for EA 175×175×15.
Dimension symbols for Equal Angle sections. Not to scale.
EA 175×175×15 section properties to EN 10056 · Continental Steel.
Geometry
Depth of section
h
175
Width of section
b
175
Web thickness
tw
15
Flange thickness
tf
15
Root fillet radius
r
16
Toe radius
r2
4.8
Mass and area
Mass per metre
mass
39.4
Cross-sectional area
A
50.7
Bending about the major axis (y-y)
Area moment of inertia about y-axis
Iy
1474
Elastic section modulus about y-axis
Wel,y
117
Radius of gyration about y-axis
iy
5.39
Bending about the minor axis (z-z)
Area moment of inertia about z-axis
Iz
1474
Elastic section modulus about z-axis
Wel,z
117
Radius of gyration about z-axis
iz
5.39
Principal axes
Area moment of inertia about u-u (major principal) axis
Iu
2342
Area moment of inertia about v-v (minor principal) axis
Iv
606
Radius of gyration about u-u axis
iu
6.8
Radius of gyration about v-v axis
iv
3.46
Elastic section modulus about u-u axis
Wel,u
117
Elastic section modulus about v-v axis
Wel,v
117
Detailing dimensions
Centroid distance from back of leg (y)
cy
4.89
Centroid distance from back of leg (z)
cz
4.89
Common questions about EA 175×175×15
EA 175×175×15 has a mass of 39.4 kg/m, tabulated to EN 10056. A 12 m length therefore weighs about 473 kg, which is the figure to use for a steel take-off or when checking a lift.
EA 175×175×15 has a depth of 175 mm, a width of 175 mm, a web thickness of 15 mm, a flange thickness of 15 mm, with a cross-sectional area of 50.7 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 117 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 1,474 cm⁴, and about the minor axis Iz is 1,474 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 5.39 cm about the major axis and iz is 5.39 cm about the minor axis. Column buckling is governed by the SMALLER value: the slenderness is lambda = L_cr / i, so with iz = 5.39 cm a 0.5 m effective length already gives lambda = 100. Minor-axis buckling almost always controls unless the weak axis is restrained.
