Steel Section Properties

European (EN 10365), American (AISC), and Indian (IS 808) standard section databases, plus custom section calculator.

📒 Section Properties — Geometry, Formulas & Diagrams

I / H Section IPE · HEA · HEB · HEM · W · S · ISMB · ISLB

Doubly symmetric open section. Strong axis (y-y) is horizontal — the flanges carry most of the bending moment. Weak axis (z-z) is vertical. The web resists shear. Widely used for beams and columns.

b h tf tw hw y z
Dimensions
hw = h − 2·tf    (clear web height)
PropertyFormula (simplified, no root radius)Unit
A2·b·tf + hw·twmm²
Iy(b·h³ − (b−tw)·hw³) / 12  ← strong axismm⁴
Iz(2·tf·b³ + hw·tw³) / 12  ← weak axismm⁴
Wel,yIy / (h/2)mm³
Wel,zIz / (b/2)mm³
Wpl,ytw·hw²/4 + b·tf·(hw+tf)mm³
Wpl,zb²·tf/2 + tw²·hw/4mm³
iy√(Iy / A)mm
iz√(Iz / A)mm
IT(2·b·tf³ + hw·tw³) / 3  (St. Venant, open)mm⁴

Tabulated values include root-radius fillet correction (reduces A by ~1–3%). Warping constant Iw requires numerical integration.

Channel Section UPN · UPE · C · MC · ISMC · ISSC

Singly symmetric open section. Centroid displaced from web toward flanges (ez). Shear center lies outside the section on the open side. Pure bending about the strong y-y axis avoids torsion; about the weak z-z axis, torsion is induced unless load passes through the shear center.

b h tf tw ez y z
Centroid from back of web (ez)
ez = (b²·tf + hw·tw²/2) / A
Centroid is closer to the web than the flange tip mid-point.
PropertyFormulaUnit
hwh − 2·tfmm
A2·b·tf + hw·twmm²
Iy(b·h³ − (b−tw)·hw³) / 12  ← strong axismm⁴
IzParallel axis theorem about ez:
= 2(tf·b³/12 + b·tf·(b/2−ez)²) + hw·tw³/12 + hw·tw·(tw/2−ez)²  ← weak axis
mm⁴
Wel,yIy / (h/2)mm³
Wel,z,maxIz / (b − ez)  (flange tip)mm³
Wel,z,minIz / ez  (back of web)mm³
iy√(Iy/A)mm
iz√(Iz/A)mm
Shear Center (S)
eS = 3·tf·b² / (h·tw + 6·tf·b)  from back of web (approx., uniform thickness)
Load must pass through the shear center to avoid torsion. For UPN/C sections, shear center lies outside the section on the open side.

Equal Angle L (EU) · L (AISC) · ISA Equal

Doubly symmetric about the 45° diagonal (principal axes u-u and v-v). The conventional legs axis (y-y, z-z) are NOT the principal axes — they are at 45° to them. The minimum radius of gyration iv governs buckling in compression members.

u v a t ȳ = z̄
Centroid (equal legs, from outer corner)
ȳ = z̄ = (a²·t − t²·(a−t)/2) / A ≈ (2·a−t) / 4  (approx.)
PropertyFormulaUnit
At·(2a − t)mm²
Iy = Izt·(a³ − (a−t)²·t/2 − (2a−t)·ȳ²)  (about centroidal leg axes)mm⁴
IuIy + Iyz  (max principal — u-u axis at +45°)mm⁴
IvIy − Iyz  (min principal — v-v axis at −45°)mm⁴
Iyz−t·(a−t)·(ȳ − t/2)·(z̄ − t/2)  (product of inertia)mm⁴
iu√(Iu/A)mm
iv√(Iv/A)  ← governs bucklingmm
ITt³·(2a−t) / 3  (St. Venant, thin-walled open)mm⁴

For equal legs: Iyz = −(Iu−Iv)/2. Principal axes u-u and v-v are at 45° to the legs. The minimum second moment of area Iv is approximately half of Iu.

Square Hollow Section (SHS) SHS (EN) · HSS Square (AISC)

Doubly symmetric closed section. Highly efficient in torsion (closed path → Bredt's formula). Equal Iy = Iz. Used for columns and members under combined bending and torsion.

a t ai Am
Key dimensions
ai = a − 2t  (inner side length)    Am = (a−t)²  (mid-line enclosed area, Bredt)
PropertyFormulaUnit
Aa² − ai² = 4t·(a−t)mm²
Iy = Iz(a⁴ − ai⁴) / 12mm⁴
WelI / (a/2)mm³
Wpl(a³ − ai³) / 6mm³
i√(I/A)mm
IT4·Am² / (4(a−t)/t) = t·(a−t)³  (Bredt, closed)mm⁴
WTIT / (a/2)  (torsion section modulus)mm³
Comparison: Closed vs Open section torsion
For open section (same area): IT,open = 4t³·a / 3
For closed SHS: IT,closed = t·(a−t)³
Ratio ≈ (a/t)² / 4 — closed section is far stiffer in torsion.
For SHS 100×100×5: IT,closed/IT,open ≈ (100/5)²/4 = 100× stiffer.

Rectangular Hollow Section (RHS) RHS (EN) · HSS Rect. (AISC)

Doubly symmetric closed section with different strong (h) and weak (b) axis properties. Excellent for beams under biaxial bending or combined bending and torsion. Bredt's formula gives the torsional constant.

b h t
Key dimensions
hi = h − 2t  (inner height)    bi = b − 2t  (inner width)
Am = (h−t)·(b−t)  (mid-line enclosed area, Bredt's formula)
PropertyFormulaUnit
Ab·h − bi·himm²
Iy(b·h³ − bi·hi³) / 12  ← strong axismm⁴
Iz(h·b³ − hi·bi³) / 12  ← weak axismm⁴
Wel,yIy / (h/2)mm³
Wel,zIz / (b/2)mm³
Wpl,y(b·h² − bi·hi²) / 4mm³
Wpl,z(h·b² − hi·bi²) / 4mm³
iy√(Iy/A)mm
iz√(Iz/A)mm
IT2·t·(h−t)²·(b−t)² / (h+b−2t)  (Bredt, closed)mm⁴

Circular Hollow Section (CHS) CHS (EN) · HSS Round (AISC)

Doubly (fully) symmetric closed section. Equal bending stiffness in all directions: Iy = Iz. Most efficient shape for pure torsion. The torsional constant IT = Ip (polar moment of area), exact (not approximate).

D t Di
Key dimensions
Di = D − 2t  (inner diameter)
PropertyFormulaUnit
Aπ·(D² − Di²)/4 = π·t·(D−t)mm²
Iy = Izπ·(D⁴ − Di⁴) / 64  ← equal both axesmm⁴
WelI / (D/2) = π·(D⁴−Di⁴) / (32·D)mm³
Wpl(D³ − Di³) / 6mm³
i√(I/A) = √(D²+Di²) / 4mm
Ipπ·(D⁴ − Di⁴) / 32 = 2·I  (polar moment)mm⁴
ITIp = 2·I  (exact — closed circular section)mm⁴
WTIT / (D/2) = π·(D⁴−Di⁴) / (16·D)mm³
Why IT = Ip for CHS (exact, not approximate)
For circular cross-sections, the shear stress distribution under torsion is exactly linear — plane sections remain plane and warping is zero. Bredt's formula and the exact torsion formula coincide. This is unique to circular sections; all other closed sections require numerical corrections.

Structural Steel Profile Matrix & Section Property Tables

This section provides structural steel cross-sectional tables for immediate geometric and mechanical parameter lookup across three major global standards. The interactive database allows engineers to filter and compare profile dimensions — cross-sectional area (A), second moment of area (I), elastic section modulus (Wel), plastic section modulus (Wpl), radius of gyration (i), and torsional constants — across European, American, and Indian section catalogs.

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