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Area moment de inertia — typical cross sections

Formulas et values pour area moment de inertia de common cross sections.

areamomentinertia

Overview

The area moment of inertia (also called second moment of area) is a geometric property of a cross section that describes its resistance to bending. It appears in the flexure formula:

σ=MyI\sigma = \frac{M \cdot y}{I}

where:

  • σ\sigma = bending stress (Pa)
  • MM = bending moment (N·m)
  • yy = distance from the neutral axis (m)
  • II = area moment of inertia (m⁴)

A larger moment of inertia means a stiffer beam — more resistant to deflection under load.

Parallel Axis Theorem

The moment of inertia about any axis parallel to the centroidal axis:

I=Icentroid+Ad2I = I_{centroid} + A \cdot d^2

where:

  • AA = cross-sectional area
  • dd = distance between the two parallel axes

Section Modulus

The elastic section modulus relates moment of inertia to the maximum bending stress:

S=IcS = \frac{I}{c}

where cc is the distance from the neutral axis to the extreme fiber.

Common Cross Sections

9 lignes
Area moment of inertia formulas for common cross sections
Cross Section
Area (A)
Moment of Inertia Ix
Section Modulus Sx
Rectangle (b × h)b·hb·h³ / 12b·h² / 6
Square (a × a)a⁴ / 12a³ / 6
Solid Circle (diameter d)π·d² / 4π·d⁴ / 64π·d³ / 32
Hollow Circle (D outer, d inner)π(D² − d²) / 4π(D⁴ − d⁴) / 64π(D⁴ − d⁴) / (32·D)
I-Beam (B×H outer, b×h web)B·H − b·h(B·H³ − b·h³) / 12(B·H³ − b·h³) / (6·H)
Triangle (base b, height h)b·h / 2b·h³ / 36b·h² / 24
Semicircle (radius r)π·r² / 2r⁴(π/8 − 8/(9π))
Thin-Wall Tube (r mean, t wall)2·π·r·tπ·r³·tπ·r²·t
Ellipse (semi-axes a, b)π·a·bπ·a·b³ / 4π·a·b² / 4

Standard Steel Shapes — Example Values

11 lignes
Properties of standard European IPE and HEB steel sections
Section
Depth (mm)
Width (mm)
Ix (10⁶ mm⁴)
Sx (10³ mm³)
Mass (kg/m)
IPE 100100551.7134.28.1
IPE 20020010019.419422.4
IPE 30030015083.655742.2
IPE 400400180231116066.3
IPE 500500200482193090.7
IPE 6006002209213070122
HEB 1001001004.5089.920.4
HEB 20020020057.057061.3
HEB 3003003002521680117
HEB 4004003005772880155
HEB 50050030010724290187

Beam Deflection

The maximum deflection of a simply supported beam with uniform load:

δmax=5wL4384EI\delta_{max} = \frac{5 \cdot w \cdot L^4}{384 \cdot E \cdot I}

where:

  • ww = load per unit length (N/m)
  • LL = span (m)
  • EE = modulus of elasticity (Pa)
  • II = moment of inertia (m⁴)

Applications

  • Structural beam and column design
  • Machine component sizing
  • Bridge and building analysis
  • Crane and hoist engineering
  • Aerospace structural analysis