Free Moment of Inertia Calculator

Calculate the second moment of area (moment of inertia) for common cross-sections. Enter dimensions below to get Iyy, Izz, and cross-sectional area instantly.

Moment of Inertia Calculator

What is Moment of Inertia?

The moment of inertia (more precisely, the second moment of area) measures how a cross-section's area is distributed relative to an axis. It determines how much a beam will bend under load-the higher the moment of inertia, the stiffer the beam.

Engineers use two main axes: the strong axis (typically z-z, giving Izz) and the weak axis (typically y-y, giving Iyy). For symmetric sections like circles and squares, these are equal. For I-beams, Izz is much larger than Iyy-that's why I-beams are oriented with the web vertical.

Formulas Used

Solid Rectangle

Izz = bh³/12
Iyy = hb³/12
A = bh

Where b is width and h is height. The moment of inertia increases with the cube of the dimension perpendicular to the bending axis-doubling the height increases Izz by a factor of 8.

Solid Circle

I = πd⁴/64
A = πd²/4

For a circle, both axes have equal moment of inertia. The formula can also be written as I = πr⁴/4 using the radius.

Hollow Rectangle (RHS/SHS)

Izz = (BH³ - bh³)/12
Iyy = (HB³ - hb³)/12
A = BH - bh

Subtract the hollow portion from the outer rectangle. B×H are outer dimensions, b×h are inner dimensions.

Hollow Circle (CHS/Pipe)

I = π(D⁴ - d⁴)/64
A = π(D² - d²)/4

D is outer diameter, d is inner diameter. Alternatively, use D and wall thickness t, where d = D - 2t.

I-Beam / H-Section

Izz = (BH³ - (B-tw)hw³)/12
Iyy = (2tfB³ + hwtw³)/12
A = 2Btf + hwtw

Where hw = H - 2tf is the web height. This simplified formula ignores fillet radii-for precise values, use our full section properties calculator or look up tabulated values.

Channel (C-Section)

Izz = (BH³ - (B-tw)hw³)/12
Iyy = requires parallel axis theorem (centroid is offset from web)

A channel has the same Izz formula as an I-beam (both are symmetric about the strong axis). However, Iyy requires finding the centroid position from the web back and applying the parallel axis theorem, since the flanges extend to one side only.

Tee (T-Section)

ȳ = (Aw·hw/2 + Af·(hw+tf/2)) / A
Izz = Σ(Ii + Ai·di²) about centroid
Iyy = (hwtw³ + tfB³)/12

A tee section is not symmetric about the strong axis, so the centroid must be calculated first. Izz then uses the parallel axis theorem for both the web and flange. Iyy is straightforward since the section is symmetric about the vertical axis.

Angle (L-Section)

Izz, Iyy = parallel axis theorem about geometric centroid

Angles are not symmetric about either axis, so both the centroid and the parallel axis theorem are needed for both Izz and Iyy. Note these are geometric-axis properties. For buckling calculations, principal-axis properties (rotated) may be required-use the section properties calculator for those.

Why Moment of Inertia Matters

The moment of inertia appears in two fundamental beam equations:

Bending stress: σ = My/I
Deflection: δ ∝ 1/(EI)

Higher I means lower stress for the same moment, and less deflection for the same load. This is why efficient structural sections (I-beams, channels, hollow sections) concentrate material away from the neutral axis-maximising I while minimising weight.

Need More Section Properties?

This calculator provides the essential properties: area and moment of inertia. For complete section analysis including torsion constant (J), section modulus (S), warping constant (Iw), and centroid location, use our full structural analysis tool with its comprehensive section library.

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