Section Properties: Centroid and Moment of Inertia Formulas

Area, centroid and second moment of area (moment of inertia) formulas for 27 cross sections, from basic shapes to structural steel profiles. The moment of inertia about the centroidal axes is what you need for bending stresses and deflections.

Open any section for its full set of properties (inertia about the base, plastic modulus, torsional constant), or press Calculate to get the values for your dimensions.

Basic shapes

SectionAreaCentroidInertia about x̄Inertia about ȳ
SquareSquare
A=l2A = l^2
xˉ=l2\bar{x} = \frac{l}{2}
yˉ=l2\bar{y} = \frac{l}{2}
Iˉx=l412\bar{I}_x = \frac{l^4}{12}
Iˉy=l412\bar{I}_y = \frac{l^4}{12}
Calculate
Diamond SquareDiamond Square
A=l2A = l^2
xˉ=l2\bar{x} = \frac{l}{\sqrt{2}}
yˉ=l2\bar{y} = \frac{l}{\sqrt{2}}
Iˉx=l412\bar{I}_x = \frac{l^4}{12}
Iˉy=l412\bar{I}_y = \frac{l^4}{12}
Calculate
RectangleRectangle
A=bhA = b h
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=h2\bar{y} = \frac{h}{2}
Iˉx=bh312\bar{I}_x = \frac{b h^3}{12}
Iˉy=b3h12\bar{I}_y = \frac{b^3 h}{12}
Calculate
Rotated RectangleRotated Rectangle
A=bhA = b h
xˉ=bcos⁡(θ)+hsin⁡(θ)2\bar{x} = \frac{b \cos(\theta) + h \sin(\theta)}{2}
yˉ=bsin⁡(θ)+hcos⁡(θ)2\bar{y} = \frac{b \sin(\theta) + h \cos(\theta)}{2}
Iˉx=bh12(b2sin⁡2(θ)+h2cos⁡2(θ))\bar{I}_x = \frac{b h}{12} (b^2 \sin^2(\theta) + h^2 \cos^2(\theta))
Iˉy=bh12(b2cos⁡2(θ)+h2sin⁡2(θ))\bar{I}_y = \frac{b h}{12} (b^2 \cos^2(\theta) + h^2 \sin^2(\theta))
Calculate
TriangleTriangle
A=bh2A = \frac{b h}{2}
xˉ=a+b3\bar{x} = \frac{a + b}{3}
yˉ=h3\bar{y} = \frac{h}{3}
Iˉx=bh336\bar{I}_x = \frac{b h^3}{36}
Iˉy=bh(a2−ab+b2)36\bar{I}_y = \frac{bh(a^2-ab+b^2)}{36}
Calculate
Isosceles TrapezoidIsosceles Trapezoid
A=h(a+b)2A = \frac{h(a + b)}{2}
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=h(2a+b)3(a+b)\bar{y} = \frac{h(2a + b)}{3(a + b)}
Iˉx=h3(a2+4ab+b2)36(a+b)\bar{I}_x = \frac{h^3(a^2 + 4ab + b^2)}{36(a + b)}
Iˉy=h(a+b)(a2+b2)48\bar{I}_y = \frac{h(a + b)(a^2 + b^2)}{48}
Calculate
General TrapezoidGeneral Trapezoid
A=h(a+b)2A = \frac{h(a + b)}{2}
xˉ=a2+ab+2ac+b2+bc3(a+b)\bar{x} = \frac{a^2 + ab + 2ac + b^2 + bc}{3(a + b)}
yˉ=h(2a+b)3(a+b)\bar{y} = \frac{h(2a + b)}{3(a + b)}
Iˉx=h3(a2+4ab+b2)36(a+b)\bar{I}_x = \frac{h^3(a^2 + 4ab + b^2)}{36(a + b)}
Iˉy=Iy−xˉ2A\bar{I}_y = I_y - \bar{x}^2 A
Calculate

Circular shapes

SectionAreaCentroidInertia about x̄Inertia about ȳ
CircleCircle
A=πr2A = \pi r^2
xˉ=r\bar{x} = r
yˉ=r\bar{y} = r
Iˉx=πr44\bar{I}_x = \frac{\pi r^4}{4}
Iˉy=πr44\bar{I}_y = \frac{\pi r^4}{4}
Calculate
Half CircleHalf Circle
A=πr22A = \frac{\pi r^2}{2}
xˉ=0\bar{x} = 0
yˉ=4r3π\bar{y} = \frac{4r}{3\pi}
Iˉx=(π8−89π)r4\bar{I}_x = \left(\frac{\pi}{8} - \frac{8}{9\pi}\right) r^4
Iˉy=πr48\bar{I}_y = \frac{\pi r^4}{8}
Calculate
Quarter CircleQuarter Circle
A=πr24A = \frac{\pi r^2}{4}
xˉ=4r3π\bar{x} = \frac{4r}{3\pi}
yˉ=4r3π\bar{y} = \frac{4r}{3\pi}
Iˉx=(π16−49π)r4\bar{I}_x = \left(\frac{\pi}{16} - \frac{4}{9\pi}\right) r^4
Iˉy=(π16−49π)r4\bar{I}_y = \left(\frac{\pi}{16} - \frac{4}{9\pi}\right) r^4
Calculate
Circle SectorCircle Sector
A=θr22A = \frac{\theta r^2}{2}
xˉ=4rsin⁡(θ/2)3θ\bar{x} = \frac{4r \sin(\theta/2)}{3\theta}
yˉ=0\bar{y} = 0
Iˉx=r4(θ−sin⁡θ)8\bar{I}_x = \frac{r^4(\theta - \sin\theta)}{8}
Iˉy=Iy−xˉ2A\bar{I}_y = I_y - \bar{x}^2 A
Calculate

Hollow and thin-walled sections

SectionAreaCentroidInertia about x̄Inertia about ȳ
Hollow RectangleHollow Rectangle
A=bh−bihiA = b h - b_i h_i
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=h2\bar{y} = \frac{h}{2}
Iˉx=bh312−bihi312\bar{I}_x = \frac{b h^3}{12} - \frac{b_i h_i^3}{12}
Iˉy=b3h12−bi3hi12\bar{I}_y = \frac{b^3 h}{12} - \frac{b_i^3 h_i}{12}
Calculate
Thin-Walled RectangleThin-Walled Rectangle
A=bh−bihiA = b h - b_i h_i
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=h2\bar{y} = \frac{h}{2}
Iˉx=bh312−bihi312\bar{I}_x = \frac{b h^3}{12} - \frac{b_i h_i^3}{12}
Iˉy=b3h12−bi3hi12\bar{I}_y = \frac{b^3 h}{12} - \frac{b_i^3 h_i}{12}
Calculate
Hollow CircleHollow Circle
A=π(R2−r2)A = \pi (R^2 - r^2)
xˉ=R\bar{x} = R
yˉ=R\bar{y} = R
Iˉx=π4(R4−r4)\bar{I}_x = \frac{\pi}{4} (R^4 - r^4)
Iˉy=π4(R4−r4)\bar{I}_y = \frac{\pi}{4} (R^4 - r^4)
Calculate
Thin-Walled CircleThin-Walled Circle
A=π(R2−r2)A = \pi (R^2 - r^2)
xˉ=R\bar{x} = R
yˉ=R\bar{y} = R
Iˉx=π4(R4−r4)\bar{I}_x = \frac{\pi}{4} (R^4 - r^4)
Iˉy=π4(R4−r4)\bar{I}_y = \frac{\pi}{4} (R^4 - r^4)
Calculate

Regular polygons

SectionAreaCentroidInertia about x̄Inertia about ȳ
HexagonHexagon
A=332l2A = \frac{3\sqrt{3}}{2}l^2
xˉ=l\bar{x} = l
yˉ=32l\bar{y} = \frac{\sqrt{3}}{2}l
Iˉx=5316l4\bar{I}_x = \frac{5\sqrt{3}}{16}l^4
Iˉy=5316l4\bar{I}_y = \frac{5\sqrt{3}}{16}l^4
Calculate
OctagonOctagon
A=2(2+1)l2A = 2(\sqrt{2}+1) l^2
xˉ=2+12l\bar{x} = \frac{\sqrt{2}+1}{2} l
yˉ=2+12l\bar{y} = \frac{\sqrt{2}+1}{2} l
Iˉx=11+8212l4\bar{I}_x = \frac{11+8\sqrt{2}}{12} l^4
Iˉy=11+8212l4\bar{I}_y = \frac{11+8\sqrt{2}}{12} l^4
Calculate

Structural profiles

SectionAreaCentroidInertia about x̄Inertia about ȳ
I-BeamI-Beam
A=td+2s(b−t)A = td +2s(b -t)
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=d2\bar{y} = \frac{d}{2}
Iˉx=bs36+bs(d−s)22+t(d−2s)312\bar{I}_x = \frac{bs^3}{6} +\frac{bs(d-s)^2}{2} +\frac{t(d-2s)^3}{12}
Iˉy=b3s6+t3(d−2s)12\bar{I}_y = \frac{b^3s}{6} +\frac{t^3(d -2s)}{12}
Calculate
Tapered I-BeamTapered I-Beam
A=dt+(b−t)(g+s)A = dt + (b-t)(g+s)
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=d2\bar{y} = \frac{d}{2}
Iˉx=d3t12+(b−t)(3d2(g+s)−4d(g2+gs+s2)+2(g+s)(g2+s2))12\bar{I}_x = \frac{d^3 t}{12} + \frac{(b - t)(3d^2(g + s) - 4d(g^2 + gs + s^2) + 2(g + s)(g^2 + s^2))}{12}
Iˉy=dt312+(b−t)((b+t)2(g+s)+2(gt2+sb2))24\bar{I}_y = \frac{d t^3}{12} + \frac{(b-t)((b + t)^2(g + s) + 2(gt^2 + sb^2))}{24}
Calculate
Unequal I-BeamUnequal I-Beam
A=dt+s1(b1−t)+s2(b2−t)A = dt+s_1(b_1-t)+s_2(b_2-t)
xˉ=max(b1,b2)2\bar{x} = \frac{\text{max}(b_1,b_2)}{2}
—
—
Iˉy=dt3+s1(b13−t3)+s2(b23−t3)12\bar{I}_y = \frac{dt^3 + s_1(b_1^3-t^3) + s_2(b_2^3 - t^3)}{12}
Calculate
T-BeamT-Beam
A=bs+t(d−s)A = bs+t(d-s)
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=bs(2d−s)+t(d−s)22A\bar{y} = \frac{bs(2d-s)+t(d-s)^2}{2A}
Iˉx=Ix−yˉ2A\bar{I}_x = I_x - \bar{y}^2 A
Iˉy=b3s12+t3(d−s)12\bar{I}_y = \frac{b^3s}{12} + \frac{t^3(d-s)}{12}
Calculate
Tapered T-BeamTapered T-Beam
A=bs+(d−s)(t1+t2)2A = bs + \frac{(d-s)(t_1+t_2)}{2}
xˉ=b2\bar{x} = \frac{b}{2}
yˉ=3bs(2d−s)+(d−s)2(t1+2t2)6A\bar{y} = \frac{3bs(2d-s) + (d-s)^2(t_1+2t_2)}{6A}
Iˉx=Ix−yˉ2A\bar{I}_x = I_x - \bar{y}^2 A
Iˉy=b3s12+(d−s)(t1+t2)(t12+t22)48\bar{I}_y = \frac{b^3s}{12} + \frac{(d-s)(t_1+t_2)(t_1^2+t_2^2)}{48}
Calculate
Square ChannelSquare Channel
A=2bs+t(d−2s)A = 2bs + t(d-2s)
xˉ=2b2s+t2(d−2s)4bs+2t(d−2s)\bar{x} = \frac{2b^2s + t^2(d-2s)}{4bs + 2t(d-2s)}
yˉ=d2\bar{y} = \frac{d}{2}
Iˉx=Ix−yˉ2A\bar{I}_x = I_x - \bar{y}^2A
Iˉy=Iy−xˉ2A\bar{I}_y = I_y - \bar{x}^2A
Calculate
Tapered ChannelTapered Channel
A=bd−(b−t)(d−n−s)A = bd - (b-t)(d-n-s)
xˉ=2b2(n+2s)+2b(n−s)t+(3d−4n−2s)t26A\bar{x} = \frac{2b^2(n+2s) + 2b(n-s)t + (3d-4n-2s)t^2}{6A}
yˉ=d2\bar{y} = \frac{d}{2}
Iˉx=Ix−yˉ2A\bar{I}_x = I_x - \bar{y}^2A
—Calculate
Square AngleSquare Angle
A=a2−(a−t)2A = a^2 - (a-t)^2
xˉ=a2+at−t22(2a−t)\bar{x} = \frac{a^2 + at - t^2}{2(2a - t)}
yˉ=a2+at−t22(2a−t)\bar{y} = \frac{a^2 + at - t^2}{2(2a - t)}
Iˉx=Ix−yˉ2A\bar{I}_x = I_x - \bar{y}^2 A
Iˉy=Iy−xˉ2A\bar{I}_y = I_y - \bar{x}^2 A
Calculate
Rectangular AngleRectangular Angle
A=t(a+b−t)A = t(a + b - t)
xˉ=at+b2−t22(a+b−t)\bar{x} = \frac{at+b^2-t^2}{2(a+b-t)}
yˉ=a2+bt−t22(a+b−t)\bar{y} = \frac{a^2+bt-t^2}{2(a+b-t)}
Iˉx=Ix−yˉ2A\bar{I}_x = I_x - \bar{y}^2 A
Iˉy=Iy−xˉ2A\bar{I}_y = I_y - \bar{x}^2 A
Calculate
Z-BeamZ-Beam
A=t(2b+d−2t)A = t(2b + d - 2t)
xˉ=b−t2\bar{x} = b-\frac{t}{2}
yˉ=d2\bar{y} = \frac{d}{2}
Iˉx=t(2b(3d2−6dt+4t2)+(d−2t)3)12\bar{I}_x = \frac{t(2b(3d^2-6dt+4t^2) + (d-2t)^3)}{12}
Iˉy=t((2b−t)3+t2(d−t))12\bar{I}_y = \frac{t((2b-t)^3+t^2(d-t))}{12}
Calculate

Notation and axes

Notation and axes

The origin is the bottom-left corner of the bounding box. x̄ and ȳ locate the centroid; Ī_x and Ī_y are the moments of inertia about the centroidal axes; I_x and I_y are taken about the base and the left edge, related by the parallel axis theorem.

Where these properties are used

Bending stress σ = M·y/Ī, deflection of beams (EI), buckling of columns (radius of gyration r = √(Ī/A)) and the plastic capacity of steel sections (Z).

Frequently Asked Questions

What is the moment of inertia of a rectangle?

About its centroidal horizontal axis, a rectangle of base b and height h has Ī_x = bh³/12. About its base it is I_x = bh³/3, which is the centroidal value plus A·(h/2)² by the parallel axis theorem.

What is the moment of inertia of a circle?

A solid circle of radius r has Ī = πr⁴/4 about any centroidal axis. A hollow circle with outer radius R and inner radius r has Ī = π(R⁴ − r⁴)/4.

Where is the centroid of a triangle or a trapezoid?

The centroid of a triangle is at one third of its height from the base. For a trapezoid with parallel sides a (top) and b (bottom) and height h, it is at ȳ = h(2a + b)/(3(a + b)) from the base.

How do I combine several shapes?

Add the areas, find the combined centroid as the area-weighted average of the individual centroids, and add each moment of inertia moved to the combined centroid with the parallel axis theorem: I = Ī + A·d².

Get the properties for your dimensions

Choose a section, enter its dimensions and get the area, centroid and moments of inertia instantly, with the section drawn to scale.

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