Lesson 4 · 35 min

Composite Bodies

A pendulum is a rod and a bob; a flywheel is a disk with a bore and a ring of holes. Split a part into standard shapes, move each one to the common axis with the parallel-axis theorem, and add, subtracting the holes.

Learning objectives

Add the parts

The moment of inertia is an integral over the body, and an integral over a whole is the sum of the integrals over its parts. So, about any one axis,

Composite body about a common axis

\[ I = \sum_i \left(\bar I_i + m_i d_i^2\right), \qquad m = \sum_i m_i \]

\(\bar I_i\): moment of inertia of part \(i\) about its own centroidal axis parallel to the common axis (Lesson 2 table). \(d_i\): distance from that centroidal axis to the common axis. A hole is a part with negative \(m_i\), and its whole \(\bar I_i + m_i d_i^2\) is subtracted.

Every term must be about the same axis. The parallel-axis theorem moves each part's table value there. When the parts are not uniform, or the densities differ, compute each mass from its own density and volume.

Example 4.1 — A rod-and-disk pendulum

A pendulum is a uniform \(2\ \text{kg}\) slender rod, \(0.8\ \text{m}\) long, pinned at its top end \(O\), with a thin \(5\ \text{kg}\) disk of radius \(0.15\ \text{m}\) welded to its lower end so that the disk's center is \(0.95\ \text{m}\) below \(O\). The pendulum swings in the plane of the disk. Find \(I_O\), the center of mass, \(I_G\) and the period of small oscillations.

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The axis at \(O\) is perpendicular to the plane of the swing. Measure distances down from \(O\):

Parts about the pin \(O\) (SI units)
Part\(m_i\)\(d_i\)\(\bar I_i\)\(m_i d_i^2\)\(I_{O,i}\)
Rod20.40\(\tfrac1{12}(2)(0.8)^2 = 0.1067\)0.32000.4267
Disk50.95\(\tfrac12(5)(0.15)^2 = 0.0563\)4.51254.5688
Pendulum74.9954

So \(I_O = 4.995\ \text{kg·m}^2\). The center of mass is \(\bar y = (2 \cdot 0.40 + 5 \cdot 0.95)/7 = 0.7929\ \text{m}\) below \(O\), and

\[ I_G = I_O - m\bar y^2 = 4.995 - 7(0.7929)^2 = 0.5951\ \text{kg·m}^2 \]

For small swings of a compound pendulum, \(\tau = 2\pi\sqrt{I_O/(m g \bar y)} = 2\pi\sqrt{4.995/(7 \cdot 9.81 \cdot 0.7929)} = 1.903\ \text{s}\).

Notice how the disk's own \(\bar I\) (0.056) is tiny next to its transfer term \(m d^2\) (4.51): far from the axis, a part behaves almost like a particle.

Holes are negative mass

A plate with a hole is the full plate minus a disk of the same material. The same goes for bores, lightening holes, slots and pockets: compute the missing piece as if it were there, then subtract its mass and its moment of inertia about the common axis, transfer term included.

Example 4.2 — A plate with two holes

A steel plate (\(\rho = 7850\ \text{kg/m}^3\)) is \(400 \times 300\ \text{mm}\) and \(10\ \text{mm}\) thick. Two holes of radius \(50\ \text{mm}\) are centered \(100\ \text{mm}\) either side of the plate's center, on its long centerline. Find the mass and the moment of inertia about the axis through the plate's center, perpendicular to the plate.

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Masses: full plate \(7850(0.4)(0.3)(0.01) = 9.420\ \text{kg}\); each hole \(7850\pi(0.05)^2(0.01) = 0.6165\ \text{kg}\).

Parts about the central axis (SI units)
Part\(m_i\)\(d_i\)\(\bar I_i\)\(m_i d_i^2\)\(I_i\)
Plate9.4200\(\tfrac1{12}m(a^2 + b^2) = 0.19625\)00.19625
Hole 1−0.61650.10\(-\tfrac12 m r^2 = -0.00077\)−0.00617−0.00694
Hole 2−0.61650.10\(-0.00077\)−0.00617−0.00694
Plate with holes8.1870.18238

\(m = 8.187\ \text{kg}\) and \(I = 0.1824\ \text{kg·m}^2\). The holes remove 13% of the mass but only 7% of the moment of inertia, because they sit fairly close to the axis.

Figure 4.1 A flywheel designer: a \(30\ \text{mm}\) thick steel disk of radius \(250\ \text{mm}\) with a \(25\ \text{mm}\) shaft bore and a ring of lightening holes. Each part's mass and moment of inertia about the shaft is listed, holes negative. Try the same holes near the bore and near the rim: which position costs more moment of inertia for the same mass saved?

The composite center of mass

Often the axis you need is through the composite center of mass \(G\), which is not the center of any single part. Find it first, as in statics,

\[ \bar x = \frac{\sum m_i \bar x_i}{\sum m_i}, \qquad \bar y = \frac{\sum m_i \bar y_i}{\sum m_i}, \]

then either transfer every part to \(G\) directly, or compute \(I\) about a convenient point \(O\) and step back once: \(I_G = I_O - m\,d_{OG}^2\).

Example 4.3 — A T-shaped bracket

A T-shaped bracket is made of two uniform slender rods: \(AB\) is \(0.6\ \text{m}\) long with mass \(1.2\ \text{kg}\), and \(CD\) is \(0.4\ \text{m}\) long with mass \(0.8\ \text{kg}\), welded at \(C\) to the midpoint of \(AB\) and perpendicular to it. Find the center of mass and the moment of inertia about the axis through \(G\) perpendicular to the plane of the T.

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Put the origin at \(C\), with \(x\) along \(AB\) and \(y\) along \(DC\) (so \(D\) is at \(y = -0.4\ \text{m}\)). By symmetry \(\bar x = 0\), and

\[ \bar y = \frac{1.2(0) + 0.8(-0.2)}{2.0} = -0.0800\ \text{m} \]

About \(C\) (axis perpendicular to the plane): \(AB\) turns about its middle and \(CD\) about its end:

\[ I_C = \tfrac1{12}(1.2)(0.6)^2 + \tfrac13(0.8)(0.4)^2 = 0.0360 + 0.0427 = 0.0787\ \text{kg·m}^2 \] \[ I_G = I_C - m\,\bar y^2 = 0.07867 - 2.0(0.08)^2 = 0.06587\ \text{kg·m}^2 \]

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Key takeaways