Perpendicular axis theorem

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The perpendicular axis theorem (or plane figure theorem) states that for a planar lamina with a uniform mass distribution, the moment of inertia about an axis perpendicular to the plane of the lamina is equal to the sum of the moments of inertia about two mutually perpendicular axes in the plane of the lamina, which intersect at the point where the perpendicular axis passes through. This theorem applies only to planar bodies with a uniform mass distribution and is valid when the body lies entirely in a single plane.

Define perpendicular axes , , and (which meet at origin ) so that the body lies in the plane, and the axis is perpendicular to the plane of the body. Let Ix, Iy and Iz be moments of inertia about axis x, y, z respectively. Then the perpendicular axis theorem states that[1]

This rule can be applied with the parallel axis theorem and the stretch rule to find polar moments of inertia for a variety of shapes.

If a planar object has rotational symmetry such that and are equal,[2] then the perpendicular axes theorem provides the useful relationship:

Derivation

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Working in Cartesian coordinates, the moment of inertia of the planar body about the   axis is given by:[3]

 

On the plane,  , so these two terms are the moments of inertia about the   and   axes respectively, giving the perpendicular axis theorem. The converse of this theorem is also derived similarly.

Note that   because in  ,   measures the distance from the axis of rotation, so for a y-axis rotation, deviation distance from the axis of rotation of a point is equal to its x coordinate.

References

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  1. ^ Tipler, Paul A. (1976). "Ch. 12: Rotation of a Rigid Body about a Fixed Axis". Physics. Worth Publishers Inc. ISBN 0-87901-041-X.
  2. ^ Obregon, Joaquin (2012). Mechanical Simmetry. Author House. ISBN 978-1-4772-3372-6.
  3. ^ K. F. Riley, M. P. Hobson & S. J. Bence (2006). "Ch. 6: Multiple Integrals". Mathematical Methods for Physics and Engineering. Cambridge University Press. ISBN 978-0-521-67971-8.

See also

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