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Beam deflections from applied bending moments

As illustrated in the diagram below, the beam curvature, κ, is approximately equal to the second derivative (curvature) of the neutral axis line (dotted line in diagram)

The approximation involved in equating beam curvature to the curvature of the neutral axis of a beam.

It follows that

Since the moment at the section concerned can also be written, for a cantilever beam, as

it follows that

This second order differential equation can be integrated (twice), with appropriate boundary conditions, to find the deflection of the beam at different points along its length. For a cantilever beam, this operation is shown below.

which can be rearranged to give

For example, at the loaded end ( x = L ), this gives

The corresponding operation for symmetrical 3-point bending can be seen by clicking here .


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