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Beam deflection during cantilever bending

The beam curvature, κ, is approximately equal to the curvature of the line traced by the neutral axis, d2y/dx2 (see diagram below), so that

Equation

where M is the bending moment, E is the Young's modulus and I is the second moment of area. Applying this to the end-loaded cantilever beam, and taking the moment as positive when it generates a displacement in the downward direction (+ive y)

Equation

where F is the load applied at the end of the beam.

Diagram of cantilever curvature

Approximation involved in equating beam curvature to the curvature of the neutral axis (Click on image for larger version)

The deflection is found by integrating this expression, using boundary conditions to establish the integration constants

Equation

Equation

The deflections along the length of the beam, and specifically at the loaded end, are thus given by

Equation


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