For a slender elastic beam, the Euler-Bernoulli beam equation assumes small strain, small deflection slopes and cross-sections that remain plane and normal to the deflected centreline. A fibre at signed distance from the neutral axis has longitudinal strain , where is the centreline curvature. Hooke's law gives , with Young's modulus .
Choose the internal bending-moment sign so that . ThenHere is the second moment of area, with units , not the mass moment of inertia of a rotating body. For a uniform material under pure bending, zero axial resultant places the neutral axis through the section's centroid.
For small slopes, . Combining the moment-curvature relation with transverse force and moment balance gives, with a consistent load sign convention,For constant stiffness this becomes . The bending stiffness has units . Boundary conditions specify displacement and slope at a clamped end, or bending moment and shear force at a free end.
For a cantilever of length carrying a transverse end load , take deflection positive towards the load. The moment magnitude is , and integration with givesThe free-end moment vanishes and the tip shear supplies the applied load. For a rectangular section of width and bending thickness , , so increasing thickness strongly increases bending resistance. The model ceases to be reliable for large deflections, plastic strains or short thick beams where shear deformation matters.
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