STRUCTURAL / BEAMS

Cantilever with a point load at any position.

Calculate the fixed-end shear and moment, movement at the loaded point, and movement at the free end for a flexible point-load position.

METHOD

What this calculator solves

This is the constant-EI Euler-Bernoulli solution for a cantilever fixed at one end and free at the other. Enter the downward point-load magnitude P and its distance a from the fixed end. The unloaded segment beyond the load moves with the rotation and translation already accumulated at the load.

|Mfixed| = Pa; Vfixed = P

δa = Pa3 / (3EI)

δfree = Pa2(3L − a) / (6EI)

θfree = Pa2 / (2EI)

Input convention: P is a non-negative downward magnitude; a is measured from the fixed end and may range from 0 to L; E is entered in GPa and I in cm4. Actions are shown as magnitudes, so the fixed-end moment is labelled by magnitude rather than a signed sagging/hogging algebraic value.

The classic free-end point-load case is recovered at a = L: the fixed-end moment is PL, free-end deflection is PL3/(3EI), and free-end rotation is PL2/(2EI). At a = 0, the entered point load has no lever arm and produces zero transverse response. Intermediate positions cover the familiar “load somewhere along a cantilever” case.

SCOPE

Assumptions and limitations

  • Euler-Bernoulli, linear-elastic beam theory with constant E and I.
  • The root is perfectly fixed and the free end is unrestrained; connection flexibility and support movement are excluded.
  • One transverse point load is included; no distributed load, axial force, torsion, or self-weight is added by this page.
  • Shear deformation, second-order effects, material nonlinearity, large rotation, and dynamic response are excluded.
  • The page reports deflection at the load and at the free end, plus free-end rotation; it does not search for a separate maximum along the span.
  • This is an analysis aid, not a section-capacity, connection, serviceability, or code-compliance check.

REFERENCES

Further reading

Compare the position-dependent load case with StructX: cantilever beam with point load at any point. Its free-end limit is also shown by StructX: cantilever beam with a free-end point load. For beam-theory assumptions and boundary conditions, see MIT OpenCourseWare beam theory notes.

Use engineering judgement.

Check that the physical load location is measured from the fixed face, not from the free end, and that the entered stiffness represents the actual cracked, composite, or uncracked model intended for the study.