Lab · Structural Mechanics

Beam Analysis Lab

One determinate beam, solved once. Reactions, shear, bending moment, extreme-fibre stress and the deflected shape all come from the same exact piecewise solution, so every diagram agrees with the others at every station.

Beam

-10 kN at x = 3 m-10 kNA pin · x = 0 mB roller · x = 6 mL = 6 m

Scroll the schematic sideways to see the whole beam; every result is also listed in the tables below.

Beam of 6 metres with 2 supports.

Beam and loads

The beam runs from x = 0 to x = L.

Supports

A
B

Point loads

P1

Point moments

Uniform distributed loads

Downward loads are negative (q < 0, Fy < 0); an applied couple is positive counter-clockwise. Internally, M > 0 is sagging, v > 0 is upward and θ > 0 is counter-clockwise.

Section and material (optional)

Leave a field empty to leave it unspecified: reactions, shear and bending moment are reported without any section data. A value that is zero or negative is not unspecified — it is reported as an invalid entry. Bending stress additionally needs I and an extreme-fibre distance c; slope and deflection need both E and I.

What this Lab models

A planar beam with rigid supports, solved by planar equilibrium and Euler–Bernoulli bending.

Model scope

  • · Statically determinate support arrangement: cantilever, simply supported or overhanging.
  • · Small displacements on the undeformed geometry, linear-elastic material, constant EI along the span.
  • · Shear deformation is neglected, so deflections are those of a slender beam.
  • · Loads act in the plane; downward is negative and an applied couple is positive counter-clockwise.
  • · Indeterminate beams, continuous beams over three or more supports, frames and support settlement are outside this Lab.
  • · Bending stress is elementary flexure; stress concentrations and local effects at supports and point loads are not modelled.

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