FrameLab bent beams & frames
Open the interactive version →

This is a static copy of the chapter for search engines. The interactive version has animated figures, check questions, and buttons that load the example into the calculator.

Deflections of bent bars by hand

You will not integrate w″ = M/EI twice for a bent bar — the axis changes direction, so there is no single w(x) to integrate. The practical hand method is the unit-load method (Castigliano’s second theorem in its engineering form), and it is worth knowing because it explains where a deflection comes from.

The recipe

To find the displacement δ of a point in a chosen direction:

  1. Solve the real structure and write the internal actions M(s), N(s), T(s) for every member.
  2. Remove the real load, apply a unit force (1 N) at the point, in the direction whose displacement you want, and solve again → M̄(s), N̄(s), T̄(s).
  3. Integrate the products over the whole developed length:
δ = ∫ M·M̄EI ds + ∫ N·N̄EA ds + ∫ T·T̄GJt ds

Each integral is one physical mechanism: bending, stretching, twisting. For a rotation instead of a displacement, apply a unit moment. Because the integrands are usually a product of two straight lines or a line and a parabola, the integrals are almost always done from a table rather than by calculus.

Which term actually matters

For slender bars, bending dominates. A quick order-of-magnitude comparison for the L-bracket of chapter 7 with a 1 m arm and a 100 mm deep section:

MechanismRelative contributionWhen it matters
bending (M·M̄/EI)100 %always
torsion (T·T̄/GJ)0 % in plane, up to several hundred % out of plane for an open sectionout-of-plane loads
axial (N·N̄/EA)typically well under 1 %short stocky members, arches, trusses
sheara few % for L/h < 10short deep members — not included here

FrameLab includes bending, axial and torsional flexibility in full (it is a finite-element solution, so all of them come out automatically). It does not include shear deformation — the Euler–Bernoulli assumption. For L/h ratios above about 10, the error from that is under a per cent.

A hand check you can always do

For the L-bracket with a vertical tip load P, arm a, column b:

δtipP·a³3EI + P·a²·bEI + P·bEA

The middle term is the rotation of the column top (caused by the constant moment P·a along it) multiplied by the lever arm a. Run the first example in chapter 1 and compare — the numbers agree to three digits.

💡 The unit-load method is also the fastest way to see why a structure is too flexible. If the torsion integral dominates, no amount of extra depth will help: you need a closed section.

Formulas in this chapter

δ — in-plane tip deflection of an L-bracket
δ = P·a³/(3EI) + P·a²·h/(EI) + P·h/(EA) [m] Castigliano's second theorem
δ_i — Castigliano's second theorem
δ = ∫ M·(∂M/∂P)/(EI) ds summed over the members [m] Castigliano