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Derive virtual work principle

Short answer

Apply a virtual unit load at the desired displacement; let it produce virtual internal forces m, n, v. External virtual work 1·Δ equals internal virtual work ∫ (m·dθ + n·dδ + v·dγ). Substituting elastic deformations dθ=Mdx/EI, etc., yields Δ = ∫ (mM/EI + nN/AE + α vV/GA)dx.

Derive the virtual work principle.

Principle of virtual work (for deformable bodies): If a deformable structure in equilibrium under a real load system is given a virtual displacement field (compatible, small and imaginary), the external virtual work done by the real forces equals the internal virtual work done by the real internal stresses on the virtual strains. In the dual form (virtual forces), virtual loads are applied and move through the real displacements; this is the form used below.

Derivation (unit load form)

Consider a structure under real loads P1,P2,…P_1, P_2,\dots producing real internal forces and real deformations. To find the displacement Δ\Delta at a point, apply a virtual unit load at that point in the required direction. Let this virtual load produce internal forces: moment mm, axial force nn and shear vv.

  1. External virtual work. The unit load, kept constant, moves through the real displacement Δ\Delta:
We=1×ΔW_e = 1\times\Delta
  1. Internal virtual work. In an element of length dxdx, the virtual internal forces move through the real deformations of the element. For a linearly elastic member, the real deformations are
dθ=M dxEI,dδaxial=N dxAE,dγ=αV dxGAd\theta = \frac{M\,dx}{EI},\qquad d\delta_{axial} = \frac{N\,dx}{AE},\qquad d\gamma = \frac{\alpha V\,dx}{GA}

so the internal virtual work of the element is

dWi=m dθ+n dδaxial+v dγ=mMEIdx+nNAEdx+αvVGAdxdW_i = m\,d\theta + n\,d\delta_{axial} + v\,d\gamma = \frac{mM}{EI}dx + \frac{nN}{AE}dx + \frac{\alpha vV}{GA}dx
  1. Equate We=WiW_e = W_i (the virtual force system is in equilibrium, and the real deformations are compatible):
1⋅Δ=∫mMEIdx+∫nNAEdx+∫αvVGAdx1\cdot\Delta = \int \frac{mM}{EI}dx + \int\frac{nN}{AE}dx + \int\frac{\alpha vV}{GA}dx

For beams and frames, usually only the first term is kept. For trusses, Δ=∑kFLAE\Delta = \sum \dfrac{kFL}{AE}.

The general principle (We=WiW_e = W_i, i.e. 1⋅Δ=∫m dθ+∫n dδ+∫v dγ1\cdot\Delta = \int m\,d\theta + \int n\,d\delta + \int v\,d\gamma) holds for any material behaviour, provided the real deformations are small and compatible and the virtual forces satisfy equilibrium. The final form with EIEI, AEAE and GAGA, however, uses dθ=M dx/EId\theta = M\,dx/EI and similar relations, so it applies only to linearly elastic members.

✓ Answer checked by Claude Opus 5.5 (high effort)

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