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Strain energy due to shear in rectangular beam

Short answer

Derive by integrating shear stress energy density over the section. For rectangular section, shear stress τ = V/(2I)(d^2/4 - y^2). The shear strain energy per length dU = (6/5)(V^2/(2GA))dx, so total Us = ∫ (6/5)(V^2/(2GA)) dx = ∫ (3V^2/(5GA)) dx.

For a beam having a rectangular cross-section and subjected to lateral loads, derive an expression for the strain energy due to shear deformation only.

Strain energy due to shear is the energy stored because of the shear deformation of the beam. For a rectangular section the shear stress varies parabolically, so the energy is found by integrating over the section.

Derivation

Take a beam of rectangular section (width bb, depth dd) carrying shear force VV at a section. Shear stress at a distance yy from the neutral axis:

τ=VAyˉIb=V2I(d24−y2)\tau = \frac{V A\bar y}{I b} = \frac{V}{2I}\left(\frac{d^2}{4} - y^2\right)

Strain energy per unit volume =τ22G= \dfrac{\tau^2}{2G}. For an element of length dxdx, with area element dA=b dydA = b\,dy:

dU=∫−d/2d/2τ22G b dy dxdU = \int_{-d/2}^{d/2} \frac{\tau^2}{2G}\, b\,dy\,dx

Substituting τ\tau:

dU=V2b dx8GI2∫−d/2d/2(d24−y2)2dy=V2b dx8GI2⋅d530\begin{aligned} dU &= \frac{V^2 b\,dx}{8GI^2}\int_{-d/2}^{d/2}\left(\frac{d^2}{4}-y^2\right)^2 dy \\ &= \frac{V^2 b\,dx}{8GI^2}\cdot\frac{d^5}{30} \end{aligned}

Using I=bd312I = \dfrac{bd^3}{12}, so I2=b2d6144I^2 = \dfrac{b^2d^6}{144}:

dU=V2b d5×1448G b2d6×30 dx=3V25 G bd dx=65⋅V22GA dxdU = \frac{V^2 b\, d^5 \times 144}{8G\,b^2 d^6\times 30}\,dx = \frac{3V^2}{5\,G\,bd}\,dx = \frac{6}{5}\cdot\frac{V^2}{2GA}\,dx

where A=bdA = bd. Hence the shear strain energy for the whole beam is

Us=∫0L65 V22GA dx=∫0L3V25GA dxU_s = \int_0^L \frac{6}{5}\,\frac{V^2}{2GA}\,dx = \int_0^L \frac{3V^2}{5GA}\,dx

The factor 65=1.2\dfrac{6}{5} = 1.2 is the form factor (shape factor) for shear α\alpha of a rectangle. If shear were uniform, dU=V22GAdxdU = \dfrac{V^2}{2GA}dx.

Example (check): simply supported beam with central load PP: V=±P/2V = \pm P/2,

Us=65×(P/2)22GA×L=3P2L20 GAU_s = \frac{6}{5}\times\frac{(P/2)^2}{2GA}\times L = \frac{3P^2L}{20\,GA}

The deflection under the load (from δ=∂U/∂P\delta = \partial U/\partial P) is δs=3PL10GA\delta_s = \dfrac{3PL}{10GA}.

Result: Us=65∫0LV22GA dxU_s = \dfrac{6}{5}\displaystyle\int_0^L \dfrac{V^2}{2GA}\,dx for a rectangular section.

✓ Answer checked by Claude Opus 5.5 (high effort)

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