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Torsion of a rectangular hollow thin-wall box

Short answer

Shear flow q = T/(2A) = 250 N/mm. Shear stresses: 62.5 MPa in the 4 mm top/bottom walls, 41.7 MPa in the 6 mm side walls. Angle of twist per metre: 0.0182 rad/m. Equivalent torsional constant J = 2.06×10⁶ mm⁴. Over 1.5 m, total twist = 0.0273 rad (1.57°).

A thin-walled rectangular box section has mean dimensions 100 mm wide and 60 mm deep. The top and bottom walls are 4 mm thick and the two side walls are 6 mm thick. The section is subjected to a torque of 3 kN m. Find the shear flow, the shear stress in each wall, the angle of twist per metre length and the equivalent torsional constant. Take G=80G = 80 GPa. Also find the total twist for a length of 1.5 m.

Bredt-Batho theory

For a thin-walled closed section, the shear flow q=τtq = \tau t is constant around the wall, and the torque is T=2AqT = 2Aq, where AA is the area enclosed by the mid-line of the wall.

        100 mm (mean)
    +-----------------+  t = 4 mm
    |                 |
    |                 | 60 mm   sides t = 6 mm
    |                 |
    +-----------------+  t = 4 mm

Data

A=100×60=6000A = 100\times60 = 6000 mm2^2, T=3 kN m=3×106T = 3\ \text{kN m} = 3\times10^6 N mm, G=80×103G = 80\times10^3 MPa.

Shear flow and stress

q=T2A=3×1062×6000=250 N/mmq = \frac{T}{2A} = \frac{3\times10^6}{2\times6000} = 250\ \text{N/mm} τtop,bottom=qt=2504=62.5 MPaτsides=2506=41.67 MPa\begin{aligned} \tau_{top,bottom} &= \frac{q}{t} = \frac{250}{4} = 62.5\ \text{MPa} \\ \tau_{sides} &= \frac{250}{6} = 41.67\ \text{MPa} \end{aligned}

The maximum shear stress occurs in the thinnest wall (4 mm): 62.562.5 MPa.

Angle of twist per unit length

Equating the strain energy to the work done by the torque gives

θ=T4A2G∮dst\theta = \frac{T}{4A^2G}\oint\frac{ds}{t} ∮dst=2(1004)+2(606)=50+20=70\oint\frac{ds}{t} = 2\left(\frac{100}{4}\right) + 2\left(\frac{60}{6}\right) = 50 + 20 = 70 θ=3×106×704×(6000)2×80×103=2.1×1081.152×1013=1.823×10−5 rad/mm\theta = \frac{3\times10^6\times70}{4\times(6000)^2\times80\times10^3} = \frac{2.1\times10^8}{1.152\times10^{13}} = 1.823\times10^{-5}\ \text{rad/mm} θ=0.01823 rad/m=1.045∘/m\theta = 0.01823\ \text{rad/m} = 1.045^\circ\text{/m}

Equivalent torsional constant

Jeq=4A2∮ds/t=4×6000270=2.057×106 mm4J_{eq} = \frac{4A^2}{\oint ds/t} = \frac{4\times 6000^2}{70} = 2.057\times10^{6}\ \text{mm}^4

Check: θ=T/(GJeq)=3×106/(80×103×2.057×106)=1.823×10−5\theta = T/(GJ_{eq}) = 3\times10^6/(80\times10^3\times2.057\times10^6) = 1.823\times10^{-5} rad/mm. ✓\checkmark

Total twist for 1.5 m

ϕ=θL=0.01823×1.5=0.0273 rad=1.57∘\phi = \theta L = 0.01823\times1.5 = 0.0273\ \text{rad} = 1.57^\circ

Answer: q=250q = 250 N/mm; τ=62.5\tau = 62.5 MPa (top and bottom), 41.741.7 MPa (sides); θ=0.0182\theta = 0.0182 rad/m; Jeq=2.06×106J_{eq} = 2.06\times10^6 mm4^4; twist over 1.5 m =0.0273= 0.0273 rad (1.57∘1.57^\circ).

✓ Answer checked by Claude Sonnet 5.5

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