Torsion of Circular Shafts — the Torsion Formula
Why twisting a shaft creates shear stress that is zero at the centre and maximum at the surface — and why hollow shafts win on efficiency.
Turn a screwdriver and the shaft twists. You cannot see it, but the material is being sheared — stressed parallel to the cross-section. That shear stress is not uniform: it is zero exactly at the centre of the shaft and largest at the outer surface. Engineers size drive shafts, propellers, and drill bits using one formula that captures this entire behaviour: the torsion formula.
From shear strain linearity to the torsion formula
When a torque is applied to a circular shaft, every cross-section rotates slightly relative to its neighbour. Imagine drawing a grid of longitudinal and circumferential lines on the surface: after twisting, the longitudinal lines become helices. The angle change between a longitudinal line and a circumferential line is the shear strain γ at the surface.
For a small twist angle, the arc length at radius ρ is proportional to ρ. That means the shear strain — and therefore the shear stress in the elastic range — grows linearly from the centre outward:
τ(ρ) ∝ ρ
To turn this proportionality into an equation, we use the fact that the sum of the moment produced by shear stresses over the entire cross-section must equal the applied torque T. That integration yields the torsion formula:
Two common misconceptions cause real design errors:
- Non-circular sections warp. A square bar under torsion does not remain plane; its cross-sections distort out of plane. The simple linear τ = Tρ/J relationship breaks down completely. Square shafts need St. Venant torsion theory — a different, more advanced analysis.
- Plastic deformation changes the distribution. Once the outer fibres yield, the stress profile flattens and spreads inward. The elastic torsion formula overestimates the torque capacity if the material has yielded.
Whenever you reach for τ = Tρ/J, confirm both that the shaft is circular and that the maximum stress is below the shear yield strength.
Why hollow shafts are more efficient
Material near the centre of a solid shaft carries almost no stress — the torsion formula shows τ is proportional to ρ, so the core is essentially along for the ride. By removing that low-stress material and relocating it to a larger outer radius, a hollow shaft achieves a much larger polar moment of inertia J without a proportional increase in mass.
The result is a higher strength-to-weight ratio. Aircraft propeller shafts, race-car drive shafts, and bicycle bottom-bracket axles are often hollow for exactly this reason. The design trade-off is that very thin walls can buckle locally, so wall thickness is chosen to resist both shear stress and local instability.
- Solid shaft: J = π/32 × 50⁴ = 6.136 × 10⁵ mm⁴ = 6.136 × 10⁻⁷ m⁴.
- Solid shaft: τ_max = 2500 × 0.025 / 6.136×10⁻⁷ = 101.9 MPa.
- Hollow shaft: J = π/32 × (60⁴ − 40⁴) = 1.021 × 10⁶ mm⁴ = 1.021 × 10⁻⁶ m⁴.
- Hollow shaft: τ_max = 2500 × 0.030 / 1.021×10⁻⁶ = 73.5 MPa.
- Area solid = π/4 × 50² = 1964 mm². Area hollow = π/4 × (60² − 40²) = 1571 mm².
- Comparison: the hollow shaft has 20% less mass but 66% higher J, giving 28% lower peak stress. This is why hollow shafts are more efficient for torsion.
- τ_max = 16T / (πd³) with T = 1500 N·m, d = 0.040 m.
- τ_max = 16 × 1500 / (π × 0.040³) = 24 000 / (2.011×10⁻⁴) = 1.194×10⁸ Pa = 119.4 MPa.
- J = π/32 × (D⁴ − d⁴) = π/32 × (80⁴ − 50⁴) = π/32 × (40 960 000 − 6 250 000).
- J = π/32 × 34 710 000 = 3 406 400 mm⁴.
Check your understanding
- The torsion formula τ = Tρ/J gives shear stress at any radius in a circular elastic shaft.
- J_solid = πd⁴/32; J_hollow = π(D⁴ − d⁴)/32.
- τ_max occurs at the outer radius and is zero at the centre.
- Hollow shafts are more efficient because they place material where stress is highest.
- The formula is valid only for circular shafts in the elastic range.
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