For a thin-walled rectangular box (closed) of depth d, width b, and uniform wall thickness t, what is the approximate torsion constant k (Saint-Venant torsional rigidity parameter)?

Difficulty: Medium

Correct Answer: k ≈ (2 * b^2 * d^2 * t) / (b + d)

Explanation:


Introduction / Context:
The torsion constant k (often denoted J for Saint-Venant torsion) governs the elastic twist of prismatic members under pure torsion: θ' = T * L / (G * k). For thin-walled closed sections, warping is restrained, and the torsional rigidity is substantially higher than for open sections. A compact approximate expression exists for rectangular thin boxes of uniform thickness t, useful in steel and aerospace structures.


Given Data / Assumptions:

  • Section: closed rectangular thin-walled box.
  • Dimensions: width b, depth d, uniform thickness t.
  • Thin-wall assumption: t << b and t << d.


Concept / Approach:
For thin closed sections, the standard approximation is k ≈ 4 * A_m^2 / Σ(s/t), where A_m is the area enclosed by the midline of the wall, and Σ(s/t) is the summation of (segment length / thickness) around the perimeter. For a rectangle with uniform thickness, A_m ≈ b * d and Σ(s/t) ≈ 2 * (b + d) / t. Substituting yields a compact formula for k in terms of b, d, and t.


Step-by-Step Solution:

Start with thin-walled closed section formula: k = 4 * A_m^2 / Σ(s/t).Use A_m ≈ b * d for a rectangle (midline area).Use Σ(s/t) ≈ 2 * (b + d) / t for uniform thickness t.Compute: k ≈ 4 * (b * d)^2 / (2 * (b + d) / t) = (2 * b^2 * d^2 * t) / (b + d).


Verification / Alternative check:

Dimensional check: k has units of length^4. Right-hand side gives b^2 * d^2 * t / (b + d) → L^4, which is correct.


Why Other Options Are Wrong:

2 * b * d * t * (b + d) and 4 * b * d * t: scale as L^4 but ignore the squared area dependence, underestimating stiffness.(b * d * t) / (b + d): scales as L^3, dimensionally incorrect for k.(b^2 * d^2 * t) / (2 * (b + d)): off by a factor of 4 relative to the correct derivation.


Common Pitfalls:

Using open-section approximate J instead of the closed-section formula.Forgetting that A_m is the midline area, not the gross area minus wall thickness corrections (difference negligible for thin walls).


Final Answer:

k ≈ (2 * b^2 * d^2 * t) / (b + d)

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