22-Mec-B9 Advanced Engineering Structures · December 2019
Question 6 of 7: Two-segment circular torsion box
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 16-Mec-B9 Advanced Engineering Structures, National Examinations, December 2019. Three hours, open book, any non-communicating calculator permitted. Seven problems of equal value; any five constitute a complete paper. All seven are solved here, because the set is a study resource rather than an examination script.
Reference texts. T. H. G. Megson, Aircraft Structures for Engineering Students, 6th ed. (thin-walled open and closed sections, structural idealisation, shear centre, multi-cell torsion); A. P. Boresi and R. J. Schmidt, Advanced Mechanics of Materials, 6th ed. (curved beams, yield criteria); A. C. Ugural and S. K. Fenster, Advanced Mechanics of Materials and Applied Elasticity, 5th ed.; R. C. Hibbeler, Mechanics of Materials, 10th ed. (statically indeterminate axial members, thermal stress); G. E. Dieter, Mechanical Metallurgy, 3rd ed. (fatigue-crack growth, Paris law).
Given. A circular thin-walled tube of median radius 200 mm divided into two equal cells by a diametral wall, in pure torsion, with a limiting shear stress imposed on the material.
Torsion box data
Quantity
Value
Median radius R
200 mm
Outer skin thickness t1
10 mm
Dividing wall thickness t2
5 mm
Shear modulus G
80 GPa
Allowable shear stress τ
20 MPa
Find. The largest torque the section can carry without exceeding 20 MPa anywhere, and the corresponding rate of twist.
Figure 6.1 — The two cells are mirror images, so they carry identical flows and the wall between them carries their difference, which is zero. The section behaves exactly as the undivided tube.
Approach. Exploit the mirror symmetry to collapse the two-cell problem to one unknown flow, set that flow from the stress limit in the governing wall, then obtain the torque from the Bredt–Batho sum and the twist rate from either cell.
Set out the cell geometry. The diametral wall splits the tube into two semicircular cells, each enclosing
$$A_1=A_2=\frac{\pi R^{2}}{2}=\frac{\pi(200)^2}{2}=62\,832\ \text{mm}^2$$
Each cell is bounded by a semicircular arc of length $\pi R = 628.3$ mm at thickness $t_1$ and by the straight dividing wall of length $2R = 400$ mm at thickness $t_2$.
Use symmetry to eliminate one unknown. For a multi-cell section in pure torsion every cell must twist at the same rate. The two cells here are geometric mirror images with identical wall thicknesses, so the equal-twist condition is satisfied by
$$q_1=q_2=q$$
and the shear flow carried by the wall they share is the difference of the two cell flows:
$$\boxed{q_{\text{wall}} = q_1 - q_2 = 0}$$
The dividing wall is unloaded, and $t_2$ cannot appear in any answer. Recognising this at the outset replaces a two-equation system with a single line.
Set the flow from the stress limit. With the wall carrying nothing, the governing stress is in the outer skin, so
$$\tau_1=\frac{q}{t_1}\le 20\ \text{MPa}\quad\Longrightarrow\quad q=\tau_1t_1=20(10)=200\ \text{N/mm}$$
Sum the cell torques. Each cell contributes $2A_iq_i$ by Bredt–Batho, so
$$T=2\left(A_1q_1+A_2q_2\right)=2\left(2\times62\,832\times200\right)$$
$$\boxed{T_{\max} = 5.027{\times}10^{7}\ \text{N}\!\cdot\!\text{mm} = 50.27\ \text{kN}\!\cdot\!\text{m}}$$
Because the flows are equal, this is identical to $2\pi R^2q$ for the undivided tube, which is a one-line independent check.
Compute the rate of twist. Applying the twist-rate integral to cell 1 and remembering that the dividing wall carries zero flow and so contributes nothing,
$$\frac{d\theta}{dx}=\frac{1}{2A_1G}\oint\frac{q\,ds}{t}=\frac{1}{2(62\,832)(80\,000)}\left[200\left(\frac{628.3}{10}\right)+0\left(\frac{400}{5}\right)\right]$$
$$\boxed{\frac{d\theta}{dx} = 1.25{\times}10^{-6}\ \text{rad/mm} = 0.0716^{\circ}\text{ per metre}}$$
Cell 2 returns the same number, as symmetry requires.
Cross-check with the torsion constant. Writing $T=GJ\,d\theta/dx$ gives $J=5.027{\times}10^{8}\ \text{mm}^4$, which is exactly the thin-ring result $2\pi R^{3}t_1$. This confirms that the dividing wall adds nothing to the torsional stiffness of a circular tube.
Say what the dividing wall is actually for. Its irrelevance here is a consequence of the perfect symmetry and of the loading being pure torsion. Make the cells unequal, change either skin gauge, or introduce a transverse shear load, and the wall immediately picks up the difference between the two cell flows. Its real structural purpose is to stabilise the skin against buckling and to carry shear when the section is bent, neither of which is examined by this question.