22-Mec-B9 Advanced Engineering Structures · December 2017
Question 7 of 8: Torsion of a three-cell thin-walled box
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2017 — 16-Mec-B9
Advanced Engineering Structures. Three hours, open book, any non-communicating
calculator permitted. The paper prints eight questions of equal value (20 marks each) and
states that any five constitute a complete exam paper. All eight are solved below,
because the set is a study resource rather than a sitting.
Reference texts.
T. H. G. Megson, Aircraft Structures for Engineering Students, 6th ed. —
unsymmetrical bending, shear flow in open and closed thin-walled sections, shear centre,
structural idealisation, single- and multi-cell torsion (Ch. 15, 16, 17, 20, 23).
A. C. Ugural and S. K. Fenster, Advanced Strength and Applied Elasticity, 5th ed.
— three-dimensional states of stress, principal stresses, the Tresca and von Mises yield
criteria (Ch. 1, 4).
A. P. Boresi and R. J. Schmidt, Advanced Mechanics of Materials, 6th ed. —
shear centre, torsion of multiply connected cells, column stability (Ch. 6, 12).
N. E. Dowling, Mechanical Behavior of Materials, 4th ed. — strain-life
fatigue, the Coffin–Manson relation, the Palmgren–Miner rule and Paris-law crack
growth (Ch. 9, 11, 14).
R. C. Hibbeler, Mechanics of Materials, 10th ed. — Euler buckling of
pin-ended columns, slenderness ratio and the transition slenderness (Ch. 13).
Sign convention used throughout. A single right-handed frame is used
for every thin-walled question: x runs along the span from the root to the free end,
Y is vertically upward and Z horizontally to the right, both measured from the
section centroid. Direct stress is written $\sigma_x = aZ + bY$, and the two coefficients follow
from $aI_{ZZ} + bI_{YZ} = M_Y$ and $aI_{YZ} + bI_{YY} = M_Z$, in which
$I_{ZZ}=\int Z^{2}\,dA$, $I_{YY}=\int Y^{2}\,dA$, $I_{YZ}=\int ZY\,dA$,
$M_Y \equiv \int \sigma_x Z\,dA$ and $M_Z \equiv \int \sigma_x Y\,dA$. This one pair of
equations replaces the memorised unsymmetrical-bending fraction and is self-checking: for a
cantilever carrying a tip load, the fibres on the side the load points toward must go into
compression.
Question 7: Torsion of a three-cell thin-walled box (20 marks)
Given. A rectangular box 200 mm deep, divided by two interior
webs into three cells 160, 300 and 160 mm wide, carrying pure torque.
Given data — three-cell torque box
Quantity
Symbol
Value
Cell widths (left, centre, right)
$b_1,b_2,b_3$
160, 300, 160 mm
Box depth
$h$
200 mm
Upper skin thickness
$t_u$
2.0 mm
Lower skin thickness
$t_l$
1.5 mm
All vertical webs
$t_w$
1.0 mm
Shear modulus
$G$
20 GPa
Applied torque
$T$
15 000 N·m = $1.5\times10^{7}$
N·mm
Find. (a) the constant shear flow circulating in each of the three cells;
(b) the largest shear stress anywhere in the box and the wall in which it occurs.
The three-cell box. Each cell carries its own circulating flow; an
interior web is shared by two cells and therefore carries only the difference between
their flows, which is why the interior webs turn out to be the quietest walls in the
section.
Approach. Write the rate of twist of each cell in terms of its own
circulating flow and those of its neighbours, set the three rates equal (the section is rigid in
its own plane, so every cell twists together), add the torque equilibrium equation and solve the
resulting four-by-four system.
Part (a) — set up the cell areas and line integrals. The enclosed
areas are $A_1 = A_3 = 160(200) = 32\,000$ mm$^{2}$ and $A_2 = 300(200) = 60\,000$ mm$^{2}$. The
line integral $\oint \mathrm{d}s/t$ around each cell's own boundary is
$$\delta_1 = \delta_3 = \frac{160}{2.0}+\frac{160}{1.5}+\frac{2(200)}{1.0} = 586.7, \qquad
\delta_2 = \frac{300}{2.0}+\frac{300}{1.5}+\frac{2(200)}{1.0} = 750,$$
while each interior web contributes $200/1.0 = 200$ to the coupling between adjacent cells.
Write the rate of twist of each cell. For cell $i$,
$$\frac{\mathrm{d}\theta}{\mathrm{d}x} = \frac{1}{2A_iG}
\left[\delta_i q_i - \sum_{j\ \text{adjacent}} \frac{h}{t_w} q_j\right],$$
in which the negative terms account for the neighbouring cell's flow running the opposite way
through the shared web.
Impose compatibility and equilibrium. All three cells must twist at the same
rate, giving two independent equations, and the torque is carried by the Bredt sum
$$T = 2\sum_i A_i q_i = 2\left(32\,000\,q_1 + 60\,000\,q_2 + 32\,000\,q_3\right).$$
Symmetry of both geometry and thickness about the centre line requires $q_1 = q_3$ before any
arithmetic is done, which is a useful check on the solution.
Solve the system. Equating the twist of cell 1 to that of cell 2 reduces to
$24\,000\,q_1 = 18\,000\,q_2$, i.e. $q_2 = \tfrac{4}{3}q_1$. Substituting into the torque
equation, $128\,000\,q_1 + 120\,000\left(\tfrac43 q_1\right) = 1.5\times10^{7}$, so
$$\boxed{q_1 = q_3 = 52.08\ \text{N/mm}, \qquad q_2 = 69.44\ \text{N/mm}}$$
Back-substituting gives $2\sum A_iq_i = 1.5\times10^{7}\ \text{N}\cdot\text{mm}$ exactly, which
confirms the solution.
Recover the rate of twist. Substituting into any one cell equation,
$\mathrm{d}\theta/\mathrm{d}x = 1.302\times10^{-5}$ rad/mm, that is $0.746^{\circ}$ per metre of
span — a useful figure because torsional stiffness, not strength, often governs a wing
box.
Part (b) — tabulate the stress in every wall type. Shear stress is
$\tau = q/t$ evaluated wall by wall, and the six distinct wall types give
$$\begin{aligned}
\text{outer webs (1.0 mm)} &: 52.08\ \text{MPa}, & \text{centre lower skin (1.5 mm)}
&: 46.30\ \text{MPa}, \\
\text{centre upper skin (2.0 mm)} &: 34.72\ \text{MPa}, & \text{end lower skins (1.5 mm)}
&: 34.72\ \text{MPa}, \\
\text{end upper skins (2.0 mm)} &: 26.04\ \text{MPa}, & \text{interior webs (1.0 mm)}
&: 17.36\ \text{MPa}.
\end{aligned}$$
Identify the maximum. The largest value is
$$\boxed{\tau_{\max} = 52.08\ \text{MPa, in the two outer vertical webs}}$$
because those walls combine the full flow of an end cell with the thinnest gauge in the section.
The centre cell carries the higher flow, but its thinnest wall is the 1.5 mm lower skin, which
reaches only 46.30 MPa.
Note where the section is least stressed. The interior webs carry
only $q_2-q_1 = 17.36$ N/mm, a third of the outer webs, because the two adjacent circulations
largely cancel there. This is the standard argument for why interior webs in a multi-cell box are
sized by buckling and by their role in carrying bending shear, not by torsion.