22-Mec-B9 Advanced Engineering Structures · December 2014
Question 1 of 8: Shear flow, shear centre and torsion of an open I-section
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2014 — 07-Mec-B9 Advanced Engineering Structures. Three hours, open book, any non-communicating calculator permitted. Eight questions of equal total value (20 marks each); the rubric states that any five constitute a complete paper. All eight are solved here, because the complete set is the study resource.
Reference texts.
T. H. G. Megson, Aircraft Structures for Engineering Students, 6th ed. — open and closed thin-walled sections, shear flow, shear centre, structural idealisation (Ch. 16, 17, 18, 20, 21, 23).
A. C. Ugural and S. K. Fenster, Advanced Strength and Applied Elasticity, 5th ed. — yield criteria, torsion of thin-walled members, statically indeterminate axial members (Ch. 2, 4, 6).
A. P. Boresi and R. J. Schmidt, Advanced Mechanics of Materials, 6th ed. — torsion of open and closed sections, multiply connected cells (Ch. 6).
N. E. Dowling, Mechanical Behavior of Materials, 4th ed. — linear elastic fracture mechanics, the Paris law, strain-life and Miner’s rule (Ch. 8, 11, 14).
R. C. Hibbeler, Mechanics of Materials, 10th ed. — thermal stress in restrained members and combined loading (Ch. 4, 8).
Axes and sign convention used throughout. A right-handed set is used for every thin-walled question: the span axis runs along the member, $Y$ is vertical (upward) in the cross-section and $Z$ is horizontal. Section constants are written $I_{ZZ}=\int Z^{2}\,dA$, $I_{YY}=\int Y^{2}\,dA$ and $I_{YZ}=\int ZY\,dA$ about the centroid, and the bending stress is carried as the linear field $\sigma = aZ + bY$. Shear flows are counted positive in the direction of the walk stated with each figure; a negative answer simply means the flow runs the other way round the circuit.
Question 1: Shear flow, shear centre and torsion of an open I-section (20 marks)
Given. An open I-section whose two flanges are identical but are not centred on the web: from the figure each flange runs 250 mm to one side of the web and 125 mm to the other, so the section is symmetric about the horizontal ($z$) axis only.
Quantity
Symbol
Value
Long flange projection
$b_L$
250 mm
Short flange projection
$b_R$
125 mm
Web depth (mid-plane to mid-plane)
$h$
320 mm
Wall thickness (all walls)
$t$
3 mm
Applied vertical shear, upward, through the shear centre
$S_y$
25 kN
Find. (a) the complete shear-flow distribution in the flanges and web, (b) the horizontal distance from the web to the shear centre, and (c) the largest shear stress anywhere in the section once the same 25 kN is moved onto the web centre-line.
Figure Q1 — the open I-section. The flanges are identical top and bottom, so the horizontal axis through mid-depth is a principal axis, but the unequal projections push the shear centre 54.7 mm away from the web, toward the short flange.
Approach. Because the section is symmetric about the horizontal axis, $I_{YZ}=0$ and the open-section shear flow reduces to $q_s = (S_y/I_{ZZ})\int_0^s t\,Y\,ds$ walked from each free edge; the four flange forces then form a couple whose arm is the web depth, and equating that couple to $S_y e$ locates the shear centre, after which moving the load onto the web adds a St Venant torque to the same bending shear flow.
Part (a) — second moment of area about the horizontal centroidal axis. The centroid sits at mid-depth by symmetry. Adding the web, the two flanges shifted to $Y=\pm h/2$, and the flanges’ own (negligible) inertia, $$I_{ZZ} = \frac{t h^{3}}{12} + 2\,(b_L+b_R)t\left(\frac{h}{2}\right)^{2} + 2\,\frac{(b_L+b_R)t^{3}}{12}$$Substituting $t=3$, $h=320$, $b_L+b_R=375$ mm gives $8.192\times10^{6} + 57.600\times10^{6} + 1.7\times10^{3}$, so $$\boxed{I_{ZZ} = 65.79\times10^{6}\ \text{mm}^{4}}$$
Flange shear flow, walked from each free tip. A flange lies at constant $Y = h/2 = 160$ mm, so the first moment grows linearly with the distance $s$ from the tip and $$q(s) = \frac{S_y}{I_{ZZ}}\,t\,\frac{h}{2}\,s = \frac{25\,000}{65.79\times10^{6}}(3)(160)\,s = 0.1824\,s \ \text{N/mm}$$The flow therefore rises from zero at each tip to $q_L = 0.1824(250) = 45.60$ N/mm where the long flange meets the web and to $q_R = 0.1824(125) = 22.80$ N/mm at the short-flange junction. Because both halves of the top flange drain toward the web, the flow entering the web at the top is their sum, $68.40$ N/mm; the bottom flange is the mirror image with the flow running outward.
Web shear flow and its peak. Continuing down the web from the top junction, each strip of web adds its own first moment, so $$q(Y) = q_{\text{top}} + \frac{S_y t}{2 I_{ZZ}}\left[\left(\frac{h}{2}\right)^{2} - Y^{2}\right]$$which is parabolic and peaks at mid-depth ($Y=0$): $q_{\max} = 68.40 + (3.800\times10^{-4})(3)(160^{2}/2)$, that is $$\boxed{q_{\max} = 82.99\ \text{N/mm}\quad\text{at web mid-depth}}$$Dividing by the 3 mm wall, the bending shear stress peaks at $\tau = 82.99/3 = 27.66$ MPa. As a check on the whole distribution, integrating $q(Y)$ over the 320 mm web returns 25.0 kN — the web carries the entire vertical shear, as it must for a section with horizontal flanges.
Part (b) — the flange forces that locate the shear centre. Integrating the linear flange flow gives a force $F = \tfrac{1}{2}q_{\text{junction}}\,b$ in each flange half. The long and short halves of one flange pull in opposite directions, so each flange delivers a net horizontal force $$\Delta F = \frac{S_y t h}{4 I_{ZZ}}\left(b_L^{2}-b_R^{2}\right) = 4\,275\ \text{N}$$The top flange pushes one way and the bottom flange the other, so the two form a couple of arm $h$.
Shear-centre offset. Equating that couple to the moment of the applied shear about the web, $S_y e = h\,\Delta F$, gives the closed form $e = h^{2}t\,(b_L^{2}-b_R^{2})/(4 I_{ZZ})$ and $$\boxed{e = 54.72\ \text{mm from the web, on the side of the 125 mm (short) flange}}$$The direction is the usual channel result seen from a different angle: the longer flange half carries the larger flange force, so the shear centre retreats away from it.
Part (c) — the torque introduced by moving the load to the web. Applying the same 25 kN on the web centre-line is statically the shear-centre case plus a torque $$T = S_y e = 25\,000 \times 54.72 = 1.368\times10^{6}\ \text{N}\cdot\text{mm}$$An open section resists this only in St Venant torsion, with $J = \sum b t^{3}/3 = (2\times375 + 320)(3)^{3}/3 = 9\,630$ mm4 — nearly four orders of magnitude below $I_{ZZ}$ (a ratio of about 6 800).
Maximum shear stress under the eccentric load. The torsional shear stress is uniform through the thickness in magnitude and peaks at the wall surface, $\tau_T = T t / J = (1.368\times10^{6})(3)/9\,630 = 426.1$ MPa. At mid-depth of the web the torsional and bending shear stresses act along the same line on one face, so they add: $$\boxed{\tau_{\max} = 426.1 + 27.7 = 453.8\ \text{MPa}}$$That is a factor of 16 above the shear stress the same load causes when it passes through the shear centre.
Check: part (c) assumes free (unrestrained) warping, which is the standard St Venant assumption for an open section and the conservative one. A real beam built into a support develops warping restraint, which reduces the twist and the torsional shear stress but adds axial warping normal stresses; the 454 MPa figure also far exceeds the shear yield strength of any structural steel, which is exactly the point of the question — an open section must not be loaded off its shear centre.