22-Mec-B9 Advanced Engineering Structures · December 2016
Question 8 of 8: Shear flow, shear centre and warping torque in an open I-section
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2016 — 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. — thin-walled open and closed sections, shear flow, shear centre, structural idealisation, single- and multi-cell torsion (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 non-circular and thin-walled members, unsymmetrical bending (Ch. 2, 4, 6).
A. P. Boresi and R. J. Schmidt, Advanced Mechanics of Materials, 6th ed. — torsion of multiply connected cells and of solid non-circular shafts (Ch. 6).
R. M. Jones, Mechanics of Composite Materials, 2nd ed. — orthotropic lamina stiffness, the reduced stiffness matrix and its transformation (Ch. 2).
N. E. Dowling, Mechanical Behavior of Materials, 4th ed. — strain-life fatigue, the Coffin–Manson relation and the Palmgren–Miner rule (Ch. 9, 14).
Question 8: Shear flow, shear centre and warping torque in an open I-section (20 marks)
Given. A deep I-section, symmetric about the horizontal ($z$) axis but with unequal flange projections either side of the web:
Given data — open section and loading
Quantity
Symbol
Value
Long flange projection (both flanges)
$b_L$
200 mm
Short flange projection (both flanges)
$b_R$
150 mm
Web depth, flange mid-plane to mid-plane
$h$
1 200 mm
Wall thickness, everywhere
$t$
2.5 mm
Applied vertical shear
$S$
23 kN upward
Find. The complete shear-flow distribution when the load passes through the shear centre, and then the maximum shear stress when the same load is instead applied on the web.
Figure 8.1 — the open I-section with unequal flange projections. The centroid C is on the web; the shear centre SC lies 15.91 mm toward the shorter (150 mm) projection.
Approach. Compute $I$, integrate the shear-flow equation outward from each free flange tip, close the walk at the web, and locate the shear centre from the couple formed by the unequal flange forces. For part (b), add the Saint-Venant torsional stress produced by moving the load onto the web.
Compute the second moment of area. The two flanges have identical total width $b_L + b_R = 350$ mm and sit at $y = \pm600$ mm, so$$I = \frac{t h^{3}}{12} + 2(b_L+b_R)t\left(\frac{h}{2}\right)^{2} = 360\times10^{6} + 630\times10^{6} = 990\times10^{6}\ \text{mm}^4 .$$Because the two flanges are identical, the section is symmetric about the horizontal axis, $I_{YZ} = 0$, and the ordinary shear-flow equation applies without any unsymmetrical-bending correction.
Walk the flange flows in from the free tips (part a). Starting from a tip, where $q = 0$, and integrating $q = -(S/I)\int y\,t\,\mathrm{d}s$ along a flange at constant $y = h/2$ gives a flow that grows linearly with distance from the tip. At the web junction,$$q_L = \frac{S}{I}\frac{h}{2}t\,b_L = \frac{23\,000}{990\times10^{6}}(600)(2.5)(200) = 6.97\ \text{N/mm},$$$$q_R = \frac{S}{I}\frac{h}{2}t\,b_R = 5.23\ \text{N/mm}.$$Both flow toward the web.
Continue down the web. The two flange flows merge at the top of the web, so it starts at$$q_{\text{top}} = q_L + q_R = 12.20\ \text{N/mm},$$and then grows parabolically as the web sweeps through the centroidal axis:$$q(y) = q_{\text{top}} + \frac{S t}{2I}\left[\left(\frac{h}{2}\right)^{2} - y^{2}\right].$$The maximum is at mid-height, $y = 0$:$$\boxed{q_{\max} = 12.20 + 10.45 = 22.65\ \text{N/mm},\qquad \tau_{\max} = \frac{22.65}{2.5} = 9.06\ \text{MPa}} .$$Integrating the web distribution confirms the statics — $q_{\text{top}}h + \tfrac23(q_{\max}-q_{\text{top}})h = 23\,000$ N — so the web alone carries the entire vertical shear, and the flanges carry none of it.
Locate the shear centre. The flange flows produce horizontal forces $H = Sht b^{2}/(4I)$ in each projection: $H_L = 697.0$ N in a long projection and $H_R = 392.0$ N in a short one. In the top flange both point away from the web, in the bottom flange both point toward it, so the projections form a couple of arm $h$. Equating that couple to $Se$,$$e = \frac{h^{2}t\left(b_L^{2} - b_R^{2}\right)}{4I} = \frac{(1200)^{2}(2.5)(200^{2}-150^{2})}{4(990\times10^{6})} = \boxed{15.91\ \text{mm toward the short flange}} .$$A cross-check from the couple directly, $(H_L - H_R)h/S = (697.0-392.0)(1200)/23\,000 = 15.91$ mm, agrees exactly. Note the direction: the shear centre moves toward the shorter projection, which is the same logic that puts a channel’s shear centre outside its web.
Move the load onto the web and find the torque (part b). Applying the same 23 kN on the web rather than 15.91 mm away from it superposes a torque$$T = S e = 23\,000(15.91) = 3.659\times10^{5}\ \text{N}\cdot\text{mm} = 366\ \text{N}\cdot\text{m}.$$An open section resists torque only by Saint-Venant shear, with torsion constant$$J = \frac{1}{3}\sum b_i t_i^{3} = \frac{(2\times350 + 1200)(2.5)^{3}}{3} = 9\,896\ \text{mm}^4 .$$
Add the torsional stress and report. The torsional shear stress on the wall surface is$$\tau_T = \frac{T\,t}{J} = \frac{3.659\times10^{5}(2.5)}{9\,896} = 92.4\ \text{MPa},$$which occurs on the surface of every 2.5 mm wall and therefore coincides at mid-web with the peak bending shear of 9.06 MPa. Adding them,$$\boxed{\tau_{\max} = 92.4 + 9.1 = 101.5\ \text{MPa, on the web surface at mid-height}} .$$The apparently trivial 15.91 mm offset multiplies the peak shear stress by more than eleven, because an open section is a catastrophically poor torsion member: $J$ is only 9 896 mm$^4$, some five orders of magnitude below the equivalent closed box.
Final results — Question 8
Quantity
Value
Second moment of area $I$
$990\times10^{6}$ mm$^4$
Flange flow at the web, long / short projection
6.97 / 5.23 N/mm (linear from zero at the tips)
Flow entering the top of the web
12.20 N/mm
Peak flow at mid-height (parabolic in the web)
22.65 N/mm
Peak shear stress, load through the shear centre
9.06 MPa
Shear centre offset
15.91 mm toward the 150 mm flange
Torque when the load moves onto the web
366 N·m
Torsion constant $J$
9 896 mm$^4$
Torsional shear stress
92.4 MPa
Combined peak shear stress (part b)
101.5 MPa
Check: part (b) assumes free (unrestrained) warping, so the whole torque is carried by uniform Saint-Venant shear. A real beam with a built-in end restrains warping, and for a deep I-section of this slenderness the warping-torsion contribution near the support can exceed the uniform-torsion term, raising the flange bending stresses considerably. The 101.5 MPa quoted here is therefore the correct answer to the question as posed, but a design check would also need the warping (Vlasov) analysis.