22-Mec-B9 Advanced Engineering Structures · May 2018
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Exams, May 2018 — 16-Mec-B9 Advanced Engineering Structures. Three hours, open book, any non-communicating calculator permitted. Eight questions are printed, each worth 20 marks, and the rubric states that any five constitute a complete exam paper. All eight are worked here. Marks for the individual parts are those printed inside each problem.
Reference texts. T. H. G. Megson, Aircraft Structures for Engineering Students, 6th ed. (thin-walled open and closed sections, shear flow, shear centre, multi-cell torsion, crack growth and Miner cumulative damage); A. P. Boresi and R. J. Schmidt, Advanced Mechanics of Materials, 6th ed. (yield criteria, unsymmetrical bending, torsion of non-circular sections, shear centre); N. E. Dowling, Mechanical Behavior of Materials, 4th ed. (Paris law, Coffin–Manson, Palmgren–Miner); R. C. Hibbeler, Mechanics of Materials, 10th ed. (statically indeterminate axial members, thermal stress).
Check: the modulus printed for rod (2) in Question 1. The paper prints E2 = 95,000 GPa. No solid has a Young’s modulus of that order — diamond, the stiffest bulk material known, reaches about 1,200 GPa — so the value as printed is not physically realisable and is almost certainly a units slip for 95,000 MPa = 95 GPa, a figure entirely typical of an aluminium alloy and consistent with the way E1 = 150 GPa is written on the same line. Question 1 is therefore worked at E2 = 95 GPa, and the answers obtained by taking the printed number literally are carried alongside in the results table, because the two readings give opposite answers to part (b). Under the paper’s own instruction 1, a candidate should record this assumption with the answer script.
Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.
Given. A three-cell rectangular thin-wall box, 180 mm deep, with cell widths 120, 250 and 120 mm, carrying a constant clockwise torque.
| Quantity | Value |
|---|---|
| Applied torque T | 10,000 N·m = 10 × 106 N·mm |
| Shear modulus G | 15 GPa |
| Upper panels | 2.5 mm thick |
| Lower panels | 2.0 mm thick |
| Vertical panels (end webs and interior webs) | 1.5 mm thick |
| Enclosed areas A1, A2, A3 | 21,600 / 45,000 / 21,600 mm² |
Find. (a) the three cell shear flows q1, q2, q3, and (b) the magnitude and location of the largest shear stress in the box.
Approach. Pure torsion of a multi-cell box is one equilibrium equation short, so write the torque equation plus the compatibility statement that all three cells twist at the same rate, and solve the three equations for the three circulating flows.
| Wall | q (N/mm) | t (mm) | τ (MPa) |
|---|---|---|---|
| Centre lower panel | 64.93 | 2.0 | 32.46 |
| End webs | 48.11 | 1.5 | 32.07 |
| Centre upper panel | 64.93 | 2.5 | 25.97 |
| Outer lower panels | 48.11 | 2.0 | 24.05 |
| Outer upper panels | 48.11 | 2.5 | 19.24 |
| Interior webs | 16.82 | 1.5 | 11.21 |
The result is a useful piece of design intuition. The thinnest walls in the box are the 1.5 mm webs, yet the interior webs are the quietest walls in the section at 11.2 MPa, because they see only the small difference between two similar circulating flows. The end webs, by contrast, carry the whole of \(q_1\) and are within 1.2 per cent of the peak. In a multi-cell box it is the outer skin and the end webs that size the section, not the internal ones.
| Quantity | Value |
|---|---|
| (a) q1 | 48.11 N/mm |
| (a) q2 | 64.93 N/mm |
| (a) q3 | 48.11 N/mm |
| Flow carried by each interior web | 16.82 N/mm |
| (b) Maximum shear stress | 32.5 MPa, in the 2.0 mm lower panel of the centre cell |
| Runner-up (end webs, 1.5 mm) | 32.07 MPa |
| Rate of twist | 1.381 × 10−5 rad/mm (0.79° per metre) |