22-Mec-B9 Advanced Engineering Structures · May 2018
Question 1 of 8: Thermal stresses in a restrained two-segment rod
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
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 1: Thermal stresses in a restrained two-segment rod (20 marks)
Given. Two uniform linearly elastic rods are welded at B and built in to rigid supports at A and C, so the assembly cannot change its overall length. The temperature of both rods is raised by \(\Delta T = 60\,{}^{\circ}\text{C}\).
Quantity
Rod (1)
Rod (2)
Modulus E
150 GPa
95 GPa (see the note above)
Area A
2000 mm²
2600 mm²
Length L
1800 mm
1000 mm
Expansion coefficient α
8 × 10−6 /°C
9 × 10−6 /°C
Find. (a) the axial stress carried by each rod after the 60 °C rise, and (b) the direction and magnitude of the movement of the welded joint B.
Question 1 — the two-segment rod between rigid supports at A and C. Rod (1) is the longer, softer, slimmer segment; the weld at B is the joint whose movement part (b) asks for.
Approach. The structure is statically indeterminate to the first degree: release the support at C, let the bar grow freely by \(\alpha \Delta T L\), then apply the single unknown axial force F that pulls the free end back to its original position, and read the movement of B off whichever segment is convenient.
Free thermal growth of each segment. With the support at C removed, each rod lengthens by \(\delta_T = \alpha\,\Delta T\,L\):
$$\delta_{T1} = (8\times10^{-6})(60)(1800) = 0.864\ \text{mm}, \qquad \delta_{T2} = (9\times10^{-6})(60)(1000) = 0.540\ \text{mm}$$
so the released bar would grow by 1.404 mm in total.
Flexibility of the two rods in series. Because the same axial force runs through both segments, their flexibilities add:
$$f = \frac{L_1}{A_1E_1} + \frac{L_2}{A_2E_2} = \frac{1800}{(2000)(150\,000)} + \frac{1000}{(2600)(95\,000)} = 6.000\times10^{-6} + 4.049\times10^{-6} = 1.0049\times10^{-5}\ \text{mm/N}$$
Working consistently in N and mm keeps every modulus in MPa.
Compatibility gives the redundant force. The rigid supports demand zero net change of length, so the mechanical shortening must cancel the thermal growth:
$$\delta_{T1} + \delta_{T2} + F f = 0 \quad\Longrightarrow\quad F = -\frac{1.404}{1.0049\times10^{-5}} = \boxed{-139.7\ \text{kN}}$$
The minus sign says the bar is in compression, which is what a restrained expansion must produce.
Axial stresses (part a). One force, two areas:
$$\sigma_1 = \frac{F}{A_1} = \frac{-139\,721}{2000} = -69.9\ \text{MPa}, \qquad \sigma_2 = \frac{F}{A_2} = \frac{-139\,721}{2600} = -53.7\ \text{MPa}$$
Both rods are in compression; the slimmer rod (1) is the more highly stressed, and neither stress is anywhere near yield for a structural alloy.
Movement of joint B (part b). Track segment (1) from the fixed support at A: it grows thermally and is squashed elastically, and the movement of B is what survives:
$$u_B = \delta_{T1} + \frac{F L_1}{A_1E_1} = 0.864 + (-139\,721)(6.000\times10^{-6}) = 0.864 - 0.838 = \boxed{+0.026\ \text{mm}}$$
The result is positive, so B moves 0.026 mm to the right, that is toward C.
Independent check from the other end. Walking back from C gives \(u_B = -(\delta_{T2} + FL_2/A_2E_2) = -(0.540 - 0.566) = +0.026\ \text{mm}\), the same number from different data — the arithmetic and the sign convention are both sound.
The movement is tiny because the two segments are so nearly balanced: rod (1) wants to grow 0.864 mm and is pushed back 0.838 mm, so only 26 microns of net motion survive. That near-cancellation is exactly why the joint position is a sensitive question and the modulus ambiguity matters — taking the printed 95,000 GPa literally makes rod (2) effectively rigid, the force rises to 234 kN, and B is dragged 0.54 mm the other way.