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16-Civ-B1 Advanced Structural Analysis · December 2019

Question 3 of 9: Least work applied to two cantilevers joined by a tension member

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Examination, December 2019 — 16-Civ-B1 Advanced Structural Analysis, 3 hours, CLOSED BOOK (an approved Casio or Sharp calculator only). Nine questions on seven pages: Questions 1 and 2 are compulsory (8 and 12 marks); the candidate then answers TWO of Questions 3, 4 or 5 (18 marks each) and TWO of Questions 6, 7, 8 or 9 (22 marks each), so six questions make a complete paper of 100 marks. Because this set is a study resource, all nine questions are solved here.

Reference texts. R. C. Hibbeler, Structural Analysis, 10th ed. (Pearson) — Ch. 6 influence lines, Ch. 8–9 deflections and virtual work, Ch. 10 force (flexibility) method, Ch. 11 slope-deflection, Ch. 12 moment distribution, Ch. 15–16 matrix stiffness. A. Kassimali, Structural Analysis, 6th ed. (Cengage) — Ch. 7 Castigliano and least work, Ch. 8 influence lines, Ch. 13 slope-deflection, Ch. 17–18 matrix stiffness. A. Ghali, A. M. Neville and T. G. Brown, Structural Analysis: A Unified Classical and Matrix Approach, 7th ed. (CRC). Canadian context for the settlement question: NBC 2020 Part 4 and CSA S6:19 treat differential support settlement as an imposed deformation to be combined with the permanent loads, so the self-equilibrating moment set computed in Question 6 is a real design action, not a curiosity.

Sign convention used throughout. End moments are written counter-clockwise-positive on the member, which is the convention that matches the standard six-degree-of-freedom element stiffness matrix; the slope-deflection equation is then $M_{ij} = \dfrac{2EI}{L}\left(2\theta_i + \theta_j - 3\psi_{ij}\right) + \mathrm{FEM}_{ij}$ with $\psi$ the counter-clockwise chord rotation and, for a downward UDL, $\mathrm{FEM}_{ij} = +wL^2/12$, $\mathrm{FEM}_{ji} = -wL^2/12$. Ordinary sagging bending moments, which is what every diagram below plots, are recovered as $M_{\text{sag}}(i) = -M_{ij}$ and $M_{\text{sag}}(j) = +M_{ji}$. Mixing this with the clockwise-positive convention of some textbooks produces clean-looking integers that are wrong.

Question 3: Least work applied to two cantilevers joined by a tension member (18 marks)

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.

QuantitySymbolValue
Span of each cantilever beam$L$6 m
Length of the vertical tie$h$5 m
UDL on the lower beam (3)–(4)$w$8 kN/m
Flexural rigidity of both beams$EI$ $1.8\times10^{5}\ \text{kN}\cdot\text{m}^2$
Axial rigidity of the tie (2)–(4)$AE$ $5.0\times10^{4}\ \text{kN}$

Find. The bending moment and the shear force in beam (3)–(4) at its built-in left end, joint (3).

8 kN/m12346 m5 m
Question 3: two 6 m cantilevers built into the wall at (1) and (3), joined at their tips by a 5 m pin-ended tension member.

Approach. The structure is once redundant. Take the axial force $S$ in the pin-ended tie as the redundant, write the total strain energy of the two beams plus the tie in terms of $S$, and impose the least-work condition $\partial U/\partial S = 0$; the tie is a two-force member, so its own extension must be included — that term is what stops the answer being the rigid-prop value.

  1. Identify the redundant and the internal forces. Both beams are built in at the wall and free at their tips; the only connection between them is the pin-ended vertical member, which can carry axial force alone. Calling that force $S$ (tension positive), the tie pulls the lower tip up and the upper tip down. Measuring $x$ from each free end, $$M_{\text{lower}}(x) = Sx - \tfrac{1}{2}wx^{2},\qquad M_{\text{upper}}(x) = -Sx$$ so that $\partial M_{\text{lower}}/\partial S = x$ and $\partial M_{\text{upper}}/\partial S = -x$.
  2. Write the least-work condition. With the beams inextensible, the strain energy is bending in the two beams plus axial in the tie, and Castigliano's second theorem applied to the redundant gives $$\frac{\partial U}{\partial S} = \frac{1}{EI}\int_0^L M\, \frac{\partial M}{\partial S}\,\mathrm{d}x \;+\; \frac{Sh}{AE} = 0 .$$ Substituting the two moment expressions, $$\frac{1}{EI}\int_0^{L}\!\left(Sx - \tfrac{1}{2}wx^{2}\right)x\,\mathrm{d}x +\frac{1}{EI}\int_0^{L}\!\left(-Sx\right)\left(-x\right)\mathrm{d}x +\frac{Sh}{AE} = 0 .$$
  3. Evaluate the integrals. Each bending integral contributes $SL^{3}/3$, and the load term contributes $-wL^{4}/8$, so $$S\left(\frac{2L^{3}}{3EI} + \frac{h}{AE}\right) = \frac{wL^{4}}{8EI}.$$ This is a flexibility statement in disguise: the bracket is the relative vertical flexibility of the two tips plus the stretch of the tie, and the right side is the free deflection of the loaded tip.
  4. Insert the numbers. With $L = 6\ \text{m}$, $h = 5\ \text{m}$, $w = 8\ \text{kN/m}$: $$\frac{2L^{3}}{3EI} = \frac{2(216)}{3(1.8\times10^{5})} = 8.000\times10^{-4}\ \text{m/kN},\qquad \frac{h}{AE} = \frac{5}{5.0\times10^{4}} = 1.000\times10^{-4}\ \text{m/kN}$$ $$\frac{wL^{4}}{8EI} = \frac{8(1296)}{8(1.8\times10^{5})} = 7.200\times10^{-3}\ \text{m}$$ so that $$S = \frac{7.200\times10^{-3}}{9.000\times10^{-4}} = \boxed{8.00\ \text{kN}\ \ (\text{tension})}$$ The tie stretch accounts for one ninth of the total flexibility; ignoring it (that is, treating the tie as a rigid prop) would give $S = 7.200\times10^{-3}/8.000\times10^{-4} = 9.00\ \text{kN}$, an error of 12.5 per cent in the wrong direction.
  5. Return to the loaded beam and take the free body. Beam (3)–(4) is now a determinate cantilever carrying the UDL downwards over 6 m and the tie force upwards at its tip. Vertical equilibrium of the whole member gives the shear at the wall, $$V_3 = wL - S = 8(6) - 8.00 = \boxed{40.0\ \text{kN}}$$ and moments about joint (3) give $$M_3 = -\frac{wL^{2}}{2} + SL = -\frac{8(36)}{2} + 8.00(6) = \boxed{-96.0\ \text{kN}\cdot\text{m}\ \ (\text{hogging})}$$ The negative sign says the top fibre of the lower beam is in tension at the wall, as a cantilever must be. For completeness the upper beam carries a pure tip load of 8.00 kN downwards, so its wall moment is $-8.00(6) = -48.0\ \text{kN}\cdot\text{m}$ and its wall shear is 8.00 kN.
  6. Check the answer two ways. First, the load path: of the $48.0\ \text{kN}$ applied to the lower beam, $40.0\ \text{kN}$ goes directly into wall (3) and $8.00\ \text{kN}$ is hung off the upper beam through the tie — the two wall shears sum to the applied load. Second, compatibility: the tip of the lower beam moves down by $wL^{4}/8EI - SL^{3}/3EI = 7.200\times10^{-3} - 3.200\times10^{-3} = 4.000\times10^{-3}\ \text{m}$, the tip of the upper beam moves down by $SL^{3}/3EI = 3.200\times10^{-3}\ \text{m}$, and the difference, $0.800\times10^{-3}\ \text{m}$, is exactly the extension $Sh/AE$ of the tie.
QuantitySymbolResult
Axial force in the vertical member (2)–(4)$S$ 8.00 kN tension
Shear force at the left end of beam (3)–(4)$V_3$ 40.0 kN
Bending moment at the left end of beam (3)–(4)$M_3$ 96.0 kN·m hogging
Wall moment in the upper beam (1)–(2)$M_1$ 48.0 kN·m hogging
Extension of the tie$Sh/AE$0.80 mm
-96.0 (at 3)0 (at 4)BMD of the loaded beam 3-4 (kN.m, x measured from 4)
Question 3: bending moment in the loaded beam (3)-(4), measured from the free end (4). Hogging throughout, 96.0 kN.m at the wall.