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16-Civ-B1 Advanced Structural Analysis · December 2018

Question 7 of 9: Slope-deflection — gable frame with load and support settlement

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

Notes on this paper

National Examinations — December 2018. 16-Civ-B1, Advanced Structural Analysis. Three hours, closed book (approved Casio or Sharp calculator only). Nine questions on seven pages: Questions 1 and 2 are compulsory (12 and 8 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 support-settlement questions: NBC 2020 Part 4 and CSA S6:19 treat differential settlement as an imposed deformation to be combined with the permanent loads, so the self-equilibrating moment sets computed in Questions 1(c), 5 and 7 are real design actions, not curiosities.

Check: representative dimensions in Questions 1 and 2. The source prints no dimensions on any of the five structures in Questions 1 and 2 — they are labelled “schematically show”. Every shape, every zero and every discontinuity below is dimension-independent and is what the marker is looking for. To put real numbers on the ordinates, representative dimensions have been adopted in the drawn proportions and are stated with each part; they are declared here rather than presented as data read off the paper.

Question 7: Slope-deflection — gable frame with load and support settlement (22 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. A two-member gable: joint ① is built in at ground level, joint ② is the apex 5 m higher carrying a roller support, and joint ③ is a roller back at ground level. Each rafter spans 12 m horizontally, so each is 13 m long. The uniformly distributed load of 8.45 kN/m is drawn as a horizontal band across the full 24 m and is therefore per metre of horizontal projection.

Given data
QuantitySymbolValue
Horizontal projection of each raftera12.0 m
Apex rise above the supportsh5.0 m
Rafter lengthL13.0 m
Distributed load (per m of projection)w8.45 kN/m
Settlement of joint ②δ12 mm downward
Flexural rigidity, both membersEI5.33 × 10⁴ kN·m²

Find. The end moments, reactions, and the shear-force and bending-moment diagrams of both members with their maxima and minima.

w = 8.45 kN/m of horizontal projection12312 m + 12 m horizontally, apex 5 m above the supportsjoint 2 settles 12 mm
Question 7 — built in at ①, roller at the apex ② and roller at ③. The load band spans the full horizontal projection, not the rafter length.

Approach. Resolve the projected load into the rafter transverse intensity, get the fixed-end moments from the projection, obtain the translations from inextensibility (there is no free sway unknown), then solve two joint equations for the two unknown rotations.

  1. Reduce the projected load. A vertical load of w per horizontal metre becomes \(w\cos^{2}\alpha\) per metre normal to a rafter, with \(\cos\alpha = 12/13\): $$w_{\perp} = 8.45\left(\dfrac{12}{13}\right)^{2} = 7.20\ \text{kN/m}$$ and the fixed-end moment collapses to a projection-only formula: $$\text{FEM} = \dfrac{w_{\perp}L^{2}}{12} = \dfrac{w a^{2}}{12} = \dfrac{8.45 \times 144}{12} = \boxed{101.40\ \text{kN}\cdot\text{m}}$$ Note which length goes where: the projection sets the fixed-end moment, the true 13 m length sets the member stiffness. Interchanging them is the standard error on sloping members.
  2. Fix the translations by inextensibility. Joint ① is built in, so member ①–② can only stay 13 m long if $$u_{2} = -\dfrac{h}{a}v_{2} = \dfrac{5}{12}(0.012) = \boxed{5.00\ \text{mm}}$$ and applying the same condition to the second rafter, with \(v_{3} = 0\) at its roller, gives \(u_{3} = 10.00\) mm. There is no independent sway unknown: the two rollers plus inextensibility determine every translation from the single imposed settlement.
  3. Chord rotations. $$\psi_{12} = \dfrac{(0.005)(-5) + (-0.012)(12)}{13^{2}} = -1.000 \times 10^{-3}, \qquad \psi_{23} = +1.000 \times 10^{-3}$$ Equal and opposite — the frame flattens symmetrically about the apex.
  4. Write the slope-deflection equations. With \(k = 2EI/L = 8200\) kN·m and \(\theta_{1} = 0\) at the built-in end, $$M_{12} = k(\theta_{2} - 3\psi_{12}) + 101.40, \qquad M_{21} = k(2\theta_{2} - 3\psi_{12}) - 101.40$$ $$M_{23} = k(2\theta_{2} + \theta_{3} - 3\psi_{23}) + 101.40, \qquad M_{32} = k(2\theta_{3} + \theta_{2} - 3\psi_{23}) - 101.40$$
  5. Two equilibrium conditions. Joint ② must balance and joint ③ is a roller end, so $$M_{21} + M_{23} = 0 \;\Rightarrow\; 4\theta_{2} + \theta_{3} = 0 \;\Rightarrow\; \theta_{3} = -4\theta_{2}$$ $$M_{32} = 0 \;\Rightarrow\; 2\theta_{3} + \theta_{2} = 3\psi_{23} + \dfrac{101.40}{k}$$ The first is remarkably clean: the fixed-end moments and the chord-rotation terms cancel identically between the two members because \(\psi_{12} = -\psi_{23}\).
  6. Solve. $$-7\theta_{2} = 3(0.001) + 0.0123659 \;\Rightarrow\; \theta_{2} = -2.1951 \times 10^{-3}\ \text{rad}, \qquad \theta_{3} = +8.7805 \times 10^{-3}\ \text{rad}$$
  7. End moments and reactions. $$M_{12} = \boxed{108.0\ \text{kN}\cdot\text{m}}, \quad M_{21} = -112.8, \quad M_{23} = +112.8, \quad M_{32} = 0$$ $$V_{1} = 50.30\ \text{kN}, \quad V_{2} = 111.20\ \text{kN}, \quad V_{3} = 41.30\ \text{kN}$$ which sum to \(8.45 \times 24 = 202.8\) kN. Both rollers are vertical-only and the load is vertical, so the horizontal reaction at the built-in end is exactly zero — a one-line check that the whole solution passes.
  8. Diagrams. Member ①–② starts at −108.0 kN·m, reaches a sagging peak of +41.71 kN·m at 6.45 m along the rafter, and ends at −112.8 kN·m at the apex, its transverse shear running from +46.43 kN to −47.17 kN. Member ②–③ starts at −112.8 kN·m, peaks at \(\boxed{+100.93\ \text{kN}\cdot\text{m}}\) at 7.71 m and closes at zero on the roller, with shear from +55.48 kN to −38.12 kN.
  9. Separate the two causes. Running the load alone and the settlement alone shows how modest the settlement contribution is here: the base moment splits 86.91 kN·m from the load and 21.09 kN·m from the 12 mm drop. Quoting the split costs one extra analysis and tells the designer whether tightening the foundation tolerance would be worth anything.
-108.0+41.71-112.8+100.93Bending moment (kN·m), ordinates normal to each member
Question 7 bending moment. Both rafters hog at the apex and sag in the middle; the diagram closes to zero at the roller ③.
Question 7 — results
QuantityValue
Transverse load intensity on a rafter7.20 kN/m
Fixed-end moment (w a²/12)101.40 kN·m
u2 / u3 from inextensibility5.00 / 10.00 mm outward
θ2 / θ3−2.1951 / +8.7805 (×10−3 rad)
Moment at the built-in end ①108.0 kN·m (minimum, hog)
Moment at the apex ②112.8 kN·m (minimum, both members)
Max sagging, member ①–②+41.71 kN·m at 6.45 m
Max sagging, member ②–③+100.93 kN·m at 7.71 m (maximum)
Shear, member ①–②+46.43 to −47.17 kN
Shear, member ②–③+55.48 to −38.12 kN
Reactions ① / ② / ③50.30 / 111.20 / 41.30 kN
Base moment split (load / settlement)86.91 / 21.09 kN·m