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. 07-Str-A4, 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)
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
Quantity
Symbol
Value
Horizontal projection of each rafter
a
12.0 m
Apex rise above the supports
h
5.0 m
Rafter length
L
13.0 m
Distributed load (per m of projection)
w
8.45 kN/m
Settlement of joint ②
δ
12 mm downward
Flexural rigidity, both members
EI
5.33 × 10⁴ kN·m²
Find. The end moments, reactions, and the shear-force and
bending-moment diagrams of both members with their maxima and minima.
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.
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.
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.
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.
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
\(\psi_{12} = -\psi_{23}\).
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.
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.
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.
Question 7 bending moment. Both rafters hog at the apex and sag in the middle; the diagram closes to zero at the roller ③.