Question 5 of 9: Slope-deflection — trapezoidal frame with a settling support
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 5: Slope-deflection — trapezoidal frame with a settling support (18 marks)
Given. A symmetric trapezoidal frame. Joint ① is
a roller at ground level; joint ② is a pin support at the top-left corner;
joint ③ is a roller support at the top-right corner; joint ④ is a
roller at ground level. The inclined legs rise 3.6 m over a 4.8 m run (6.0 m long,
a 3-4-5 triangle) and the top member spans 8.0 m.
Given data
Quantity
Symbol
Value
Leg length (rise 3.6 m, run 4.8 m)
L12, L34
6.0 m
Top member
L23
8.0 m
Imposed settlement of joint ③
δ
12.0 mm downward
Flexural rigidity, all members
EI
3.6 × 10⁵ kN·m²
Applied loads
—
none
Find. The end moments, reactions, shear-force and
bending-moment diagrams produced by the imposed settlement alone.
Question 5 — roller, pin, roller, roller. Five reaction components against three equations makes the frame two degrees indeterminate, which is exactly why an imposed settlement stresses it.
Approach. With no external load the entire answer comes
from kinematics: fix the imposed and inextensibility-driven displacements first,
convert them to chord rotations, then write two joint-moment equations in the two
unknown rotations. Both outer joints are single-member ends free to rotate, so use
the modified stiffness 3EI/L there and drop their rotations from the unknowns.
Fix the displacement field. The pin at ② holds that joint
in both directions. The top member is inextensible and horizontal, so
\(u_{3} = u_{2} = 0\); the left leg is inextensible with both its ends already
fixed vertically, so \(u_{1} = 0\). Only joint ④ can move, and the
inextensible right leg forces
$$u_{4} = \dfrac{\delta\,h}{r} = \dfrac{0.012 \times 3.6}{4.8}
= \boxed{9.00\ \text{mm outward}}$$
This spreading of the base is the physical heart of the question: a 12 mm drop at
the top pushes the foot out by 9 mm.
Convert to chord rotations. Using
\(\psi_{ij} = (\mathbf{d}_{j} - \mathbf{d}_{i})\cdot\mathbf{e}_{2}/L\) with
\(\mathbf{e}_{2}\) the member axis turned 90° counter-clockwise,
$$\psi_{12} = 0, \qquad
\psi_{23} = -\dfrac{\delta}{L_{23}} = -1.500 \times 10^{-3}, \qquad
\psi_{34} = \dfrac{\delta}{r} = +2.500 \times 10^{-3}$$
The left leg is unaffected because neither of its ends moves; the right leg feels
the largest rotation of the three.
Write the two joint equations. With
\(3EI/L_{\text{leg}} = EI/2\) and \(2EI/L_{23} = EI/4\), joint ② and
joint ③ give
$$\theta_{2} + 0.25\theta_{3} = -1.125 \times 10^{-3}, \qquad
0.25\theta_{2} + \theta_{3} = +0.125 \times 10^{-3}$$
Solve.
$$\theta_{2} = -1.2333 \times 10^{-3}\ \text{rad}, \qquad
\theta_{3} = +0.4333 \times 10^{-3}\ \text{rad}$$
The two rotations have opposite signs, which is the frame folding about the
settling corner.
Recover the end moments.
$$M_{21} = \dfrac{3EI}{L}\theta_{2} = \boxed{-222.0\ \text{kN}\cdot\text{m}},
\qquad M_{23} = +222.0\ \text{kN}\cdot\text{m}$$
$$M_{32} = \boxed{+372.0\ \text{kN}\cdot\text{m}}, \qquad
M_{34} = -372.0\ \text{kN}\cdot\text{m}$$
with \(M_{12} = M_{43} = 0\) at the two roller ends. Each joint balances exactly,
which is the only free check available on a load-free problem.
Shears from the end moments. No member carries a span load, so
each shear is constant and equal to \((M_{ij} + M_{ji})/L\):
$$V_{12} = \dfrac{222.0}{6} = 37.00\ \text{kN}, \quad
V_{23} = \dfrac{222.0 + 372.0}{8} = 74.25\ \text{kN}, \quad
V_{34} = \dfrac{372.0}{6} = 62.00\ \text{kN}$$
Reactions, and why they must sum to zero.
$$R_{1} = -46.25\ \text{kN}, \quad R_{2} = +120.50\ \text{kN}, \quad
R_{3} = -151.75\ \text{kN}, \quad R_{4} = +77.50\ \text{kN}$$
There is no applied load, so this set is self-equilibrating: the four values sum to
zero and their moments about any point sum to zero. Two of the four are
hold-downs — a settlement of a redundant support does not push down
on that support, it drags the whole frame with it, and the anchorage has to be
designed for the reversal.
Question 5 bending moment. Every member is straight (no span loads) and the diagram closes to zero at the two roller ends.