16-Civ-B1 Advanced Structural Analysis · December 2019
Question 8 of 9: Slope-deflection analysis of a sway portal with free stubs
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 8: Slope-deflection analysis of a sway portal with free stubs
(22 marks)
Given. Column height $h = 4\ \text{m}$, beam span
$L = 4\ \text{m}$, free stub $s = 1\ \text{m}$ above each beam joint, a
horizontal load $F = 21\ \text{kN}$ at the top of each stub, both bases built
in, uniform $EI$, all members inextensible.
Find. The joint rotation and sway, all member end moments,
and the shear force and bending moment diagrams.
Question 8: portal frame with built-in bases and 1 m free stubs above each beam joint, each carrying a 21 kN horizontal load.
Approach. Replace each determinate stub by the force and the
couple it delivers to its joint; note that the two loads and the symmetric
geometry make the response antisymmetric, so the two joint rotations are equal
and one sway parameter remains; write one joint equation and one storey-shear
equation and solve the pair.
Replace the stubs. Each stub is a free cantilever standing
above its joint, so it is determinate. Transferring its load to the joint gives
a horizontal force $F = 21\ \text{kN}$ and a couple
$$M_{\text{stub}} = F s = 21(1) = 21.0\ \text{kN}\cdot\text{m}$$
applied to the joint. Forgetting that couple is the classic error on this
question — the storey-shear equation is still satisfied without it, so
nothing looks wrong until the overturning check fails.
Reduce the unknowns. Both columns are the same height and
the beam is inextensible, so joints (2) and (3) translate together by $\Delta$;
the geometry and the two equal loads are mirror images, so
$\theta_2 = \theta_3 = \theta$. Writing $A = EI\theta$ and $B = EI\Delta$, the
whole frame carries two unknowns.
Joint equilibrium at (2). Summing the column and beam end
moments against the applied stub couple,
$$\left(\frac{4}{h} + \frac{6}{L}\right)A + \frac{6}{h^{2}}B = -Fs$$
$$\left(\frac{4}{4} + \frac{6}{4}\right)A + \frac{6}{16}B = -21.0
\quad\Longrightarrow\quad 2.5A + 0.375B = -21.0$$
Storey shear. The two columns together must carry the
$2F$ applied above them, which gives
$$\frac{6}{h}A + \frac{12}{h^{2}}B = Fh
\quad\Longrightarrow\quad 1.5A + 0.75B = 84.0$$
Solve. Doubling the joint equation and subtracting the
shear equation eliminates $B$:
$$5.0A + 0.75B = -42.0 \;\Longrightarrow\; 3.5A = -126.0 \;\Longrightarrow\;
\boxed{EI\theta = -36.0\ \text{kN}\cdot\text{m}^{2}}$$
$$0.75B = 84.0 - 1.5(-36.0) = 138.0 \;\Longrightarrow\;
\boxed{EI\Delta = 184.0\ \text{kN}\cdot\text{m}^{3}}$$
The sway is to the right, as it must be under two rightward loads — a
negative $B$ would have signalled a sign slip.
Back-substitute for the member end moments. With
$M_{\text{base}} = \frac{2EI}{h}\!\left(\theta + \frac{3\Delta}{h}\right)$ and
$M_{\text{top}} = \frac{2EI}{h}\!\left(2\theta + \frac{3\Delta}{h}\right)$,
$$M_{\text{base}} = \tfrac{2}{4}\left(-36.0 + 138.0\right)
= \boxed{51.0\ \text{kN}\cdot\text{m}},\qquad
M_{\text{top}} = \tfrac{2}{4}\left(-72.0 + 138.0\right)
= \boxed{33.0\ \text{kN}\cdot\text{m}}$$
for both columns, and the beam carries
$$M_{23} = -M_{32} = \frac{2EI}{L}\left(3\theta\right) = -54.0
\;\Longrightarrow\; \boxed{M_{\text{beam}} = 54.0\ \text{kN}\cdot\text{m}}$$
hogging at (2) and sagging at (3), zero at mid-span.
The joint check that finds a dropped stub couple. At joint
(2) three members meet — column, beam and stub — so the moments must
balance:
$$M_{\text{top}} + M_{\text{stub}} = 33.0 + 21.0 = 54.0 = M_{\text{beam}}
\quad\checkmark$$
The column moment therefore steps by the full beam moment at the
connection, and both ordinates should be shown on the diagram. Had the stub
couple been omitted, the beam moment would have come out equal to the column-top
moment and this line would not close.
Shears, axial forces and the overturning check. Each column
shear is
$$V_{\text{col}} = \frac{M_{\text{base}} + M_{\text{top}}}{h}
= \frac{51.0 + 33.0}{4} = 21.0\ \text{kN},$$
so the two columns carry the two 21 kN loads exactly. The beam shear is
$$V_{\text{beam}} = \frac{2 M_{\text{beam}}}{L} = \frac{2(54.0)}{4}
= 27.0\ \text{kN},$$
which is also the axial force in each column — tension (uplift) at base
(1), compression at base (4). Global overturning about base (1):
$$2F(h+s) = 2(21.0)(5) = 210.0
\;=\; 2M_{\text{base}} + V_{\text{beam}}L = 2(51.0) + 27.0(4) = 210.0
\quad\checkmark$$
Question 8: bending moment plotted normal to each member. The column moment steps by the full beam moment at each joint.
The two diagrams in words.Shear: constant
21.0 kN in each stub, constant 21.0 kN in each column, constant 27.0 kN in the
beam — every member is unloaded along its length, so no shear varies.
Moment: linear from zero at each stub tip to 21.0 kN·m at the
joint; linear down each column from 33.0 kN·m at the top to
51.0 kN·m at the base, with no sign change (both columns bend in the same
single curvature, because the loading is a pure storey shear applied above the
beam); and linear across the beam from 54.0 hogging at (2) to 54.0 sagging at
(3), passing through zero at mid-span.