16-Civ-B1 Advanced Structural Analysis · December 2014
Question 4 of 9: Least work — moment and shear at joint (2) of a two-hinged portal (18 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examination, December 2014, 98-Civ-B1 Advanced Structural Analysis — 3 hours, closed book (approved Sharp or Casio calculator permitted). Nine questions over six pages: Questions 1 and 2 are compulsory (12 and 8 marks), then any two of Questions 3, 4, 5 (18 marks each) and any two of Questions 6, 7, 8, 9 (22 marks each). Six questions constitute a complete paper and total 100 marks; marks are printed in the left margin. All nine questions are solved here, because the set is a study resource rather than a three-hour sitting.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 6 (influence lines), Ch. 9 (deflections by energy methods), Ch. 10 (force/flexibility method), Ch. 11 (slope-deflection).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3 (determinacy and stability), Ch. 8 (influence lines for floor-beam systems), Ch. 13 (least work), Ch. 15–16 (slope-deflection with and without sidesway).
A. Ghali, A. M. Neville and T. G. Brown, Structural Analysis: A Unified Classical and Matrix Approach, 7th ed. — Ch. 4 (force method), Ch. 5 (lack of fit and support movement).
W. McGuire, R. H. Gallagher and R. D. Ziemian, Matrix Structural Analysis, 2nd ed. — Ch. 4–5 (member stiffness, assembly, kinematic constraints).
CSA S6:19 Canadian Highway Bridge Design Code and NBCC 2020 — the Canadian codes that these analysis methods feed; no code check is required by this paper.
Sign convention used throughout. End moments are counter-clockwise positive, the convention that matches the standard six-degree-of-freedom stiffness element. In it the slope-deflection equation is
the chord rotation is $\psi_{ij}=\bigl[(\mathbf{d}_j-\mathbf{d}_i)\cdot\mathbf{e}_2\bigr]/L$ with $\mathbf{e}_2$ the member axis turned $+90^\circ$, the fixed-end moment of a downward UDL is $\mathrm{FEM}_{i}=+wL^{2}/12$ and $\mathrm{FEM}_{j}=-wL^{2}/12$, and the ordinary sagging bending moment is recovered as $M_{\text{sag}}(i)=-M_{ij}$ and $M_{\text{sag}}(j)=+M_{ji}$. Every translation degree of freedom is closed with the virtual-work statement
in which $\mathbf{F}$ are the equivalent nodal loads and $\mathbf{d}^{*}$, $\psi^{*}$ belong to the unit sway pattern. Mixing this with the clockwise-positive convention of some textbooks produces clean-looking but wrong answers, which is the single most common failure on this subject.
All work below uses the drawing.
Question 4: Least work — moment and shear at joint (2) of a two-hinged portal (18 marks)
Given. A rectangular portal with pinned bases, carrying a uniform load on the beam.
Given data
Quantity
Symbol
Value
Column height, (1)–(2) and (4)–(3)
$h$
3 m
Beam span, (2)–(3)
$L$
6 m
Uniform load on the beam
$w$
12 kN/m downward
Supports at (1) and (4)
—
pinned (two reactions each)
Flexural rigidity
$EI$
the same for every member
Find. The bending moment at joint (2) and the shear force in the column immediately below joint (2).
Question 4: pinned bases give four reactions for three equations, so the frame is one degree indeterminate and the horizontal thrust $H$ is the redundant.
Approach. Take the horizontal thrust as the redundant, write the internal moments in terms of it, and impose $\partial U/\partial H=0$ — the least-work condition that the thrust does no net work at a pinned base.
Establish the degree of indeterminacy. Both bases are drawn as pins (a circle on a hatched triangle), so $r=4$ against three equations of statics: the frame is one degree indeterminate. Reading either base as a roller makes it determinate and least work would be unnecessary — the question's wording confirms the pins.
Statics with the redundant carried symbolically. By symmetry the vertical reactions are
$$V=\frac{wL}{2}=\frac{12(6)}{2}=36\ \text{kN}$$
and $H$ acts inward at each base. Measuring $y$ up a column and $x$ along the beam from joint (2),
$$M_{\text{col}}(y)=Hy,\qquad M_{\text{beam}}(x)=Vx-\frac{wx^{2}}{2}-Hh$$
Apply the least-work condition. With $\partial M_{\text{col}}/\partial H=y$ and $\partial M_{\text{beam}}/\partial H=-h$,
$$\frac{\partial U}{\partial H}=\frac{2}{EI}\int_{0}^{h}(Hy)(y)\,\mathrm{d}y-\frac{h}{EI}\int_{0}^{L}\Bigl(Vx-\frac{wx^{2}}{2}-Hh\Bigr)\mathrm{d}x=0$$
Evaluate the integrals. The first is $2Hh^{3}/3$; in the second, $\int_{0}^{L}(Vx-wx^{2}/2)\,\mathrm{d}x=wL^{3}/12$, so
$$\frac{2Hh^{3}}{3}-h\left(\frac{wL^{3}}{12}-HhL\right)=0 \;\Longrightarrow\; H=\frac{wL^{3}}{8h^{2}+12hL}$$
Substitute the numbers.
$$H=\frac{12(6)^{3}}{8(3)^{2}+12(3)(6)}=\frac{2592}{72+216}=\frac{2592}{288}=\boxed{9.00\ \text{kN}}$$
Bending moment at joint (2). The column is straight, unloaded along its length and pinned at the base, so its moment grows linearly to
$$\boxed{M_2=Hh=9.00(3)=27.0\ \text{kN}\cdot\text{m}\ \text{(hogging at the beam end)}}$$
Shear in the column below joint (2). The only transverse force on that column is the base thrust, so the shear is constant over its full height:
$$\boxed{V_{\text{col}}=H=9.00\ \text{kN}}$$
Check with the beam. At midspan,
$$M_{\text{mid}}=V\frac{L}{2}-\frac{w}{2}\left(\frac{L}{2}\right)^{2}-Hh=108-54-27=+27.0\ \text{kN}\cdot\text{m}$$
so the frame divides the free-beam moment $wL^{2}/8=54\ \text{kN}\cdot\text{m}$ into equal hogging and sagging halves — a well-known result for this ratio of $h$ to $L$, and a strong confirmation that $H$ is right.
The thrust is what makes the portal efficient: it lifts 27 kN·m of the 54 kN·m free-beam moment off the midspan and puts it into the corners, where the column can share it.
Question 4: beam bending moment. Equal hogging and sagging peaks of 27.0 kN·m are a consequence of $h/L=1/2$ with uniform $EI$.