Question 3 of 9: Castigliano’s theorem — horizontal deflection at joint 3 (16 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2017 — 07-Str-A4 Advanced Structural Analysis. Three hours, CLOSED BOOK (an approved Sharp or Casio calculator is the only aid). Nine questions: answer BOTH #1 and #2, then ONLY TWO of #3, #4 or #5, and ONLY TWO of #6, #7, #8 or #9 — six questions constitute a complete paper. Marks are printed in the left margin: 8, 12, 16, 16, 16, 24, 24, 24, 24. All nine questions are worked below, because the complete set is the study resource rather than a sitting.
Reference texts. R. C. Hibbeler, Structural Analysis, 10th ed. (Pearson) — Ch. 4 shear and moment diagrams, Ch. 9–10 the force (flexibility) method, Ch. 11 slope-deflection, Ch. 14–16 the stiffness method; A. Kassimali, Structural Analysis, 6th ed. (Cengage) — Ch. 7 deflections by work and energy (Castigliano and least work), Ch. 13 slope-deflection, Ch. 16 sidesway frames; W. McGuire, R. H. Gallagher and R. D. Ziemian, Matrix Structural Analysis, 2nd ed., for the planar frame element stiffness matrix used as the independent check on every answer below. Member sizing that would follow such an analysis is governed in Canada by CSA A23.3:19, CSA S16:19 and CSA O86:19, with load combinations from NBCC 2020.
Check: sign convention, stated once and used throughout. End moments $M_{ij}$ are counter-clockwise positive on the member end — the convention that matches the six-degree-of-freedom planar frame element, so every result below can be reproduced by a direct-stiffness solution. The chord rotation is $\psi_{ij}=\left[(\mathbf{D}_{j}-\mathbf{D}_{i})\cdot\mathbf{n}\right]/L$ with $\mathbf{n}$ the member axis turned $+90^\circ$; the fixed-end moment of a downward UDL is $\mathrm{FEM}_{ij}=+wL^{2}/12$ at the $i$ end; and the ordinary sagging moment is $M_{\text{sag}}(i)=-M_{ij}$, $M_{\text{sag}}(j)=+M_{ji}$. Mixing this with the clockwise-positive convention produces clean-looking integers that are wrong.
Given. A symmetric two-member frame: a pin at joint 1, a roller at joint 3 on the same level, and a rigid apex at joint 2 carrying a 60 kN vertical load.
Question 3 — data
Quantity
Value
Horizontal run of each member
4 m
Rise of the apex above the supports
3 m
Length of each member
5 m
Applied load at joint 2
60 kN downward
Flexural rigidity of both members
$EI=2.0\times10^{4}$ kN·m$^{2}$
Find. The horizontal deflection of joint 3.
Q3: symmetric two-member frame, pin at joint 1 and roller at joint 3, 60 kN applied vertically at the apex. Each member is 5 m long (4 m run, 3 m rise).
Approach. Add a dummy horizontal force $Q$ at the roller, write the bending moment in each member as a function of $Q$, and evaluate $\delta=\partial U/\partial Q$ at $Q=0$.
Find the reactions. With the dummy force $Q$ applied to the right at joint 3, horizontal equilibrium requires the pin to supply $Q$ to the left. Both horizontal forces act at support level, so neither exerts a moment about the other support and the vertical reactions are untouched: $$V_{1}=V_{3}=\frac{60}{2}=30\ \text{kN}$$
Write the bending moment. Measure $s$ along a member from its support, so a point on the left member sits at $(0.8s,\,0.6s)$. The vertical reaction contributes $30\times0.8s$ and the collinear horizontal pair contributes $-Q\times0.6s$, because a horizontal force at support level has a lever arm equal to the height of the section: $$M(s)=-\left(24+0.6Q\right)s,\qquad 0\le s\le 5\ \text{m}$$ Symmetry makes the right member identical, which is the simplification the question invites.
Differentiate with respect to the dummy force. $$\frac{\partial M}{\partial Q}=-0.6\,s$$ on both members, so the integrand is the product of two linear functions of $s$ and the integral is elementary.
Integrate over both members and set $Q=0$. $$\delta_{3H}=\frac{2}{EI}\int_{0}^{5}(24s)(0.6s)\,ds=\frac{2}{EI}\left[14.4\,\frac{s^{3}}{3}\right]_{0}^{5}=\frac{1200}{EI}$$
Substitute the stiffness. With $EI=2.0\times10^{4}$ kN·m$^{2}$, $$\delta_{3H}=\frac{1200}{2.0\times10^{4}}=\boxed{0.060\ \text{m}=60\ \text{mm outward}}$$
The result is positive in the direction of the dummy force, so joint 3 moves away from the frame: the two members flatten under the load and the base spreads by 60 mm. Because the members are declared inextensible, no axial term appears in the strain energy; had they been elastic, the collinear pair would also have stretched the line 1–3 and added a small extra spread. As a check on the bending field, the moment at the apex is $M(5)=-120$ kN·m, that is 120 kN·m with the outside face in tension, and a direct-stiffness solution of the same frame with axially rigid members returns 60.0 mm and 120 kN·m exactly.
Question 3 — results
Quantity
Value
Vertical reaction at each support
30 kN
Horizontal reaction with no dummy load
0
Bending moment at the apex
120 kN·m
$\int M\,(\partial M/\partial Q)\,ds$ over both members