Question 3 of 9: Castigliano's theorem of least work on a two-member frame (16 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examination, May 2018, 16-Civ-B1 Advanced Structural Analysis — 3 hours, CLOSED BOOK (an approved Casio or Sharp calculator is permitted). Nine questions: #1 and #2 are compulsory (8 and 12 marks), then TWO of #3, #4, #5 (16 marks each) and TWO of #6, #7, #8, #9 (24 marks each); six questions constitute a complete paper (100 marks). All nine are solved here, because the set is a study resource rather than a timed sitting.
Ghali, A., Neville, A. M. and Brown, T. G., Structural Analysis: A Unified Classical and Matrix Approach, 7th ed., CRC Press — Ch. 4 (force method), Ch. 5 (displacement method), Ch. 24 (effects of temperature and lack of fit).
Canadian design context for the member sizing that follows this analysis: CSA S16:19 Design of Steel Structures, CSA A23.3:19 Design of Concrete Structures and the National Building Code of Canada 2020 (Part 4 loads and load combinations).
Sign convention used throughout. Member end moments $M_{ij}$ are counter-clockwise positive on the member end, which is the convention that matches the standard 6-degree-of-freedom element stiffness matrix and the counter-clockwise-positive joint rotations that Question 9 asks for. With that convention the fixed-end moment of a downward uniform load is $M^{F}_{ij}=+wL^{2}/12$ at the near end, the chord rotation is $\psi_{ij}=\left[(\mathbf{D}_{j}-\mathbf{D}_{i})\cdot\mathbf{e}_{2}\right]/L$ with $\mathbf{e}_{2}$ the member axis turned $+90^{\circ}$, and the ordinary sagging moments plotted on the diagrams are $M_{\text{sag}}(i)=-M_{ij}$ and $M_{\text{sag}}(j)=+M_{ji}$. Where a step of the working is quicker in the clockwise-positive (Hibbeler) form the sign is stated explicitly.
Question 3: Castigliano's theorem of least work on a two-member frame (16 marks)
Given. A two-member rigid frame with a built-in support at joint 1 and a horizontal-plane roller at joint 3.
Given data — Question 3
Quantity
Value
joint 1 (built in)
(0, 0) m
joint 2 (apex, loaded)
(3, 4) m
joint 3 (roller)
(6, 0) m
length of each member
5.00 m
point load at joint 2
32 kN downward
flexural rigidity
EI, the same in both members; axial strain neglected
Find. The bending moment and the shear force carried by member 1–2 at joint 1.
Question 3: built-in at joint 1, roller at joint 3, 32 kN at the apex — one degree statically indeterminate.
Approach. The frame is one degree indeterminate; take the roller reaction as the redundant, write the bending moment in every member as a linear function of it, and set $\partial U/\partial V_{3}=0$.
Establish the degree of indeterminacy. The built-in support supplies three components and the roller one, and the frame has no closed loop, so $$\text{DSI}=r-3=4-3=1.$$ One redundant — take the roller reaction $V_{3}$ (upward positive).
Express the reactions in terms of the redundant. Horizontal equilibrium gives $H_{1}=0$ immediately (the roller cannot push sideways and there is no horizontal load). Then $$V_{1}=32-V_{3},\qquad M_{1}=32(3)-V_{3}(6)=96-6V_{3}\ \text{kN}\cdot\text{m}.$$
Write the bending moment fields. Measure $s$ from joint 3 along member 2–3 and $t$ from joint 1 along member 1–2; both members have direction cosines $(0.6,\,0.8)$, so a point at $s$ sits $0.6s$ horizontally from joint 3. Taking the far free body in each case, $$M_{23}(s)=0.6\,V_{3}\,s,\qquad M_{12}(t)=V_{3}\!\left(6-0.6t\right)-32\!\left(3-0.6t\right).$$ At $t=5$ both give $3V_{3}$, so the two expressions agree at the apex.
Differentiate with respect to the redundant. $$\frac{\partial M_{23}}{\partial V_{3}}=0.6s,\qquad \frac{\partial M_{12}}{\partial V_{3}}=6-0.6t.$$ Because the members are inextensible only the bending strain energy contributes, so least work reads $$\frac{\partial U}{\partial V_{3}}=\frac{1}{EI}\int_{0}^{5}M_{12}\,\frac{\partial M_{12}}{\partial V_{3}}\,dt+\frac{1}{EI}\int_{0}^{5}M_{23}\,\frac{\partial M_{23}}{\partial V_{3}}\,ds=0.$$ $EI$ is the same in both members, so it cancels — the answer needs no numerical stiffness.
Evaluate the integrals. The second integral is $0.36V_{3}\int_{0}^{5}s^{2}ds=15V_{3}$. Writing $M_{12}=a+bt$ with $a=6V_{3}-96$ and $b=19.2-0.6V_{3}$, the first integral is $22.5a+50b=105V_{3}-1200$. Adding, $$120\,V_{3}-1200=0\;\Rightarrow\;\boxed{V_{3}=10.0\ \text{kN (up)}}$$
Recover the remaining reactions. $$V_{1}=32-10=22.0\ \text{kN (up)},\qquad H_{1}=0,\qquad M_{1}=96-6(10)=36.0\ \text{kN}\cdot\text{m}.$$ The built-in support therefore carries a hogging moment of 36.0 kN·m and a vertical force of 22.0 kN.
Resolve the 22 kN into the member axes. Member 1–2 runs along $\mathbf{e}_{1}=(0.6,\,0.8)$, so its shear direction is $\mathbf{e}_{2}=(-0.8,\,0.6)$. With the joint force $(0,\,22)$ acting on the member, $$V=(0,22)\cdot(-0.8,\,0.6)=\boxed{13.2\ \text{kN}},\qquad N=(0,22)\cdot(0.6,\,0.8)=17.6\ \text{kN (compression)}.$$ The resultant closes exactly, $\sqrt{13.2^{2}+17.6^{2}}=22.0$ kN, which is the cheapest available check on the decomposition.
Bending moment at joint 1. The moment on the member at joint 1 is the support moment itself, $$\boxed{M_{1}=36.0\ \text{kN}\cdot\text{m (hogging)}}$$ and the moment falls linearly along member 1–2 to $3V_{3}=30.0$ kN·m at the apex, then linearly to zero at the roller.
Question 3: bending moment diagram, 36.0 kN·m at the built-in support falling to 30.0 kN·m at the apex and zero at the roller.