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07-Str-A4 · May 2018

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, 07-Str-A4 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.

Reference texts.

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)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

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
QuantityValue
joint 1 (built in)(0, 0) m
joint 2 (apex, loaded)(3, 4) m
joint 3 (roller)(6, 0) m
length of each member5.00 m
point load at joint 232 kN downward
flexural rigidityEI, the same in both members; axial strain neglected

Find. The bending moment and the shear force carried by member 1–2 at joint 1.

32 kN1233 m3 m4 m
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 $\partial U/\partial V_{3}=0$.

  1. 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).
  2. 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 $$V_{1}=32-V_{3},\qquad M_{1}=32(3)-V_{3}(6)=96-6V_{3}\ \text{kN}\cdot\text{m}.$$
  3. 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.
  4. 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.
  5. 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, $$120\,V_{3}-1200=0\;\Rightarrow\;\boxed{V_{3}=10.0\ \text{kN (up)}}$$
  6. 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.
  7. 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.
  8. 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.
36.0 kN·m30.0 kN·mjoint 1joint 2 (apex)joint 3distance along members 1-2 then 2-3 (hogging plotted upward)
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.
Question 3 — results
QuantitySymbolValue
Redundant roller reactionV310.0 kN up
Vertical reaction at joint 1V122.0 kN up
Horizontal reaction at joint 1H10
Bending moment on the member at joint 1M136.0 kN·m hogging
Shear on the member at joint 1V13.2 kN
Axial force on the member at joint 1N17.6 kN compression
Bending moment at the apex (joint 2)M230.0 kN·m