16-Civ-A1 Elementary Structural Analysis · May 2016
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Reference texts: R.C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy, method of joints/sections, virtual-work deflections, moment distribution / slope–deflection, influence lines; A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound (Gerber) beams and three-hinged frames. Sign convention: sagging bending moment positive; upward reactions positive; member tension positive (T), compression negative (C).
The paper directs candidates to answer Q1–Q5 and then one of Q6/Q7/Q8. For completeness all eight questions are worked here.
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. Pin $A$ at $x=1\text{ m}$, roller $C$ at $x=7\text{ m}$; $60\text{ kN}$ on the $1\text{ m}$ left overhang (tip $x=0$) and $40\text{ kN}$ on the $1\text{ m}$ right overhang (tip $x=8$). $B$ is the mid-point of span $A\!-\!C$ ($x=4\text{ m}$). $EI=15{,}000\text{ kN}\cdot\text{m}^2$.
Find. Vertical deflection at $B$.
Approach. Unit-load (virtual-work) method: $\displaystyle \delta_B=\int \frac{M\,m}{EI}\,dx$, with $M$ the real moment and $m$ the moment from a unit vertical load at $B$.
Because the structure is statically determinate, both the real moment $M$ and the virtual moment $m$ follow from statics alone, so no compatibility solution is needed. The integral is conveniently evaluated span-by-span between the supports (the virtual moment is zero on the two overhangs, so those regions drop out of the calculation entirely); using the diagram-multiplication (Vereshchagin) shortcut on the two triangular $m$-segments reproduces the same $-225{,}000/EI$. It is worth checking the reactions independently — the right-overhang $40\text{ kN}$ places $M_C=-40\text{ kN}\cdot\text{m}$ and the left-overhang $60\text{ kN}$ places $M_A=-60\text{ kN}\cdot\text{m}$, both recovered above — before trusting the deflection value.
| Quantity | Value |
|---|---|
| $V_A,\;V_C$ | $63.33,\;36.67$ kN |
| $M$ at $A,B,C$ | $-60,\;-50,\;-40$ kN·m (hogging) |
| Deflection at $B$ | $\mathbf{15.0\text{ mm}}$ upward |