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16-Civ-A1 Elementary Structural Analysis · May 2017

Question 8 of 8: Vertical deflection at C (beam propped by a strut)

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper: National Exams — May 2017, 16-Civ-A1 Elementary Structural Analysis (closed book, 3 h). Six questions constitute a complete paper: answer Q1–Q5 and one of Q6/Q7/Q8. For completeness all eight questions are worked here.

Reference texts: R.C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy (Ch. 2), joints/sections (Ch. 3), shear & moment diagrams (Ch. 4), influence lines (Ch. 6), virtual-work deflections (Ch. 8–9), moment distribution / slope–deflection (Ch. 11–12); A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound beams, indeterminate frames.

Sign convention: upward reactions positive; sagging bending moment positive (tension on the underside); member tension positive (T), compression negative (C).

These A1 papers are defined entirely by their figures, so every structure has been read from the printed figure and redrawn to scale below.

Question 8: Vertical deflection at C (beam propped by a strut) (22 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. Horizontal beam $A(0,0)$–$B(4,0)$ ($2EI$) –$C(6,0)$ ($EI$); pin at $A$; pin at $D(0,3)$; a strut $D$–$B$ (axial, $AE{=}25000$); a UDL over $B$–$C$. Find. $\delta_C$.

2EIEISTRUTwABCD3 m4 m2 m
Q8: beam A–B–C propped at B by the inclined strut D–B.
Check: the paper shows the UDL on span $B$–$C$ (its arrows) but no legible magnitude. The deflection is therefore given as a coefficient times the intensity $w$; substitute the intended $w$ (kN/m) to obtain the number.

Approach. The strut is a two-force member (axial only). Solve the real system (beam + strut) for member moments $M$ and strut force $N$; apply a unit vertical load at $C$ for the virtual $m,n$; then $\delta_C=\int\frac{Mm}{EI}\,dx+\frac{N\,n\,L_{strut}}{AE}$.

  1. Real system. Under the UDL $w$ on $B$–$C$, equilibrium of the propped beam gives the strut force $N=-4.17\,w$ (compression) and the corresponding bending moments along $A$–$B$–$C$.
  2. Virtual system. A unit downward load at $C$ produces its own bending moments $m$ and strut force $n$.
  3. Combine (beam bending + strut axial). Evaluating $\displaystyle \delta_C=\int\frac{Mm}{EI}dx+\frac{NnL}{AE}$ with $EI=3500$ and $AE=25000$ gives the flexibility $\dfrac{\delta_C}{w}=3.42\times10^{-3}\ \text{m per (kN/m)}$, i.e. $\boxed{\delta_C\approx 3.42\,w\ \text{mm (downward)}}$, $w$ in $\text{kN/m}$.

For example, a UDL of $w=10\text{ kN/m}$ would give $\delta_C\approx34.2\text{ mm}$ downward; $w=20\text{ kN/m}$ gives $\approx68.3\text{ mm}$.

QuantityValue
Strut force $N$4.17 $w$ kN (compression)
$\delta_C$ (per unit $w$)3.42 $w$ mm (down)
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