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16-Civ-A1 Elementary Structural Analysis · December 2014

Question 3 of 8: Deflection of a non-prismatic beam by virtual work

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

Notes on this paper

Reference texts: R.C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy, method of joints/sections, virtual-work deflections, moment distribution, influence lines; A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges and compound (Gerber) structures, three-hinged frames. Sign convention: sagging bending moment positive; upward reactions positive; tension member forces positive (T), compression negative (C); distances in metres, forces in kN.

Exam rule: six questions constitute a complete paper — answer all of #1–#5 and only one of #6/#7/#8. All eight are solved here as a complete study resource.

Source note: Member geometry, support types and load directions for Questions 4, 7 and 8 were read from the printed figures; every reconstructed dimension yields clean, self-consistent equilibrium. Where a figure value was inferred, it is stated explicitly — verify against the original booklet if using for assessment.

Question 3: Deflection of a non-prismatic beam by virtual work (18 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.

84 kN36 kNEI2EI2EI3 m3 m3 mABCD
Simply-supported beam A(pin)–C(roller) with cantilever to D; 84 kN at B, 36 kN at D; segment stiffnesses $EI$ (A–B) and $2EI$ (B–C–D).

Given. $A$ pin at $x=0$, $C$ roller at $x=6$; $84$ kN at $B$ ($x=3$), $36$ kN at $D$ ($x=9$, cantilever tip); $EI_{AB}=EI$, $EI_{BC}=EI_{CD}=2EI$, $EI=7.5\times10^4$ kN·m². Find. the vertical deflection $\delta_B$.

Approach. Determinate beam → unit-load (virtual-work) method $\displaystyle \delta_B=\int \frac{M\,m}{EI}\,dx$, with the real moment $M$ from the 84/36 kN loads and the virtual moment $m$ from a unit load at $B$.

  1. Real reactions and moments. $\sum M_A: 6R_C = 84(3)+36(9) \Rightarrow R_C = 96$ kN, $R_A = 24$ kN. Then $M=24x$ (A–B), $M=24x-84(x-3)$ (B–C), and $M=-36(9-x)$ on the cantilever (0 at B-line references). Key values: $M_B=72$, $M_C=-108$ kN·m.
  2. Virtual system. Unit downward load at $B$: $R_A=R_C=0.5$, giving $m=0.5x$ (A–B), $m=3-0.5x$ (B–C), $m=0$ on the cantilever.
  3. Integrate with the correct $EI$ per segment. $$\delta_B=\underbrace{\frac{1}{EI}\!\int_0^3 (24x)(0.5x)\,dx}_{=108/EI}+\underbrace{\frac{1}{2EI}\!\int_3^6 M\,m\,dx}_{=13.5/EI}+0 = \frac{121.5}{EI}.$$
  4. Evaluate. $\displaystyle \delta_B=\frac{121.5}{7.5\times10^4}=1.62\times10^{-3}\text{ m} = \boxed{1.62\text{ mm}\ (\downarrow)}$.

The deflection is small — about $1/1850$ of the 3 m A–B span — because the stiffer $2EI$ segment covers the region where the virtual moment is largest, and because the cantilever load contributes only indirectly. As a sanity check, ignoring the stiffness step (treating the whole beam as $EI$) would over-predict the deflection by the $13.5/EI$ that the $2EI$ segment saves, i.e. by roughly 11 %, confirming that the non-prismatic modelling matters here.

QuantityValue
$R_A,\;R_C$24 kN, 96 kN
$\int Mm/EI$$121.5/EI$
$\delta_B$1.62 mm downward