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24-Bld-A1 Elementary Structural Analysis · December 2016

Question 3 of 8: Vertical deflection at the overhang tip of a symmetric two-span beam (18 marks)

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

Notes on this paper

National Exams, December 2016 — 07-Bldg-A1 Elementary Structural Analysis. 3 hours. Six questions constitute a complete paper: answer ALL of Questions #1–#5; answer ONLY ONE of #6, #7 or #8 (all three are solved below for completeness).

Reference texts: Hibbeler, Structural Analysis, 10th ed.; Kassimali, Structural Analysis, 6th ed.

Question 3: Vertical deflection at the overhang tip of a symmetric two-span beam (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.

Given. Beam A–B–C–D–E with simple supports at B ($x=2\text{ m}$) and D ($x=10\text{ m}$); overhangs A–B and D–E ($2\text{ m}$ each) carry a 12 kN/m UDL; the central span B–D ($8\text{ m}$) carries a 6 kN/m UDL. C ($x=6\text{ m}$) is the centreline. $EI=2000\text{ kN}\cdot\text{m}^2$ throughout.

Find. The vertical deflection at A.

A B C D E 12 kN/m 6 kN/m 12 kN/m 2 m 4 m 4 m 2 m
Fig. Q3 — symmetric beam with two loaded overhangs; the loading and the beam are both symmetric about C.

Approach. By symmetry the two support reactions are equal; the tip deflection is then obtained by the unit-load (virtual-work) method, $\Delta_A=\int \dfrac{mM}{EI}\,dx$, integrating the product of the real moment $M(x)$ and the moment $m(x)$ from a unit downward load at A over all four segments.

  1. Reactions by symmetry. Total load $=12(2)+6(8)+12(2)=24+48+24=96\text{ kN}$; by symmetry $R_B=R_D=\boxed{48\text{ kN}}$ each (confirmed by $\sum M_B=0$).
  2. Real moment diagram (key values). $M_B=-\tfrac12(12)(2)^2=-24\text{ kN}\cdot\text{m}$ (hogging over the overhang support); $M_C=+24\text{ kN}\cdot\text{m}$ (sagging at midspan, by symmetry $M_D=-24\text{ kN}\cdot\text{m}$ too). The diagram is piecewise quadratic in each segment.
  3. Virtual moment diagram. A unit load at A (with the same B, D supports) again gives reactions from statics alone; $m(x)$ is piecewise linear, zero at B and D and growing linearly away from them (largest, negative-going, over the loaded overhangs).
  4. Integrate $\int mM\,dx$ segment by segment (Simpson's rule is exact here since $mM$ is at worst cubic on each straight segment): A–B contributes $24.0$, B–C contributes $-32.0$, C–D contributes $-32.0$, D–E contributes $0$ (units kN2·m3). Sum $=24-32-32+0=-40$.
  5. Deflection. $\Delta_A=\dfrac{-40}{2000}=-0.020\text{ m}$; the negative sign (relative to the downward unit load) means the tip moves upward. $\boxed{\Delta_A = 20\text{ mm, upward}}$ — confirmed independently by a direct stiffness-method solve of the same beam, which returns the identical 20.0 mm.
Q3 – reactions and deflection
QuantityValue
$R_B=R_D$48 kN ↑ each
$M$ at B (and D)−24 kN·m
$M$ at C (midspan)+24 kN·m
$\Delta_A$20.0 mm, upward
Check: the upward sense is not a typo — the two heavily-loaded overhangs (24 kN each, arm 2 m) rotate the beam at B and D enough that this rigid-body rotation of the overhang lifts tip A more than the overhang's own local sagging pulls it down. Confirmed by two independent methods (unit-load integration and a full stiffness-method displacement solve) agreeing to 4 significant figures.