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04-BS-6 · May 2014

Question 8 of 8: Overhang Beam Deflection by the Method of Integration

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

Notes on this paper

National Exams May 2014 – 04-BS-6: Mechanics of Materials
3 hours duration, closed book (one hand-written aid sheet permitted). Any five of the eight questions constitute a complete paper; all eight are solved below as a complete study resource.

Reference texts: R.C. Hibbeler, Mechanics of Materials, 10th ed. (Ch. 5 torsion, Ch. 6 shear/moment diagrams & composite beams, Ch. 7 transverse shear, Ch. 8 combined loadings, Ch. 9 stress transformation, Ch. 12 deflection by integration, Ch. 13 buckling); F. Beer & E.R. Johnston, Mechanics of Materials; W. Gere & B. Goodno, Mechanics of Materials (alternates). A wide-flange (W-shape) properties table printed on the exam's last page supplies the section used in Question 8.

Question 8: Overhang Beam Deflection by the Method of Integration (20 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.

20 kNABC4 m2 mFig. Q8 – overhang beam (W150x30), tip load at C
Simply supported beam with overhang: A–B = 4 m, B–C = 2 m overhang, 20 kN at C; W150x30 section (I = 17.1 × 106 mm4 from the printed W-shape table).

Given.

QuantityValue
Span A–B4 m (pin at A, roller at B)
Overhang B–C2 m
Tip load at C20 kN, downward
SectionW150x30: Ix = 17.1 × 106 mm4 (printed W-shape table)
E200 GPa

Find. The deflection and slope at the overhang tip C, by direct double integration of the moment-curvature relation (no superposition).

Approach. Find the reactions, write a single Macaulay-bracket moment expression valid over the whole beam, integrate $EI y''=M(x)$ twice, fix the two constants from the zero-deflection conditions at the two supports, then evaluate the resulting slope and deflection expressions at x = 6 m (point C).

  1. Reactions. Summing moments about A (CCW+, load at 6 m): $$R_B(4) - 20(6) = 0 \ \Rightarrow\ R_B = 30\ \text{kN}, \qquad R_A = 20-30 = -10\ \text{kN}\ \text{(i.e. 10 kN downward — the overhang load pulls the near support down)}$$
  2. Moment function (Macaulay form, x from A, in mm). $$M(x) = R_A x + R_B\langle x-4000\rangle = -10{,}000\,x + 30{,}000\langle x-4000\rangle \quad [\text{N}\cdot\text{mm}]$$ Check at the tip: $M(6000)=-10{,}000(6000)+30{,}000(2000) = -60\times10^6+60\times10^6=0$ (free end, as required), and at B: $M(4000^-)=-40\times10^6\ \text{N}\cdot\text{mm} = -40$ kN·m, matching $-P\times(\text{overhang length})=-20(2)$ from the free-end side — consistent hogging over the whole overhang.
  3. Section property. $$I = 17.1\times10^6\ \text{mm}^4, \qquad EI = 200{,}000(17.1\times10^6) = 3.42\times10^{12}\ \text{N}\cdot\text{mm}^2$$
  4. First integration (slope). $$EI\,y' = -5000x^2+15{,}000\langle x-4000\rangle^2 + C_1$$
  5. Second integration (deflection) and boundary conditions. $$EI\,y = -\tfrac{5000}{3}x^3+5000\langle x-4000\rangle^3+C_1x+C_2$$ $y(0)=0\Rightarrow C_2=0$. $y(4000)=0$ gives $$-\tfrac{5000}{3}(4000)^3 + C_1(4000) = 0 \ \Rightarrow\ \boxed{C_1 = 2.667\times10^{10}\ \text{N}\cdot\text{mm}^2}$$
  6. Evaluate slope and deflection at C (x = 6000 mm). $$EI\,y'(6000) = -5000(6000)^2+15{,}000(2000)^2+2.667\times10^{10} = -9.333\times10^{10}\ \text{N}\cdot\text{mm}^2$$ $$\theta_C = \frac{-9.333\times10^{10}}{3.42\times10^{12}} = -0.02729\ \text{rad} = \boxed{-1.564^\circ}\ \text{(rotating clockwise, tip dipping down)}$$ $$EI\,y(6000) = -\tfrac{5000}{3}(6000)^3+5000(2000)^3+2.667\times10^{10}(6000) = -1.600\times10^{14}\ \text{N}\cdot\text{mm}^3$$ $$\boxed{\delta_C = \frac{-1.600\times10^{14}}{3.42\times10^{12}} = -46.8\ \text{mm}\ (46.8\ \text{mm downward})}$$

Final Results.

QuantityValue
RA, RB−10 kN (down), 30 kN (up)
EI3.42 × 1012 N·mm2
Slope at C−1.564° (clockwise)
Deflection at C46.8 mm, downward
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