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04-BS-6 · May 2015

Question 2 of 8: Cantilever Deflection by the Method of Integration

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

Notes on this paper

National Exams May 2015 – 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 2.

Question 2: Cantilever 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.

w = 15 kN/m 50 kN·m 4 m 2 m A B (free end)
Cantilever, 6 m total span: UDL w = 15 kN/m over the first 4 m, concentrated couple 50 kN·m at the free end.

Given.

QuantityValue
Span6 m total, fixed at A (x=0), free at x=6 m
UDL w15 kN/m over x ∈ [0, 4] m
End couple M050 kN·m at the free end
Section (W310×129, from the printed table)Ix = 308 × 106 mm4, Sx = 1940 × 103 mm3
E200 GPa

Find. (a) Slope and deflection at the free end by direct double integration (no superposition). (b) Whether the deflection satisfies the L/120 limit.

Approach. Write M(x) piecewise from statics (free body to the right of the cut), integrate $EI\,y''=M(x)$ twice in each region, use the two fixed-end conditions $y(0)=y'(0)=0$ plus continuity of slope and deflection at x = 4 m to fix all constants, then evaluate at the free end.

  1. Moment function, by region. For $0\le x\le4$ (m), the free body to the right of the cut carries the remaining UDL plus the end couple: $$M(x) = -\!\left[15(4-x)\!\left(\frac{4-x}{2}\right)+50\right] = -7.5x^2+60x-170\ \ [\text{kN}\cdot\text{m}]$$ For $4\le x\le6$, only the end couple remains: $$M(x)=-50\ \text{kN}\cdot\text{m (constant)}$$ Check at the fixed end: $M(0)=-170\ \text{kN}\cdot\text{m}$, matching the reaction moment by statics ($15(4)(2)+50=120+50=170$ kN·m, hogging) — confirms the sign and magnitude before integrating.
  2. Section stiffness. $$EI = 200{,}000\ \text{MPa}\times308\times10^6\ \text{mm}^4 = 6.16\times10^{13}\ \text{N}\cdot\text{mm}^2 = 61{,}600\ \text{kN}\cdot\text{m}^2$$
  3. Integrate region 1 (0≤x&le4), fixed-end BCs. $$EI\,y' = -2.5x^3+30x^2-170x+C_1, \qquad EI\,y=-0.625x^4+10x^3-85x^2+C_1x+C_2$$ $y'(0)=0$ and $y(0)=0$ (fixed support) give directly $$\boxed{C_1=0,\ C_2=0}$$
  4. Integrate region 2 (4≤x&le6), match at x=4. $$EI\,y'=-50x+D_1, \qquad EI\,y=-25x^2+D_1x+D_2$$ Matching $EI\,y'(4^-)=-2.5(64)+30(16)-170(4)=-360$ to $EI\,y'(4^+)=-200+D_1$ gives $D_1=-160$. Matching $EI\,y(4^-)=-0.625(256)+10(64)-85(16)=-880$ to $EI\,y(4^+)=-400-640+D_2$ gives $D_2=160$: $$EI\,y'(x)=-50x-160, \qquad EI\,y(x)=-25x^2-160x+160 \quad [4\le x\le6]$$
  5. (a) Evaluate at the free end, x = 6 m. $$EI\,y'(6)=-50(6)-160=-460\ \text{kN}\cdot\text{m}^2 \ \Rightarrow\ \theta_{free}=\frac{-460}{61{,}600}=\boxed{-7.47\times10^{-3}\ \text{rad}\ (-0.428^\circ, \text{ tip rotating downward})}$$ $$EI\,y(6)=-25(36)-160(6)+160=-1700\ \text{kN}\cdot\text{m}^3\ \Rightarrow\ \delta_{free}=\frac{-1700}{61{,}600}=-0.02760\ \text{m}=\boxed{27.6\ \text{mm, downward}}$$
  6. (b) Allowable-deflection check. $$\delta_{allow}=\frac{L}{120}=\frac{6000}{120}=50.0\ \text{mm}$$ $$\boxed{27.6\ \text{mm} < 50.0\ \text{mm}\ \Rightarrow\ \text{the beam SATISFIES the allowable deflection limit}}$$

Final Results.

QuantityValue
M(x), 0≤x&le4−7.5x²+60x−170 kN·m
M(x), 4≤x&le6−50 kN·m (constant)
EI61,600 kN·m²
(a) Slope at free end−7.47×10−3 rad (−0.428°)
(a) Deflection at free end27.6 mm, downward
(b) Allowable (L/120)50.0 mm — SATISFIED