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04-BS-6 · Undated paper

Question 3 of 8: Shear/Moment Diagrams for an Overhanging Beam with a Tip Moment

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

Notes on this paper

National Exam, May 2019 — 04-BS-06: Mechanics of Materials. Closed book, one 8.5"×11" handwritten aid sheet permitted, 3 hours, 8 questions of equal value (any 5 of 8 constitute a complete paper — all 8 are answered here as a complete study resource).

Reference texts: R.C. Hibbeler, Mechanics of Materials, 10th ed. (Pearson) — axial deformation of statically indeterminate assemblies, beam deflection by integration, shear/moment diagrams, plane-stress transformation and Mohr's circle, column buckling, torsion of circular shafts, composite (transformed-section) beams, combined axial-flexural loading, transverse shear.

Question 3: Shear/Moment Diagrams for an Overhanging Beam with a Tip Moment

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.

QuantityValue
Span A–B (pin at A, roller at B)6 m
Overhang B–C (free end at C)4 m
UDL $w$ (over A–B)5 kN/m
Applied moment at C60 kN·m, clockwise

Find. $V(x)$ and $M(x)$ over the full 10 m length; the SFD and BMD with $M_{max}^{+}$, $M_{max}^{-}$, and any inflection point identified.

ABC5 kN/m60 kN·m6 m4 m
Beam A-B-C: pin A, roller B (6 m), overhang to free end C (4 m); 5 kN/m over A-B; 60 kN.m CW at C.

Approach. Find reactions from global equilibrium (the applied end moment enters directly, independent of position), then integrate the load to get $V(x)$ and $M(x)$ in the two regions (loaded span, unloaded overhang).

  1. Reactions. Taking moments about A (CCW+, clockwise applied moment enters as $-60$): $$\sum M_A=0:\ 6B_y-(5)(6)(3)-60=0 \Rightarrow B_y=25\text{ kN}$$ $$\sum F_y=0:\ A_y=5(6)-25=5\text{ kN}$$
  2. Region 1, $0\le x\le6$ m (measured from A). $$V(x)=A_y-wx=5-5x\ \text{kN}$$ $$M(x)=A_y x-\tfrac{w}{2}x^2=5x-2.5x^2\ \text{kN}\!\cdot\!\text{m}$$ $V=0$ at $x=1$ m, giving the local maximum positive moment $M(1)=2.5$ kN·m. At $x=6^-$: $V=-25$ kN, $M(6)=-60$ kN·m; the roller reaction $B_y=+25$ kN then brings $V$ back to $0$ just past B.
  3. Region 2, $6\le x\le10$ m (the overhang carries no load). $$V(x)=0,\qquad M(x)=-60\ \text{kN}\!\cdot\!\text{m (constant)}$$ This constant value is confirmed independently from the free body to the RIGHT of any cut in this region (just the 60 kN·m clockwise tip moment, giving internal $M=-60$ kN·m by equilibrium of that small free body) — consistent with the value carried through from Region 1 at $x=6$, so $M(x)$ has no jump at B (only $V$ jumps, from the roller force).
  4. Inflection point. $M(x)=5x-2.5x^2=0\Rightarrow x=0$ or $x=2$ m — curvature reverses at $x=2$ m. $$\boxed{M_{max}^{+}=2.5\text{ kN}\cdot\text{m at }x=1\text{ m};\quad M_{max}^{-}=-60\text{ kN}\cdot\text{m from }x=6\text{ to }10\text{ m};\quad \text{inflection at }x=2\text{ m}}$$
ResultValue
$A_y$, $B_y$5 kN, 25 kN
$V(x)$$5-5x$ (0–6 m); $0$ (6–10 m)
$M(x)$$5x-2.5x^2$ (0–6 m); $-60$ (6–10 m)
$M_{max}^{+}$ / $M_{max}^{-}$$+2.5$ kN·m at $x=1$ m / $-60$ kN·m over the overhang
Inflection point$x=2$ m