Question 2 of 8: Shear and Moment Functions and Diagrams
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 2: Shear and Moment Functions and Diagrams (20 marks)
Simply supported beam: L = 10 m; 20 kN at x = 4 m; UDL 6 kN/m over x ∈ [4, 10] m.
Given.
Quantity
Value
Span L
10 m, pin at A, roller at B
Concentrated load
20 kN, downward, at x = 4 m
UDL w
6 kN/m over x ∈ [4, 10] m
Find. V(x) and M(x) as explicit functions over the whole span; the shear and
moment diagrams; the maximum positive moment; any inflection point.
Approach. Find the reactions from statics, then cut the beam at a general x in
each of the two load regions and sum forces/moments of everything to the left of the cut.
Reactions. UDL resultant $=6(6)=36$ kN at its centroid $x=4+3=7$ m.
Summing moments about A (CCW+): $$R_B(10) - 20(4) - 36(7) = 0 \ \Rightarrow\ R_B=33.2\
\text{kN}, \qquad R_A = 20+36-33.2=22.8\ \text{kN}$$
Region 1 (0 ≤ x ≤ 4 m).
$$V(x) = R_A = 22.8\ \text{kN (constant)}, \qquad M(x) = R_A x = 22.8x \quad
[\text{kN, kN}\cdot\text{m; }x\text{ in m}]$$
Region 2 (4 ≤ x ≤ 10 m).
$$V(x) = R_A - 20 - 6(x-4) = 2.8 - 6(x-4)$$
$$M(x) = R_A x - 20(x-4) - \frac{6(x-4)^2}{2} = 22.8x - 20(x-4) - 3(x-4)^2$$
Check: $M(10) = 22.8(10)-20(6)-3(36) = 228-120-108=0$ (roller) and
$V(10)=2.8-36=-33.2=-R_B$, both as required.
Maximum moment, from V(x)=0. In region 2, $V=0$ at
$x=4+2.8/6=4.467$ m, giving the maximum sagging moment:
$$M(4.467) = 22.8(4.467)-20(0.467)-3(0.467)^2 = \boxed{+91.9\ \text{kN}\cdot\text{m}}$$
Inflection point. $M(x)=22.8x\ge0$ throughout region 1 (zero only at the
pin itself), and $M(x)$ in region 2 stays positive all the way to the roller (both supports carry
only downward loads, so the beam sags everywhere). $$\boxed{\text{No interior inflection point
exists} - M(x)\ge 0 \text{ over the whole span}}$$
Shear force and bending moment diagrams, with the maximum moment labelled; M(x) never changes sign, so there is no inflection point.
Final Results.
Quantity
Value
RA, RB
22.8 kN, 33.2 kN
V(x), M(x)
region 1: V=22.8, M=22.8x; region 2: V=2.8−6(x−4), M=22.8x−20(x−4)−3(x−4)²