Question 6 of 8: Shear and Moment Functions, Diagrams and Inflection Point
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams December 2013 – 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 W-shape properties table printed on
the exam's last page is not needed — every question supplies its own section dimensions.
Question 6: Shear and Moment Functions, Diagrams and Inflection Point (20 marks)
Simply supported beam: L = 4 m, M0 = 1 kN·m CCW at A, UDL w = 2 kN/m over the last 3 m.
Given.
Quantity
Value
Span L
4 m
Applied couple M₀ (CCW, at A)
1 kN·m
UDL w
2 kN/m over x ∈ [1, 4] m
Find. V(x) and M(x) as explicit functions over the whole span; the shear and
moment diagrams; the maximum positive/negative moments; any inflection point.
Approach. Find the reactions, then cut the beam at a general x in each of the
two load regions (before and after the UDL begins) and sum forces/moments of everything to the
left of the cut.
Reactions. UDL resultant $=2(3)=6$ kN at its centroid $x=1+1.5=2.5$ m.
Summing moments about A (CCW+): $$R_B(4) - 6(2.5) + 1 = 0 \Rightarrow R_B=3.5\ \text{kN},
\qquad R_A = 6-3.5=2.5\ \text{kN}$$
Region 1 (0 ≤ x ≤ 1 m, before the UDL).
$$V(x)=R_A=2.5\ \text{kN (constant)}, \qquad M(x)=R_A x - M_0 = 2.5x-1\quad[\text{kN,
kN}\cdot\text{m; }x\text{ in m}]$$
Region 2 (1 ≤ x ≤ 4 m, UDL active).
$$V(x)=R_A-w(x-1)=2.5-2(x-1)$$
$$M(x)=R_A x - M_0 - \frac{w(x-1)^2}{2} = 2.5x-1-(x-1)^2$$
Check: $M(4)=2.5(4)-1-9=0$ (roller) and $V(4)=2.5-6=-3.5=-R_B$, both as required.
Maximum moments, from V(x)=0. In region 2, $V=0$ at
$x=1+1.25=2.25$ m, giving the maximum positive (sagging) moment:
$$M(2.25)=2.5(2.25)-1-(1.25)^2=\boxed{+3.06\ \text{kN}\cdot\text{m}}$$
The maximum negative (hogging) moment occurs right at the left support, where the
applied couple produces a jump from the (zero) moment just outside the span to
$$M(0)=\boxed{-1.00\ \text{kN}\cdot\text{m}}$$
Inflection point. M(x) is continuous throughout the interior of the span
(the applied couple sits at the boundary, x=0, not mid-span, so there is no internal jump).
Setting the region-1 expression to zero: $2.5x-1=0 \Rightarrow \boxed{x=0.40\ \text{m}}$,
where the curvature genuinely reverses from hogging to sagging.
Shear force and bending moment diagrams, with the maximum/minimum moments and the inflection point labelled.
Final Results.
Quantity
Value
RA, RB
2.5 kN, 3.5 kN
V(x), M(x)
region 1: V=2.5, M=2.5x−1; region 2: V=2.5−2(x−1), M=2.5x−1−(x−1)²