Question 2 of 8: Reactions, Shear Force and Bending Moment Diagrams
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2016 —
07-Str-A1 Elementary Structural Analysis, 3 hours, CLOSED BOOK
(an approved Sharp or Casio calculator is permitted). Six questions constitute
a complete paper: Questions 1–5 are compulsory and one only of
Questions 6, 7 or 8 is attempted, for 100 marks
(6 + 18 + 15 + 18 + 21 + 22). Marks are shown in the left margin.
All eight questions are worked below, because the three
alternatives exercise three different methods — slope deflection,
virtual work and three-hinged-frame statics — and the complete set is
the more useful study resource.
Every structure on this paper is defined by a hand-drawn figure and nothing
else: the printed text gives the task, the drawing gives the geometry, the
loads and the support types.
Sign conventions used throughout. Shear force is positive
when the resultant of the forces to the left of a section acts upwards;
bending moment is positive when it sags the member (tension on the underside),
and sagging ordinates are plotted above the axis in every diagram.
Truss member forces are quoted as T for tension and C for
compression. In the slope-deflection work of Question 6 the member-end moments
follow the usual convention, clockwise on the member end taken as positive.
Find. The three reaction components, then the complete
shear and bending moment diagrams with the maximum positive and negative
ordinates labelled.
Approach. Four unknown reaction components against three
equations of equilibrium plus one condition of zero moment at the hinge: cut
the beam at the hinge, solve the short left segment first, then pass the hinge
force onto the right segment.
Take moments about the hinge for the left segment.
The segment from $x = 0$ to $x = 6$ carries only the reaction $A_y$ and the
30 kN load, and the hinge cannot transmit moment, so
$$\sum M_{\text{hinge}} = A_y (6) - 30 (6-4) = 0
\;\Longrightarrow\; \boxed{A_y = 10.0\ \text{kN}\ \uparrow}$$
The pin also supplies a horizontal component, which is zero because no
horizontal load is applied.
Extract the force carried through the hinge. Vertical
equilibrium of the same segment gives the force the left half hands to the
right half:
$$V_{\text{hinge}} = 30 - A_y = 30 - 10 = 20.0\ \text{kN}$$
acting downward on the right segment at $x = 6\ \text{m}$.
Solve the right segment. It runs from $x = 6$ to
$x = 16$, carries the 20.0 kN hinge force at its left end and a resultant
$W = wL = 4(8) = 32\ \text{kN}$ acting at $x = 12\ \text{m}$, and is
supported by the rollers at C and D. Taking moments about C,
$$D(16-8) - 32(12-8) + 20(8-6) = 0
\;\Longrightarrow\; \boxed{D = 11.0\ \text{kN}\ \uparrow}$$
and vertical equilibrium of the same segment then gives
$$\boxed{C = 20 + 32 - 11 = 41.0\ \text{kN}\ \uparrow}$$
As a check, $A_y + C + D = 10 + 41 + 11 = 62\ \text{kN}$, which is exactly
the applied total $30 + 32$.
Build the shear diagram. Working from the left,
$V = +10.0$ kN up to the point load, $V = 10 - 30 = -20.0$ kN from the load
through the hinge to C, then C lifts it to
$V = -20 + 41 = +21.0$ kN, after which the uniform load drives it down at
$4\ \text{kN}/\text{m}$ to $V = 21 - 32 = -11.0$ kN at D. The maximum
positive and negative ordinates are therefore
$$\boxed{V_{\max}^{+} = +21.0\ \text{kN}\ \text{just right of C},\quad
V_{\max}^{-} = -20.0\ \text{kN}\ \text{between the load and C}}$$
Integrate for the bending moments. The moment rises
linearly to $M(4) = 10(4) = +40.0\ \text{kN}\cdot\text{m}$ under the point
load, falls to zero at the hinge as it must, and continues down to
$M(8) = -20(2) = -40.0\ \text{kN}\cdot\text{m}$ over C. Beyond C the shear
is $V(x) = 21 - 4(x-8)$, which vanishes at
$$x = 8 + \frac{21}{4} = 13.25\ \text{m}$$
and the sagging peak inside the right span is
$$M(13.25) = -40 + 21(5.25) - 2(5.25)^2 = +15.125\ \text{kN}\cdot\text{m}$$
so that
$$\boxed{M_{\max}^{+} = +40.0\ \text{kN}\cdot\text{m}\ \text{at }x=4\ \text{m},
\quad M_{\max}^{-} = -40.0\ \text{kN}\cdot\text{m}\ \text{at C}}$$
The moment returns to zero at D, confirming the arithmetic.
Q2(a). Blue fill marks positive (upward shear, sagging moment) and red fill negative (downward shear, hogging moment). The bending moment is zero at the internal hinge by definition, and the two extreme moment ordinates happen to be equal and opposite here.
Result
Value
Reaction at A (pin)
$10.0\ \text{kN}\ \uparrow$ (no horizontal component)
Reaction at C (roller)
$41.0\ \text{kN}\ \uparrow$
Reaction at D (roller)
$11.0\ \text{kN}\ \uparrow$
Maximum positive shear
$+21.0\ \text{kN}$ just right of C
Maximum negative shear
$-20.0\ \text{kN}$ from $x=4$ to $x=8\ \text{m}$
Maximum positive moment
$+40.0\ \text{kN}\cdot\text{m}$ at $x = 4\ \text{m}$
Maximum negative moment
$-40.0\ \text{kN}\cdot\text{m}$ at C
Local sagging peak, right span
$+15.125\ \text{kN}\cdot\text{m}$ at $x = 13.25\ \text{m}$
(b) Overhanging beam with a partial uniform load
Given. A 12 m beam with the origin at the free left
end: pin B at $x = 2\ \text{m}$, roller D at $x = 12\ \text{m}$, a 44 kN
downward point load at $x = 7\ \text{m}$, and $w = 12\ \text{kN}/\text{m}$
running from the free end to the point load, i.e. over
$0 \le x \le 7\ \text{m}$. The load block on the drawing begins at the very tip
of the overhang and stops exactly under the 44 kN arrow, so the loaded length
is 7 m and not the 5 m span between the supports.
Find. Both reactions, and the shear and bending moment
diagrams with their extreme ordinates.
Approach. The beam is simply supported with one overhang,
so ordinary statics is enough; replace the distributed load by its resultant
for the reaction calculation, then return to the distributed form to integrate
the shear.
Replace the uniform load by its resultant.
$$W = wL_w = 12(7) = 84.0\ \text{kN}\quad\text{acting at }
\bar{x} = \tfrac{7}{2} = 3.5\ \text{m}$$
Take moments about the pin to find the far reaction.
$$\sum M_B = D(12-2) - 84(3.5-2) - 44(7-2) = 0$$
$$10 D = 126 + 220 = 346 \;\Longrightarrow\;
\boxed{D = 34.6\ \text{kN}\ \uparrow}$$
Close vertical equilibrium for the pin reaction.
$$\boxed{B = 84 + 44 - 34.6 = 93.4\ \text{kN}\ \uparrow}$$
with no horizontal component.
Trace the shear. On the overhang the shear falls
linearly to $V(2^-) = -12(2) = -24.0$ kN; the pin lifts it to
$V(2^+) = -24 + 93.4 = +69.4$ kN, and the uniform load then reduces it to
$V(7^-) = 69.4 - 12(5) = +9.4$ kN. Since the shear has not reached zero
before the point load, there is no interior sagging peak in that stretch.
The 44 kN load drops it to $V(7^+) = 9.4 - 44 = -34.6$ kN, which then holds
constant to the roller. Hence
$$\boxed{V_{\max}^{+} = +69.4\ \text{kN},\qquad
V_{\max}^{-} = -34.6\ \text{kN}}$$
Integrate for the moments. Over the overhang
$M(x) = -6x^2$, giving the hogging peak
$M(2) = -24.0\ \text{kN}\cdot\text{m}$ at the pin. Between the supports the
shear stays positive, so the moment climbs monotonically to its maximum
under the point load:
$$M(7) = -6(7)^2 + 93.4(7-2) = -294 + 467 = +173.0\ \text{kN}\cdot\text{m}$$
Beyond the load the shear is constant at $-34.6$ kN, so the moment runs
straight back to $173 - 34.6(5) = 0$ at the roller, as it must. Therefore
$$\boxed{M_{\max}^{+} = +173.0\ \text{kN}\cdot\text{m}\ \text{at }
x = 7\ \text{m},\quad M_{\max}^{-} = -24.0\ \text{kN}\cdot\text{m}\
\text{at the pin}}$$
Q2(b). The hogging region is confined to the overhang and a short length past the pin; the moment changes sign where the diagram crosses the axis, at $x = 2.357$ m.
Result
Value
Reaction at B (pin)
$93.4\ \text{kN}\ \uparrow$
Reaction at D (roller)
$34.6\ \text{kN}\ \uparrow$
Maximum positive shear
$+69.4\ \text{kN}$ just right of B
Maximum negative shear
$-34.6\ \text{kN}$ from $x = 7$ to $12\ \text{m}$
Maximum positive moment
$+173.0\ \text{kN}\cdot\text{m}$ at $x = 7\ \text{m}$
Maximum negative moment
$-24.0\ \text{kN}\cdot\text{m}$ at B
(c) Inclined member on a pin and an inclined roller
Given. A straight member running from a pin at
$(0,\,12)$ down to a roller at $(16,\,0)$ — a 3:4 slope, marked as such on
the drawing, so the member length is
$L = \sqrt{16^2 + 12^2} = 20.0\ \text{m}$. Vertical point loads of 5 kN and
7 kN act at horizontal offsets of 6 m and 10 m from the pin, i.e. at 7.5 m and
12.5 m measured along the member. The roller hatching at the lower end
is drawn parallel to the member, so its reaction is taken normal to the member
axis.
Find. The reactions, and the shear and bending moment
diagrams for the inclined member with the extreme ordinates.
Approach. Resolve along and normal to the member axis. The
useful geometric fact is that a reaction normal to the member has the whole
member length as its lever arm about the pin, which delivers the reaction in
one line.
Take moments about the pin. With the reaction
$R_n$ normal to the member, its lever arm about the pin is the member
length itself, 20 m, while the applied loads act at horizontal offsets of
6 m and 10 m:
$$R_n (20) = 5(6) + 7(10) = 100 \;\Longrightarrow\;
\boxed{R_n = 5.0\ \text{kN}}$$
Resolve the roller reaction into components. The unit
normal to a 3:4 member is $(0.6,\ 0.8)$, so
$$\mathbf{R}_{\text{roller}} = 5.0\,(0.6,\ 0.8)
= (3.0,\ 4.0)\ \text{kN}$$
i.e. 3.0 kN horizontal and 4.0 kN vertical.
Close global equilibrium at the pin.
$$\begin{aligned}
A_x &= -3.0\ \text{kN} \quad (3.0\ \text{kN acting to the left})\\
A_y &= 5 + 7 - 4.0 = 8.0\ \text{kN} \quad (\text{upward})
\end{aligned}$$
so $\boxed{\mathbf{A} = (-3.0,\ +8.0)\ \text{kN},\ |\mathbf{A}| =
8.544\ \text{kN}}$
Resolve the forces normal to the member for the shear.
Taking $s$ along the member from the pin and dotting each force with the
unit normal $(0.6,\ 0.8)$,
$$\begin{aligned}
V &= (-3.0)(0.6) + (8.0)(0.8) = +4.6\ \text{kN} && 0 < s < 7.5\ \text{m}\\
V &= 4.6 - 5(0.8) = +0.6\ \text{kN} && 7.5 < s < 12.5\ \text{m}\\
V &= 0.6 - 7(0.8) = -5.0\ \text{kN} && 12.5 < s < 20\ \text{m}
\end{aligned}$$
so $\boxed{V_{\max}^{+} = +4.6\ \text{kN},\quad V_{\max}^{-} = -5.0\
\text{kN}}$
Integrate the shear along the member for the moment.
The moment grows at $4.6\ \text{kN}$ per metre of member to
$M = 34.5\ \text{kN}\cdot\text{m}$ under the 5 kN load, then at
$0.6\ \text{kN}$ per metre to its peak under the 7 kN load,
$$M_{\max} = 34.5 + 0.6(5.0) = +37.5\ \text{kN}\cdot\text{m}
\quad\text{at } s = 12.5\ \text{m}$$
and finally falls at $5.0\ \text{kN}$ per metre back to zero at the roller,
$37.5 - 5.0(7.5) = 0$. The member sags everywhere, so
$$\boxed{M_{\max}^{+} = +37.5\ \text{kN}\cdot\text{m},\qquad
M_{\max}^{-} = 0}$$
Record the axial force, which is what makes this member
unusual. Dotting the same forces with the unit vector along the
member, $(0.8,\ -0.6)$, the member carries $7.2\ \text{kN}$ tension above
the 5 kN load, $4.2\ \text{kN}$ tension between the loads and zero below the
7 kN load — it hangs from the pin, and the normal roller adds no axial
force at all.
Q2(c). The shear and moment diagrams are developed: they are plotted against distance along the member axis rather than hung off the inclined member itself, which keeps the ordinates legible.
Check: the roller plane at the lower end is read from the printed figure as
parallel to the member, giving a reaction normal to it. If it were instead a
horizontal plane the reaction would be
$R_v = 100/16 = 6.25\ \text{kN}$ vertical and the pin reaction
$(0,\ 5.75)\ \text{kN}$. The two readings differ by
$3.75\ \text{kN}$ acting along the member axis, which produces neither
shear nor bending moment, so the shear and moment diagrams above and every
ordinate on them are identical either way — only the reaction components
and the axial force change.