Question 2 of 8: Reactions, shear and bending moment for three structures
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2015,
07-Str-A1 — Elementary Structural Analysis. Three hours, closed book,
approved Sharp or Casio calculator only. Six questions constitute a complete
paper: answer ALL of Questions 1 to 4, then ONLY TWO of Questions 5, 6, 7 or 8.
Marks are shown in the left margin
(6 + 18 + 18 + 18 + 20 + 20 = 100). All eight questions are worked
below, because the four alternatives exercise four different methods
— moment distribution, three-hinged-frame statics, influence lines and
virtual work — and the complete set is the more useful study resource.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 2
(determinacy and stability), Ch. 3–5 (trusses, internal loadings, frames),
Ch. 6 (influence lines), Ch. 8–9 (deflections and virtual work),
Ch. 11–12 (slope-deflection and moment distribution).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3
(equilibrium and determinacy), Ch. 4 (plane trusses), Ch. 5 (beams and frames),
Ch. 7 (virtual work), Ch. 8–9 (influence lines), Ch. 16–17
(slope-deflection and moment distribution).
K. Leet, C.-M. Uang and A. Gilbert, Fundamentals of Structural
Analysis, 5th ed. — a parallel treatment of the same syllabus.
C. H. Norris, J. B. Wilbur and S. Utku, Elementary Structural
Analysis, 4th ed. — the classical text this exam code is named
after.
Check: the roller in Question 2(c).
The roller under the inclined member of Question 2(c) is drawn on a bed ruled
parallel to the member, so its reaction is taken normal to the member
axis. A vertical-roller reading is also arithmetically self-consistent. The
distinction changes only the reaction components and the axial force: the shear
and bending-moment diagrams the question asks for are identical under
either reading, and both sets of reactions are reported.
Question 2: Reactions, shear and bending moment for three structures (18 marks)
Given. Three plane structures, dimensions and loads read from
the examination figures.
Given data for Question 2
Structure
Geometry
Loading
Supports
(a) Gerber beam
Overall 21 m: pin at 0, internal hinge at 9 m, roller at 12 m, roller at 21 m
6 kN/m over 0 to 12 m; 18 kN at 15 m; 18 kN at 18 m
Pin + two rollers, one hinge
(b) Bent (L-shaped)
Horizontal member 9 m, then a 3 m leg down to the base
6 kN/m over the 9 m member; 12 kN horizontal, acting to the right at the corner
Roller at the free end of the horizontal member, pin at the foot of the leg
(c) Inclined member
Straight member on a 3 : 4 slope; pin at the foot; roller at a horizontal offset of 9.6 m (rise 7.2 m); free end a further 2.4 m horizontally
6 kN/m applied over the full 12 m horizontal projection
Pin at the foot, roller normal to the member at 9.6 m
Find. The reactions, the shear force and bending moment
diagrams for each structure, with the maximum and minimum ordinates and the sign
of every segment.
2(a) — Gerber beam with an internal hinge
Figure 2 — structure 2(a) with
its reactions, and the shear and bending moment diagrams. Sagging moment is
plotted positive (above the axis, blue); hogging is negative (below, pink).
Approach. The hinge supplies the fourth equation: take
moments about it for the length to its left, then apply global vertical
equilibrium and a global moment equation for the two remaining reactions.
Reaction at the pin, from the hinge condition. The length
from the pin to the hinge carries only the first 9 m of the uniform load,
$6 \times 9 = 54$ kN acting at 4.5 m from the pin, and the moment of everything
on that side about the hinge must vanish:
$$ \sum M_{\text{hinge, left}} = 0 : \qquad R_A(9) - 54(4.5) = 0
\quad\Longrightarrow\quad \boxed{R_A = 27\ \text{kN} \uparrow} $$
Global vertical equilibrium. The total load is the uniform
load plus the two point loads,
$$ \sum F_y = 0 : \qquad R_A + R_B + R_C = 6(12) + 18 + 18 = 108\ \text{kN}, $$
so $R_B + R_C = 81$ kN.
Global moment about the pin. Taking moments about the
support at 0 m, with the uniform load resultant 72 kN at 6 m,
$$ 12 R_B + 21 R_C = 72(6) + 18(15) + 18(18) = 1026\ \text{kN}\cdot\text{m}. $$
Solving with $R_B + R_C = 81$ gives
$$ \boxed{R_B = 75\ \text{kN} \uparrow, \qquad R_C = 6\ \text{kN} \uparrow} $$
The small reaction at the far support is the signature of this arrangement: the
right-hand span carries its own two point loads, but the 3 m overhang beyond the
hinge levers most of that load back onto the 12 m support.
Shear force. Working from the left, the shear starts at
$+27$ kN and falls at 6 kN per metre, passing through zero at
$x = 27/6 = 4.5$ m and reaching
$$ V(12^-) = 27 - 6(12) = -45\ \text{kN} $$
just left of the roller. The 75 kN reaction lifts it to $+30$ kN, each 18 kN load
steps it down, and the final $-6$ kN is closed by $R_C$:
$$ V = +30 \to +12 \to -6\ \text{kN}. $$
The maximum ordinate is $+30$ kN and the minimum is $-45$ kN.
Bending moment. The moment is zero at the pin, rises to its
peak where the shear vanishes,
$$ M_{\max} = 27(4.5) - \tfrac{1}{2}(6)(4.5)^2 = \boxed{+60.75\ \text{kN}\cdot\text{m}} $$
and returns to zero at the hinge, as it must. Beyond the hinge the beam hogs over
the roller,
$$ M(12) = 27(12) - \tfrac{1}{2}(6)(12)^2 = 324 - 432 = \boxed{-108\ \text{kN}\cdot\text{m}} $$
which is the minimum ordinate. In the right-hand span the moment climbs at
30 kN per metre to $-18$ kN·m under the first 18 kN load, crosses zero at
$x = 16.5$ m, reaches $+18$ kN·m under the second load and falls to zero at
the end support.
Sign of each segment. The beam sags (positive) from the pin
to the hinge and again from 16.5 m to the right-hand support; it hogs (negative)
from the hinge to 16.5 m. Both changes of sign are points of contraflexure and
are marked on the diagram.
2(b) — Bent with a horizontal load at the corner
Figure 3 — structure 2(b) and
its developed shear and bending moment diagrams: the abscissa runs 9 m
along the horizontal member from the roller at A to the corner C, then 3 m down
the leg from C to the pin at D. The dashed line marks the corner.
Approach. Take moments about the pin at the foot of the leg
— the 12 kN horizontal load then contributes through its 3 m lever arm
— and plot the two members on one developed abscissa so that the continuity
of moment round the rigid corner is visible.
Reactions. Horizontal equilibrium is settled by the pin
alone, so the pin pushes back 12 kN to the left. Moments about the pin, with the
54 kN load resultant 4.5 m from the roller and the 12 kN load 3 m above the pin,
give
$$ 9 R_A = 54(4.5) - 12(3) = 243 - 36 = 207
\quad\Longrightarrow\quad \boxed{R_A = 23\ \text{kN} \uparrow} $$
and vertical equilibrium then gives
$$ \boxed{D_y = 54 - 23 = 31\ \text{kN} \uparrow, \qquad
D_x = 12\ \text{kN} \leftarrow} $$
Shear in the horizontal member. $V(x) = 23 - 6x$, so the
shear runs from $+23$ kN at the roller to
$23 - 54 = -31$ kN just left of the corner, crossing zero at
$$ x_0 = \frac{23}{6} = 3.833\ \text{m}. $$
Bending moment in the horizontal member. At the point of
zero shear,
$$ M_{\max} = \frac{R_A^{\,2}}{2w} = \frac{23^2}{2(6)}
= \boxed{+44.083\ \text{kN}\cdot\text{m}} $$
a sagging (positive) peak, and at the corner
$$ M(9) = 23(9) - \tfrac{1}{2}(6)(9)^2 = 207 - 243 = \boxed{-36\ \text{kN}\cdot\text{m}} $$
a hogging (negative) value. The beam changes sign at
$x = 2 \times 3.833 = 7.667$ m.
The leg. Below the corner the only forces are the two pin
reactions, so the leg carries a constant shear of 12 kN and a moment that varies
linearly with the height $y$ above the pin,
$$ M(y) = -12\,y, $$
zero at the pin and $-36$ kN·m at the corner — equal to the moment
delivered by the horizontal member, as a rigid corner with no applied couple
requires. The leg also carries 31 kN of axial compression.
Extreme ordinates. Over the whole bent the shear ranges from
$+23$ kN to $-31$ kN, and the bending moment from $+44.083$ kN·m in the
span to $-36$ kN·m at the corner. The horizontal member sags over its first
7.667 m and hogs thereafter; the leg hogs throughout, with tension on its outer
(right-hand) face.
2(c) — Inclined member with a load on its horizontal projection
Figure 4 — structure 2(c),
with the shear and bending moment plotted against distance measured
along the member axis from the pin at A. The 6 kN/m load acts over the
12 m horizontal projection, so the member itself is 15 m long.
Approach. Because the roller bed is ruled parallel to the
member, its reaction is normal to the member; its lever arm about the pin is then
exactly the length A to B. Take moments about the pin for the reaction, resolve
the internal actions along and normal to the member, and note that the peak
moment sits under the point of zero shear.
Geometry. The member rises 3 in 4, so its unit vector is
$(0.8,\ 0.6)$ and the outward normal is $(-0.6,\ 0.8)$. The roller sits at a
horizontal offset of 9.6 m, that is
$$ L_{AB} = \sqrt{9.6^2 + 7.2^2} = 12.0\ \text{m}, \qquad
L_{AC} = \sqrt{12^2 + 9^2} = 15.0\ \text{m}. $$
The whole 12 m projection carries the load, so the resultant is
$6 \times 12 = 72$ kN acting downwards at a horizontal distance of 6 m from the
pin.
Reaction at the roller. Because the reaction is normal to
AB, its lever arm about the pin is the member length $L_{AB} = 12$ m, and
$$ \sum M_A = 0 : \qquad R_B (12) = 72(6)
\quad\Longrightarrow\quad \boxed{R_B = 36\ \text{kN}} $$
directed normal to the member, up and to the left. Its components are
$(-21.6,\ +28.8)$ kN.
Reaction at the pin. Global equilibrium then gives
$$ A_x = 21.6\ \text{kN} \rightarrow, \qquad
A_y = 72 - 28.8 = 43.2\ \text{kN} \uparrow . $$
Read instead as a vertical roller, the same figure yields $R_B = 45$ kN vertical
with $A_x = 0$ and $A_y = 27$ kN. The two readings differ by a force of
$27(0.8,\,0.6)$ acting along the member, which produces neither shear nor
moment anywhere — hence the identical diagrams noted at the head of this
paper.
Shear force. Resolving the forces to the left of a section
at horizontal coordinate $x$ onto the normal direction,
$$ V(x) = 21.6 - 4.8\,x \quad (x < 9.6\ \text{m}), $$
so the shear starts at $+21.6$ kN, passes through zero at $x = 4.5$ m —
that is 5.625 m along the member — and reaches $-24.48$ kN just below the
roller. The 36 kN reaction lifts it to $+11.52$ kN, from which it decays linearly
to zero at the free end. The extreme ordinates are $+21.6$ kN and
$-24.48$ kN.
Bending moment. Below the roller the moment about a section
at $x$ is
$$ M(x) = 27x - 3x^2, $$
a parabola whose peak lies at the point of zero shear:
$$ M_{\max} = 27(4.5) - 3(4.5)^2 = \boxed{+60.75\ \text{kN}\cdot\text{m}} $$
sagging. At the roller
$$ M(9.6) = 27(9.6) - 3(9.6)^2 = 259.2 - 276.48 = \boxed{-17.28\ \text{kN}\cdot\text{m}} $$
hogging, and beyond it the moment closes to zero at the free end, as a free end
must. The member sags from the pin to $x = 9$ m and hogs over the last 3 m of
projection.
Axial force, as a check. Resolving along the member,
$N(x) = 3.6x - 43.2$ kN, so the member carries 43.2 kN of compression at the pin,
8.64 kN just below the roller and exactly zero at the free end — the
arithmetic closes.
Question 2 — reactions and extreme diagram ordinates
Structure
Reactions
Shear: max / min
Moment: max / min
(a)
$R_A = 27$, $R_B = 75$, $R_C = 6$ kN
$+30$ / $-45$ kN
$+60.75$ (at 4.5 m) / $-108$ kN·m (at 12 m)
(b)
$R_A = 23$ kN, $D_y = 31$ kN, $D_x = 12$ kN ←
$+23$ / $-31$ kN (leg: 12 kN constant)
$+44.083$ (at 3.833 m) / $-36$ kN·m (at the corner)
(c)
$R_B = 36$ kN normal to the member; $A_x = 21.6$, $A_y = 43.2$ kN
$+21.6$ / $-24.48$ kN
$+60.75$ (at $x = 4.5$ m) / $-17.28$ kN·m (at the roller)