Question 2 of 8: Reactions, shear force and bending moment diagrams for three structures
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations,
May 2015 — 07-Str-A1 Elementary Structural Analysis. Three hours,
CLOSED BOOK, an approved Sharp or Casio calculator permitted. Six questions
constitute a complete paper: answer ALL of Questions 1 to 5 and ONE of
Questions 6, 7 or 8. Marks are shown in the left margin
(6 + 18 + 16 + 18 + 20 + 22 = 100). All eight questions are solved below,
because the three alternatives exercise quite different methods —
slope-deflection, virtual work and the statics of a three-hinged frame —
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 (slope-deflection).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3
(equilibrium and determinacy), Ch. 4 (plane trusses), Ch. 5 (beams and frames),
Ch. 7 (deflections by the method of virtual work), Ch. 8–9 (influence
lines), Ch. 16 (slope-deflection).
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: every support type, hinge and member below
was read off the drawings, not off the printed text. In this subject the text carries almost no data: spans, loads, support types and hinge positions exist only in the hand-drawn figures. The classification in Question 1 in particular turns
entirely on telling a pin (plain triangle on hatching) from a roller (triangle
over two rollers) and a rigid joint from an internal hinge (small open
circle).
Question 2: Reactions, shear force and bending moment diagrams for three structures (18 marks)
Check: the right-hand support of structure (a) is
taken to be at the 12 m dimension point. The printed figure of structure (a)
carries only one support symbol, drawn at the 2 m mark, yet the question asks
for reactions and a bending-moment diagram, which needs two. The dimension
string 2 m + 5 m + 5 m + 4 m places nodes at 0, 2, 7, 12 and 16 m, and the two
10 kN/m load blocks sit exactly over 0–2 m and 12–16 m. Reading the
second support at 12 m makes those two blocks symmetric overhang loads and puts
the 60 kN load at the exact mid-span of the 10 m interior span, and every
reaction and ordinate then comes out in round numbers (44, 76, 100, 80 kN and
kN·m). That is the intended structure; the alternative reading, a support
at the far right end, produces no round value anywhere. The solution is
therefore written for a pin at 2 m and a roller at 12 m.
(a) Beam with two loaded overhangs and a central point load
Given. A 16 m beam supported at $x = 2$ m (pin, A) and
$x = 12$ m (roller, B), carrying 10 kN/m over the left overhang
(0 to 2 m), a 60 kN point load at $x = 7$ m, and 10 kN/m over the right overhang
(12 to 16 m).
Given data — structure 2(a)
Quantity
Value
Overall length
16 m (2 + 5 + 5 + 4)
Supports
pin at 2 m, roller at 12 m
Left overhang load
10 kN/m over 0–2 m (20 kN at $x=1$ m)
Point load
60 kN at $x = 7$ m
Right overhang load
10 kN/m over 12–16 m (40 kN at $x=14$ m)
Find. The two reactions, and the shear force and bending
moment diagrams with the maximum positive and negative ordinates labelled.
Figure 2 — structure 2(a):
loading, shear force diagram and bending moment diagram. Sagging moments are
plotted above the axis and hogging below.
Approach. Replace each distributed block by its resultant,
take moments about A for the roller reaction, then integrate the load to build
the shear diagram and integrate the shear to build the moment diagram.
Reduce the distributed loads. The left block is
$W_1 = 10 \times 2 = 20$ kN acting at $x = 1$ m and the right block is
$W_2 = 10 \times 4 = 40$ kN acting at $x = 14$ m. Together with the 60 kN load
the total downward force is 120 kN.
Take moments about A ($x = 2$ m). With $R_B$ acting 10 m to
the right of A,
$$ 10\,R_B = 20(1-2) + 60(7-2) + 40(14-2) = -20 + 300 + 480 = 760 $$
so that
$$ \boxed{R_B = 76.0\ \text{kN}\ (\uparrow)} $$
Vertical equilibrium. Summing forces,
$R_A = 120 - 76 = \boxed{44.0\ \text{kN}\ (\uparrow)}$. As a check, moments
about B give $10 R_A = 20(12-1) + 60(12-7) - 40(14-12) = 220 + 300 - 80 = 440$,
the same answer.
Shear force. Working from the left free end, the shear falls
linearly to $-20$ kN just left of A, jumps by $+44$ kN to $+24$ kN, stays
constant to the 60 kN load, drops to $-36$ kN, stays constant to B, jumps by
$+76$ kN to $+40$ kN, and falls linearly to zero at the free right end. The
governing ordinate is
$$ \boxed{V_{\max} = +40\ \text{kN just right of B}} $$
with $-36$ kN the largest negative value.
Bending moment. Integrating the shear, the moment is zero at
both free ends. Over the left overhang it is hogging,
$M = -10x^{2}/2$, reaching $-20$ kN·m at A. It then rises linearly at
24 kN per metre to the point load,
$$ M(7) = -20 + 24(5) = \boxed{+100\ \text{kN}\!\cdot\!\text{m}} , $$
falls at 36 kN per metre to $M(12) = 100 - 36(5) = \boxed{-80\ \text{kN}\!\cdot\!\text{m}}$
at B, and closes to zero at the free end. The right-hand overhang value checks
independently as $-10(4)^{2}/2 = -80$ kN·m.
Read off the sign changes. The moment is negative (hogging)
from 0 to 2 m and again from about 9.8 m to 16 m, and positive (sagging) in
between; the contraflexure point in the interior span is where the linear branch
from $+100$ crosses zero, at $x = 7 + 100/36 = 9.78$ m.
(b) Continuous beam with two internal hinges and a built-in end
Given. A 22 m beam carrying 2 kN/m over its whole length,
supported on rollers at $x = 0$ (A) and $x = 10$ m (B), with internal hinges at
$x = 12$ m (C) and $x = 20$ m (D) and a built-in end at $x = 22$ m (E).
Find. All reactions, including the fixing moment, and the two
diagrams with their extreme ordinates.
Figure 3 — structure 2(b):
loading, shear force and bending moment. The moment passes through zero at each
of the two hinges, as it must.
Approach. The two hinges cut the beam into three rigid
lengths. Analyse the suspended length C–D first, because it is simply
supported by the hinge forces; then carry those forces into the cantilever
D–E and into the two-span length A–C.
Check determinacy. There are $r = 1 + 1 + 3 = 5$ reaction
components and two hinges, so $i = 5 - (3 + 2) = 0$: the beam is determinate and
can be solved by statics alone.
The suspended length C–D. It spans 8 m between the two
hinges and carries 2 kN/m, so by symmetry each hinge delivers
$$ V_h = \tfrac{1}{2}(2)(8) = \boxed{8.0\ \text{kN}} $$
to the lengths on either side.
The cantilever D–E. This 2 m length carries its own
4 kN of distributed load plus the 8 kN handed over at the hinge D. The built-in
end therefore takes
$$ V_E = 4 + 8 = \boxed{12.0\ \text{kN}\ (\uparrow)} $$
and, taking moments about E,
$$ M_E = -\left[8(2) + 4(1)\right] = \boxed{-20.0\ \text{kN}\!\cdot\!\text{m}} $$
(hogging, as a built-in end must be).
The length A–C. It runs 12 m from the left end to the
hinge C, carries $2 \times 12 = 24$ kN of distributed load acting at its
mid-length, and carries the 8 kN handed down at C. Taking moments about A,
$$ 10\,R_B = 24(6) + 8(12) = 144 + 96 = 240
\;\Rightarrow\; \boxed{R_B = 24.0\ \text{kN}\ (\uparrow)} $$
and vertical equilibrium gives
$R_A = 24 + 8 - 24 = \boxed{8.0\ \text{kN}\ (\uparrow)}$.
Global check. The three upward forces are
$8 + 24 + 12 = 44$ kN, exactly the total load $2 \times 22 = 44$ kN.
Shear force. $V = 8 - 2x$ on the first span, so the shear
vanishes at $x = 4$ m and reaches $-12$ kN just left of B; the roller lifts it to
$+12$ kN, after which it falls at 2 kN per metre, passing 8 kN at the hinge C and
zero at $x = 16$ m (the mid-point of the suspended length), reaching $-8$ kN at
D and $-12$ kN just left of E. The largest ordinate either way is
$\boxed{12\ \text{kN}}$.
Bending moment. On the first span
$M = 8x - x^{2}$, giving the sagging maximum
$$ M(4) = 32 - 16 = \boxed{+16.0\ \text{kN}\!\cdot\!\text{m}} $$
and $M(10) = 80 - 100 = \boxed{-20.0\ \text{kN}\!\cdot\!\text{m}}$ over the
roller B. The moment returns to zero at the hinge C, rises to
$2(8)^{2}/8 = +16.0$ kN·m at the middle of the suspended length,
returns to zero at the hinge D, and falls to $-20.0$ kN·m at the built-in
end.
The largest positive and negative ordinates therefore happen to be equal in
pairs, $+16$ kN·m at $x = 4$ m and $x = 16$ m and $-20$ kN·m at
$x = 10$ m and $x = 22$ m — a useful reminder that a Gerber (cantilever)
beam is laid out precisely to balance the sagging and hogging peaks.
(c) Beam with a cross-piece carrying an applied couple
Given. A 10 m beam, pinned at A ($x = 0$) and on a roller at
B ($x = 10$ m), with a vertical post rigidly attached at C ($x = 6$ m) extending
2 m above and 3 m below the beam. A 10 kN horizontal force acts to the left at
the top of the post and a 10 kN horizontal force acts to the right at the
bottom.
Find. The reactions and the two diagrams, for the beam and
for the post.
Figure 4 — structure 2(c). The
two 10 kN forces are equal and opposite, so the post delivers a pure couple to
the beam and the shear is constant along the whole span.
Approach. Recognise that the two horizontal forces form a
couple, reduce them to a single moment applied at C, then solve the beam.
Reduce the pair of forces. The two 10 kN forces are equal,
opposite and not collinear, so their resultant force is zero and they are
statically equivalent to a couple. Taking moments about C,
$$ M_0 = 10(2) + 10(3) = \boxed{50\ \text{kN}\!\cdot\!\text{m}} $$
acting anticlockwise. Because the resultant force vanishes,
$\Sigma F_x = 0$ gives $A_x = \boxed{0}$.
Reactions from the couple. A couple is the same about every
point, so taking moments about A,
$$ 10\,B_y + 50 = 0 \;\Rightarrow\; \boxed{B_y = 5.0\ \text{kN}\ (\downarrow)} $$
and vertical equilibrium gives
$A_y = \boxed{5.0\ \text{kN}\ (\uparrow)}$. The reactions form a couple of
$5 \times 10 = 50$ kN·m that balances the applied one, as it must.
Shear force in the beam. No vertical load acts between the
supports, so the shear is constant at
$\boxed{V = +5.0\ \text{kN}}$ from A to B.
Bending moment in the beam. Because the shear is constant,
the moment varies linearly. From the left, $M = 5x$, so
$$ M(6^-) = \boxed{+30.0\ \text{kN}\!\cdot\!\text{m}} , $$
and the applied couple produces a step of 50 kN·m at C. From the right,
$M(6^+) = -5(10-6) = \boxed{-20.0\ \text{kN}\!\cdot\!\text{m}}$, and the
difference $30 - (-20) = 50$ kN·m is exactly the applied couple, which is
the check on the sign of the step.
The post. Each arm is a cantilever off the beam. The upper
arm carries the 10 kN force at 2 m, so its moment grows linearly from zero at
the free top to $10(2) = 20$ kN·m at the beam, with a constant shear of
10 kN; the lower arm carries the 10 kN force at 3 m, giving
$10(3) = 30$ kN·m at the beam. The two moments add to the 50 kN·m
step, and each arm carries a constant 10 kN shear.
Question 2 — reactions and extreme ordinates
Structure
Reactions
Max +ve / −ve shear
Max +ve / −ve moment
(a)
$R_A = 44.0$ kN ↑ at 2 m; $R_B = 76.0$ kN ↑ at 12 m