Question 2 of 8: Reactions, shear force and bending moment diagrams for three determinate structures
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2013
— 07-Str-A1 Elementary Structural Analysis. Three hours, CLOSED BOOK, an
approved Sharp or Casio calculator permitted. Six questions constitute a complete paper:
candidates answer ALL of Questions 1 to 5 and ONE of Questions 6, 7 or 8. Marks are shown in
the left margin (6 + 18 + 18 + 18 + 20 + 20 = 100). All eight questions are solved below,
because the three alternatives test different topics and the whole set is useful for
study.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 2 (determinacy and
stability), Ch. 3 to 5 (trusses, internal loadings, frames), Ch. 6 (influence lines),
Ch. 8 to 9 (deflections and virtual work), Ch. 11 to 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 (deflections by virtual
work), Ch. 8 (influence lines), Ch. 16 to 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 after which this exam code is named.
Canadian design context: CSA S16 Design of Steel Structures, CSA A23.3
Design of Concrete Structures and the National Building Code of Canada.
This is an analysis paper, so no code clause is needed to answer it, but every result below is
expressed in the SI units those documents use.
Sign conventions used throughout. For beams and for each individual frame
member, shear is positive when the resultant of the forces to the left of (or below) a section
acts upward, and bending moment is positive when it sags the member, that is when it puts the
underside of a beam or the inside face of a frame member in tension. Member end moments in the
slope-deflection work of Question 5 are clockwise-positive on the member, which is the usual
convention for that method. Truss forces are quoted as tension or compression rather than by
sign. Reactions are drawn in blue and applied loads in red on every figure.
A note on reading this paper. The figures are hand drawn and carry no dimensions that are not on the drawings, so the geometry of every structure below was read from the support symbols one at a time. Two readings materially affect the answers and are flagged
where they arise: the plane on which the roller of Question 2(c) bears, and the position of
the 50 kN load in Question 8.
Question 2: Reactions, shear force and bending moment diagrams for three determinate structures (18 marks)
Given. Three determinate structures, all dimensions read from the figures.
Part
Supports
Loading
Length
(a)
Pin 3 m from the left end, roller at the right end
10 kN at the free left end, 4 kN/m over the whole beam, 25 kN at midspan
15 m overall (3 m overhang + 12 m span)
(b)
Rollers at 0 m and 12 m, pin at 6 m, internal hinge at 4 m
4 kN/m from 0 m to 6 m, 24 kN at 10 m
12 m
(c)
Roller normal to the incline at the lower bend, pin at the upper bend
33.8 kN/m on the horizontal projection over the whole length
3 m level + 12 m horizontal by 5 m rise + 2 m level
Find. The reactions, then the shear force and bending moment diagrams with the maximum positive and maximum negative ordinate of each.
Part (a): 15 m beam with a 3 m overhang, pinned 3 m from the left end and on a roller at the right end. Reactions in blue.
Part (a) shear force (kN, left) and bending moment (kN·m, right). Blue is positive, red negative.
Part (b): compound beam with an internal hinge 4 m from the left roller.
Part (b) shear force (kN, left) and bending moment (kN·m, right); the moment passes through zero at the hinge.
Part (c): bent member carrying 33.8 kN/m on its horizontal projection, on a roller normal to the incline and a pin at the upper bend.
Part (c) bending moment (kN·m) plotted against the horizontal coordinate; hogging is drawn above the axis and the sagging peak below it.
Approach. Take global moments about one support to get the other reaction in parts (a) and (c); in part (b) release the structure at the internal hinge first, because the hinge supplies the fourth equation the four reaction components need. Then walk the shear from the free end, locate every point of zero shear, and evaluate the moment there and at every support and load point.
Part (a) — reactions. Measure $x$ from the free left end, so
the pin is at $x = 3$ m and the roller at $x = 15$ m. Taking moments about the pin, with the
15 m run of 4 kN/m acting as 60 kN at $x = 7.5$ m,
$$R_{15}\,(15 - 3) = 10\,(0 - 3) + 60\,(7.5 - 3) + 25\,(9 - 3)$$
$$R_{15} = \frac{-30 + 270 + 150}{12} = \boxed{32.5\ \text{kN}\ \uparrow}$$
and vertical equilibrium gives
$$R_{3} = 10 + 60 + 25 - 32.5 = \boxed{62.5\ \text{kN}\ \uparrow}$$
Part (a) — shear. Starting from the free end the shear falls
under the 10 kN load and then under the distributed load at 4 kN per metre, reaching
$-10 - 4(3) = -22$ kN just left of the pin. The pin adds 62.5 kN, so the shear jumps to
$+40.5$ kN, then falls to $40.5 - 4(6) = +16.5$ kN just left of the 25 kN load, drops to
$-8.5$ kN just right of it, and reaches $-8.5 - 4(6) = -32.5$ kN at the roller, where the
32.5 kN reaction closes the diagram. The extreme ordinates are
$$V_{\max}^{+} = \boxed{+40.5\ \text{kN}}, \quad V_{\max}^{-} = \boxed{-32.5\ \text{kN}}$$
Part (a) — bending moment. Over the overhang
$M = -10x - 2x^{2}$, which reaches $-30 - 18 = -48$ kN·m at the pin. That is the largest
hogging value, because the shear does not pass through zero anywhere in the 3 m to 9 m reach
(it runs from $+40.5$ to $+16.5$ kN) nor in the 9 m to 15 m reach (from $-8.5$ to $-32.5$ kN).
The moment therefore peaks at the 25 kN load, where the shear changes sign:
$$M(9) = -10(9) - 2(9)^{2} + 62.5(6) = -90 - 162 + 375 = \boxed{+123.0\ \text{kN}\cdot\text{m}}$$
Between the two the moment vanishes at
$-2x^{2} + 52.5x - 187.5 = 0$, that is at $x = 4.264$ m, which is the point of
contraflexure.
Part (b) — use the hinge to unlock the reactions. Four
reaction components (one at each roller, two at the pin) face three equilibrium equations, and
the internal hinge at $x = 4$ m supplies the fourth. Isolate the 4 m piece to the left of the
hinge, which carries $4(4) = 16$ kN of distributed load at its own mid-length, and take
moments about the hinge:
$$R_{0}\,(4) - 16\,(2) = 0 \;\Rightarrow\; R_{0} = \boxed{8.0\ \text{kN}\ \uparrow}$$
Part (b) — the remaining two reactions. Carry the hinge force
into the right-hand piece. That piece runs from the hinge to the right roller and carries the
remaining $4(2) = 8$ kN of distributed load at $x = 5$ m, the 24 kN load at $x = 10$ m, and the
8 kN downward pull that the left piece exerts through the hinge. Moments about the pin at
$x = 6$ m give
$$R_{12}\,(6) = 24\,(10 - 6) - 8\,(6 - 4) - 8\,(6 - 5) = 96 - 16 - 8 = 72$$
$$\begin{aligned} R_{12} &= \boxed{12.0\ \text{kN}\ \uparrow} \\ R_{6} &= 4(6) + 24 - 8 - 12 = \boxed{28.0\ \text{kN}\ \uparrow} \end{aligned}$$
Part (b) — diagrams. The shear starts at $+8$ kN, falls at
4 kN per metre to zero at $x = 2$ m, continues to $-16$ kN just left of the pin, jumps to
$+12$ kN, holds until the 24 kN load takes it to $-12$ kN, and holds to the right roller.
Hence $V_{\max}^{+} = +12$ kN and $V_{\max}^{-} = -16$ kN. Integrating,
$M(2) = 8(2) - 2(2)^{2} = +8$ kN·m, the moment is zero at the hinge as it must be,
and
$$M(6) = 8(6) - 2(6)^{2} = 48 - 72 = \boxed{-24.0\ \text{kN}\cdot\text{m}}$$
$$M(10) = M(6) + 12(4) = -24 + 48 = \boxed{+24.0\ \text{kN}\cdot\text{m}}$$
The moment is negative from $x = 4$ m to $x = 8$ m and positive elsewhere.
Part (c) — geometry and total load. The member is a single
bent beam: 3 m level, then 12 m horizontal by 5 m rise, then 2 m level, so the sloping reach
is $\sqrt{12^{2} + 5^{2}} = 13$ m and its direction cosines are $12/13$ and $5/13$. The
33.8 kN/m acts on the horizontal projection, so
$$W = 33.8\,(17) = 574.6\ \text{kN} \quad\text{at}\quad \bar{x} = 8.5\ \text{m}$$
Part (c) — reactions. The roller sits on a plane parallel to
the incline, so its reaction $R$ is normal to the incline, with components
$-5R/13$ horizontally and $12R/13$ vertically. Moments about the pin at the upper bend
$(15,\,5)$, noting that the perpendicular distance from that pin to the line of $R$ is exactly
the 13 m sloping length,
$$574.6\,(15 - 8.5) = 13R \;\Rightarrow\; R = \frac{3734.9}{13} = \boxed{287.3\ \text{kN}}$$
so the roller pushes 110.5 kN to the left and 265.2 kN upward, and the pin carries
$$\begin{aligned} H &= \boxed{110.5\ \text{kN}\rightarrow} \\ V &= 574.6 - 265.2 = \boxed{309.4\ \text{kN}\uparrow} \end{aligned}$$
Part (c) — diagrams. On the 3 m cantilever the shear is the
accumulated load, $-33.8x$, reaching $-101.4$ kN, and the moment reaches
$-33.8(3)^{2}/2 = -152.1$ kN·m (hogging). Just past the roller the shear taken
perpendicular to the incline is
$42.5 + (265.2 - 101.4)(12/13) = +193.7$ kN, and it falls to
$42.5 - 241.8(12/13) = -180.7$ kN just below the pin, vanishing where
$265.2 - 33.8x = -46.04$, that is at $x = 9.208$ m. There the sagging moment is greatest:
$$M_{\max} = \boxed{499.3\ \text{kN}\cdot\text{m}\ \text{sagging}}$$
The right-hand 2 m cantilever hogs $33.8(2)^{2}/2 = 67.6$ kN·m at the pin and closes to
zero at the free end.
Part
Reactions
Max +V
Max −V
Max +M
Max −M
(a)
62.5 kN at the pin, 32.5 kN at the roller
+40.5 kN just right of the pin
−32.5 kN at the roller
+123.0 kN·m at the 25 kN load
−48.0 kN·m at the pin
(b)
8.0 kN, 28.0 kN, 12.0 kN
+12.0 kN between the pin and the 24 kN load
−16.0 kN just left of the pin
+24.0 kN·m under the 24 kN load
−24.0 kN·m at the pin
(c)
287.3 kN normal to the incline; pin 110.5 kN → and 309.4 kN ↑
+193.7 kN just above the roller
−180.7 kN just below the pin
+499.3 kN·m at 9.208 m from the free end
−152.1 kN·m at the roller
Check: the roller of part (c) is drawn on hatching that runs parallel to the inclined member, so its reaction has been taken normal to the incline. That reading is what makes the structure determinate with a pin at the far end and produces the clean 13 m lever arm used above. Had the plane been horizontal the roller reaction would be 311.2 kN vertical and the pin would carry 0 kN horizontally and 263.4 kN vertically. The two reaction sets differ only by a pair of equal and opposite forces along the line from the roller to the pin, which is the axis of the incline, so the shear force and bending moment diagrams are unchanged; only the reactions and the axial force in the inclined reach change. State the reading you adopt before you solve.