Question 2 of 8: Reactions, Shear and Bending Moment Diagrams
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 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 + 18 + 20 + 18 + 20). Marks are shown in the left margin.
All eight questions are worked below, because the three
alternatives exercise three quite different methods — three-hinged-frame
statics, influence lines and virtual work — 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 states the task, the drawing carries 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 along
the positive local normal of the member; 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 5 the member-end moments follow the usual convention,
clockwise on the member end taken as positive, so that the sagging moment is
$+M_{ij}$ at the left end of a member and $-M_{ji}$ at its right end.
Given. A straight beam 16 m long measured from the left-hand
pin. The concentrated load and the distributed load are read from the figure as
follows.
Given data, structure 2(a)
Quantity
Value
Pin support A
x = 0
Concentrated load
60 kN downward at x = 6 m
Uniformly distributed load
6 kN/m from x = 6 m to the right-hand end at x = 16 m
Roller support B
x = 12 m
Overhang
4 m, from x = 12 m to x = 16 m
The extent of the load block is the reading that decides the whole answer.
Its left edge sits exactly on the 60 kN arrow and its right edge on the end of
the member line, so the ruling covers 10 m and not the 6 m bay between the load
and the roller. The reactions that follow are integers, which is the usual
confirmation that a hand-drawn extent has been read correctly.
Find. The two reactions, and the shear and bending moment
diagrams with the maximum and minimum ordinates labelled.
Structure 2(a): loading, reactions, shear force diagram and bending moment diagram. Sagging moments are plotted above the axis.
Approach. Take moments about the pin to find the roller
reaction, then build the shear diagram from the left by accumulating the loads
and read the moment diagram off it, the moment being the running area under the
shear curve.
Resolve the loading into two resultants. The distributed
load acts over $16 - 6 = 10$ m, so
$$W = w L = (6\ \text{kN/m})(10\ \text{m}) = 60\ \text{kN}$$
acting at the centroid of the block, $x = 11$ m. Together with the 60 kN
concentrated load at $x = 6$ m the total applied load is 120 kN.
Take moments about A to find the roller reaction.
With $R_B$ acting at $x = 12$ m,
$$\sum M_A = 0: \quad 12 R_B = (60)(6) + (60)(11) = 360 + 660 = 1020$$
$$R_B = \boxed{85\ \text{kN} \uparrow}$$
Vertical equilibrium gives the pin reaction.
$$R_A = 120 - 85 = \boxed{35\ \text{kN} \uparrow}$$
Both reactions are integers, which is the arithmetic check on the load extent
read in the Given. block.
Build the shear diagram from the left. Over
$0 \le x \lt 6$ m no load acts, so $V = +35$ kN, constant. At $x = 6$ m the
60 kN load drops the shear to $35 - 60 = -25$ kN, after which the ruling
removes 6 kN per metre:
$$V(x) = -25 - 6(x - 6)\ \text{kN}, \qquad 6 \le x \lt 12\ \text{m}$$
so that just left of the roller $V = -25 - 36 = -61$ kN. The roller adds
85 kN, lifting the shear to $+24$ kN, and it then falls linearly to zero at the
free end, as it must.
Locate the maximum sagging moment. The shear does not pass
through zero inside a span here; it jumps straight from $+35$ kN to $-25$ kN at
the concentrated load, so the peak sagging moment is at $x = 6$ m:
$$M_{\max} = R_A x = (35)(6) = \boxed{+210\ \text{kN}\cdot\text{m}}$$
Compute the hogging moment over the roller. The tidiest
route is from the right, using the overhang alone:
$$M_B = -\frac{w a^{2}}{2} = -\frac{(6)(4)^{2}}{2} = \boxed{-48\ \text{kN}\cdot\text{m}}$$
Working from the left gives the same figure,
$M = (35)(12) - (60)(6) - 3(6)^{2} = 420 - 360 - 108 = -48\ \text{kN}\cdot\text{m}$,
which is the check that the shear diagram and the reactions agree.
Find the point of contraflexure. Between the load and the
roller the moment is $M = 210 - 25u - 3u^{2}$ with $u = x - 6$; setting this to
zero gives $3u^{2} + 25u - 210 = 0$, so $u = 5.18$ m and the moment changes
sign at $x = 11.18$ m. The diagram is therefore positive (sagging) from the
pin to $x = 11.18$ m and negative (hogging) from there to the free end.
(b) Propped cantilever with an internal hinge and an overhang
Given. A beam 14 m long built into a wall at the left-hand
end, with an internal hinge 4 m from the wall, a roller 6 m beyond the hinge
(at x = 10 m) and a free end 4 m beyond the roller. A uniformly distributed
load of 6 kN/m covers the whole 14 m — the load block on the figure runs
from the wall face to the free end.
Find. The reactions at the built-in end and at the roller,
and the shear and bending moment diagrams with maximum and minimum ordinates.
Structure 2(b): loading, reactions, shear force diagram and bending moment diagram. The moment is zero at the internal hinge.
Approach. The hinge makes the beam determinate, so start
with the free body to the right of the hinge, which contains only one unknown
reaction; the force it transmits back through the hinge then loads the
cantilever portion.
Free body of the beam to the right of the hinge. That
piece runs from $x = 4$ m to $x = 14$ m, carries $W = (6)(10) = 60$ kN at
$x = 9$ m, and is held by the roller at $x = 10$ m and by the vertical force
$F$ that the hinge transmits. Moments about the roller give
$$6F = (60)(1) \quad\Rightarrow\quad F = \boxed{10\ \text{kN}}$$
Vertical equilibrium of the same piece gives the roller
reaction.
$$R_2 = 60 - 10 = \boxed{50\ \text{kN} \uparrow}$$
Transfer the hinge force to the cantilever. The 4 m piece
between the wall and the hinge carries its own $6 \times 4 = 24$ kN of ruling
plus the 10 kN reaction the right-hand piece pushes down through the hinge:
$$R_1 = 24 + 10 = \boxed{34\ \text{kN} \uparrow}$$
$$M_1 = -\left[ (24)(2) + (10)(4) \right] = -48 - 40 = \boxed{-88\ \text{kN}\cdot\text{m}}$$
the negative sign meaning a hogging moment, tension on the top of the beam at
the wall.
Write the shear as one expression. Because the ruling is
continuous the shear is simply
$$V(x) = 34 - 6x\ \text{kN}, \qquad 0 \le x \lt 10\ \text{m}$$
falling from $+34$ kN at the wall through $+10$ kN at the hinge to $-26$ kN just
left of the roller, where the 50 kN reaction lifts it to $+24$ kN. Over the
overhang it falls to zero at the free end.
Locate and evaluate the peak sagging moment. The shear
vanishes at
$$x_{0} = \frac{34}{6} = 5.667\ \text{m}$$
and the moment there is
$$M(x_{0}) = -88 + 34(5.667) - 3(5.667)^{2} = \boxed{+8.33\ \text{kN}\cdot\text{m}}$$
Check the two other controlling ordinates. At the hinge
$M(4) = -88 + 136 - 48 = 0$, exactly as a hinge requires, which validates
$R_1$ and $M_1$ together. Over the roller the overhang gives
$M = -(6)(4)^{2}/2 = -48\ \text{kN}\cdot\text{m}$, and the moment is negative
from the wall to $x = 4$ m, positive from $x = 4$ m to $x = 7.33$ m, and
negative again to the free end.
(c) Bent member on a pin and a roller
Given. A single bent member. The pin is taken as the origin;
the knee sits 12 m to the right of it and 9 m above it, and the member then
falls 4 m over a further 3 m to a roller resting on a horizontal plane. A
uniformly distributed load of 10 kN/m acts on the horizontal projection over
the whole 15 m width.
Given data, structure 2(c)
Quantity
Value
Pin support, node 1
(0, 0)
Knee, node 2
(12 m, 9 m); member 1-2 length 15 m, slope 3:4
Roller support, node 3
(15 m, 5 m); member 2-3 length 5 m, slope 4:3
Distributed load
10 kN/m on the horizontal projection, x = 0 to 15 m
Roller plane
horizontal, so the reaction is vertical
Check: the roller at node 3 is drawn
on horizontal hatching, so its reaction is taken as vertical. That reading is
worth stating because a roller on a plane parallel to the inclined member would
give a reaction normal to the member instead. It happens not to matter for the
diagrams: two such readings differ by a force acting along the member axis,
which produces neither shear nor bending moment anywhere, so only the reaction
components and the axial force would change.
Find. The reactions, and the shear and bending moment
diagrams developed along the member axis with maximum and minimum ordinates.
Structure 2(c): geometry and reactions, with the shear and bending moment diagrams developed along the member axis. The abscissa s runs 0 to 15 m on member 1-2 and 15 to 20 m on member 2-3.
Approach. Because the roller reaction and every applied
load are vertical, the pin can carry no horizontal force; the bending moment at
any section is then simply the moment of the vertical forces to its left, and
the shear is the component of that same resultant taken perpendicular to
whichever member the section lies on.
Establish that the pin carries no thrust. The only applied
loading is vertical and the roller reaction is vertical, so horizontal
equilibrium gives $H_1 = \boxed{0}$. This is what makes the rest of the
question short.
Find the reactions. The total load is
$W = (10)(15) = 150$ kN acting at the centroid of the projection, $x = 7.5$ m.
Moments about the pin, with the roller 15 m away horizontally, give
$$15 R_3 = (150)(7.5) = 1125 \quad\Rightarrow\quad R_3 = \boxed{75\ \text{kN} \uparrow}$$
$$V_1 = 150 - 75 = \boxed{75\ \text{kN} \uparrow}$$
Write the bending moment as a function of the horizontal
coordinate. Since all forces are vertical, the height of the section
does not enter and
$$M(x) = 75x - \frac{10x^{2}}{2} = 75x - 5x^{2}\ \text{kN}\cdot\text{m}$$
holds over the entire structure, both members included.
Evaluate the peak moment. Differentiating,
$\mathrm{d}M/\mathrm{d}x = 75 - 10x = 0$ at $x = 7.5$ m, which lies on the
inclined member at $s = 7.5/0.8 = 9.375$ m along its axis. There
$$M_{\max} = (75)(7.5) - 5(7.5)^{2} = 562.5 - 281.25 = \boxed{+281.25\ \text{kN}\cdot\text{m}}$$
Evaluate the moment at the knee. Substituting $x = 12$ m,
$$M_{2} = (75)(12) - 5(12)^{2} = 900 - 720 = \boxed{+180\ \text{kN}\cdot\text{m}}$$
and $M = 0$ at both supports, so the whole bending moment diagram is sagging;
there are no negative segments and the minimum ordinates are the zeros at the
two ends.
Resolve the shear on member 1-2. Its axis is the unit
vector $(0.8,\ 0.6)$, so the shear is $0.8$ times the net vertical force to the
left of the section:
$$V = 0.8\left(75 - 10x\right)$$
which runs from $+60$ kN at the pin to $0.8(75 - 120) = -36$ kN at the knee,
passing through zero at $x = 7.5$ m as the moment peak requires.
Resolve the shear on member 2-3. Its axis is
$(0.6,\ -0.8)$, so the shear is now $0.6$ times the same net vertical force:
$$V = 0.6\left(75 - 10x\right)$$
giving $-27$ kN just past the knee and $-45$ kN just before the roller. The step
at the knee is not an error — it is the change of direction of the member,
which redistributes the same resultant between shear and axial force.
Question 2 — reactions and controlling diagram ordinates