Question 2 of 8: Reactions, shear 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,
December 2014 — 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 + 18 + 18 + 20 + 20 = 100). All eight questions are solved below,
because the three alternatives test quite different methods
— moment distribution, statics of a three-hinged frame, 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 (deflections by 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: support types were read from the printed drawings, not from the text. Every support symbol, internal hinge and member line quoted below was taken from the drawings. In this subject the drawings carry data that appears nowhere
in the printed text, and the classification in Question 1 in particular turns
entirely on telling a pin (plain triangle on hatching) from a roller (triangle
over rollers) and a rigid joint from a hinge (small open circle).
Question 2: Reactions, shear and bending moment diagrams for three structures (18 marks)
Given. Three determinate structures, all dimensions and
loads read from the drawings.
Given data for the three structures
Part
Geometry
Loading
Supports
(a)
14 m beam; pin 2 m from the left tip, roller 8 m further,
4 m of overhang beyond
20 kN at the left tip; 8 kN/m over the whole
14 m
pin + roller
(b)
Inclined leg 4.5 m by 6 m (length 7.5 m) meeting a 7.5 m
horizontal member; roller 5.5 m along it
10 kN/m normal to the inclined
leg; 10 kN/m vertical on the horizontal member
pin at the foot +
roller
(c)
16 m in four 4 m bays; built-in left end, internal hinge at
4 m, roller at 12 m
4 kN/m over 0–8 m, 2 kN/m over 8–16 m,
20 kN at 8 m and at 16 m
fixed + roller
Find. All support reactions, and shear and bending moment
diagrams labelled with the maximum positive and negative ordinates.
Approach. Each structure is determinate, so global
equilibrium alone fixes the reactions — with the hinge in part (c)
supplying the fourth equation as $\sum M = 0$ for the segment on one side of it
— after which the diagrams follow by integrating the load.
(a) Beam with a tip load and a full-length distributed load
Beam (a): loading, reactions, shear force and bending moment. Note that the load block on the exam drawing runs the full 14 m, not just the 8 m between supports.
Total load and reactions. The distributed load acts over
the entire 14 m, so its resultant is $W = wL = 8(14) = 112$ kN acting at
mid-length, $x = 7$ m, and the tip load adds 20 kN at $x = 0$. Taking moments
about the pin at $x = 2$ m,
$$R_{\text{roller}} = \frac{20(0 - 2) + 112(7 - 2)}{10 - 2}
= \frac{-40 + 560}{8} = 65\ \text{kN}$$
and vertical equilibrium gives
$$R_{\text{pin}} = 20 + 112 - 65 = \boxed{67\ \text{kN}}, \qquad
R_{\text{roller}} = \boxed{65\ \text{kN}}$$
Both act upwards. The clean values are a useful check that the load really does
cover the full span.
Shear force. Starting at the free tip and accumulating
upward forces, $V = -20 - 8x$ on the first 2 m, so $V$ falls from
$-20$ kN to $-36$ kN at the pin, jumps to $-36 + 67 = +31$ kN, falls again to
$31 - 8(8) = -33$ kN just left of the roller, jumps to $+32$ kN and runs out to
zero at the right tip. The largest ordinates are
$$V_{\max}^{+} = +32\ \text{kN}, \qquad V_{\max}^{-} = -36\ \text{kN}$$
Shear passes through zero at $x = 2 + 31/8 = 5.875$ m.
Bending moment. Integrating the shear,
$M = -20x - 4x^{2}$ up to the pin and $M = -20x - 4x^{2} + 67(x - 2)$ between
the supports. At the pin $M = -56\ \text{kN}\cdot\text{m}$; at the point of
zero shear $M = +4.06\ \text{kN}\cdot\text{m}$; at the roller
$M = -64\ \text{kN}\cdot\text{m}$; and the moment closes to zero at the free
right tip, as it must. Hence
$$M_{\max}^{+} = \boxed{+4.06\ \text{kN}\cdot\text{m}}, \qquad
M_{\max}^{-} = \boxed{-64\ \text{kN}\cdot\text{m}}$$
The diagram is negative (hogging, tension on top) over almost the whole beam,
with a very shallow positive lobe between the two points of contraflexure. This
is characteristic of a beam whose overhangs are long relative to the span: the
cantilever moments very nearly swallow the sagging moment of the interior
span.
(b) Bent frame with a load normal to the inclined leg
Frame (b): the 10 kN/m on the inclined leg acts normal to that member, so its resultant is 10(7.5) = 75 kN perpendicular to the leg. Bending moment is plotted on the tension face.
Resolve the load on the inclined leg. The leg rises 6 m
over a horizontal run of 4.5 m, so its length is
$\sqrt{4.5^{2} + 6^{2}} = 7.5$ m and its direction cosines are
$(0.6,\ 0.8)$. The load block is drawn parallel to the member with its arrows
perpendicular to it, so the intensity is per metre of member and the
resultant is
$$F = 10(7.5) = 75\ \text{kN} \quad \text{acting along } (0.8,\ -0.6),
\quad \text{i.e. } (60,\ -45)\ \text{kN}$$
applied at the mid-length of the leg. The vertical load on the top member is
$10(7.5) = 75$ kN at its mid-length.
Reactions. Taking moments about the pin at the foot, with
the corner 4.5 m to the right and 6 m above it and the roller a further 5.5 m
along the top member,
$$R_{\text{roller}} = \frac{281.25 + 618.75}{10} = \boxed{90\ \text{kN}}$$
Then horizontal and vertical equilibrium give
$$H_{\text{pin}} = \boxed{60\ \text{kN} \text{ (to the left)}}, \qquad
V_{\text{pin}} = 75 - 45 + \ldots = \boxed{30\ \text{kN (up)}}$$
where the vertical sum is $V_{\text{pin}} - 45 - 75 + 90 = 0$.
Internal forces in the inclined leg. Resolving the base
reaction along and normal to the member, the axial force is a constant
$12$ kN tension, while the shear falls linearly from $66$ kN at the pin to
$-9$ kN at the corner, vanishing at $s = 66/10 = 6.6$ m. The bending moment
therefore peaks a little below the corner:
$$M_{\max} = \boxed{217.8\ \text{kN}\cdot\text{m}} \ \text{at } s = 6.6
\ \text{m}, \qquad M_{\text{corner}} = 213.75\ \text{kN}\cdot\text{m}$$
Both put the outside (upper-left) face of the leg in tension.
Internal forces in the horizontal member. Working from the
free right-hand tip, $M = -5(7.5 - \xi)^{2}$ over the 2 m overhang, reaching
$-20\ \text{kN}\cdot\text{m}$ at the roller, and
$M = -5(7.5-\xi)^{2} + 90(5.5-\xi)$ inboard of it, which returns
$+213.75\ \text{kN}\cdot\text{m}$ at the corner. Moment continuity at the
rigid corner is the check that the two limbs have been solved consistently. The
diagram crosses zero at $\xi = 5.21$ m from the corner. The shear is $-15$ kN
at the corner, $-70$ kN just left of the roller, $+20$ kN just right of it and
zero at the tip, so
$$V_{\max}^{-} = \boxed{-70\ \text{kN}}, \qquad
M_{\max}^{+} = \boxed{+213.75\ \text{kN}\cdot\text{m}}, \qquad
M_{\max}^{-} = \boxed{-20\ \text{kN}\cdot\text{m}}$$
Check: the 10 kN/m on the inclined leg is taken
normal to the member and per metre of member. The load block on the
exam drawing is ruled parallel to the leg with its arrows at right angles to it,
which is the standard convention for a wind or pressure load. Read instead as a
vertical load per metre of horizontal projection it would give
$10(4.5) = 45$ kN and a quite different corner moment; the perpendicular reading
is the one that makes the reactions come out as round numbers.
(c) Propped cantilever with an internal hinge
Beam (c): the internal hinge at 4 m releases the moment there, which is the fourth equation the four reaction components need.
Use the hinge to break the problem in two. The built-in end
supplies three components and the roller one, so four equations are needed and
the hinge supplies the fourth. Isolating everything to the right of the hinge at
$x = 4$ m and taking moments about the hinge,
$$R_{C}(8) = 16(2) + 20(4) + 16(8) + 20(12) = 480 \ \Rightarrow \
R_{C} = \boxed{60\ \text{kN}}$$
where the four terms are, in order, the remaining 4 m of the 4 kN/m load, the
20 kN at $x = 8$ m, the 2 kN/m load over 8 m, and the 20 kN at the right
tip.
Carry the hinge force back to the built-in end. Vertical
equilibrium of the same right-hand segment gives a hinge shear of
$72 - 60 = 12$ kN transmitted from the left. The left segment then carries its
own 16 kN of distributed load plus that 12 kN at its tip, so
$$V_{A} = 16 + 12 = \boxed{28\ \text{kN}}, \qquad
M_{A} = -\left[16(2) + 12(4)\right] = \boxed{-80\ \text{kN}\cdot\text{m}}$$
with $H_{A} = 0$ because no horizontal load is applied. The negative sign means
hogging — tension on the top face at the wall, as expected.
Shear diagram. $V$ starts at $+28$ kN and falls at
4 kN/m to $-4$ kN just left of $x = 8$ m, drops 20 kN to $-24$ kN, falls at
2 kN/m to $-32$ kN just left of the roller, jumps 60 kN to $+28$ kN, falls to
$+20$ kN at the right tip and is closed by the 20 kN tip load. Hence
$$V_{\max}^{+} = +28\ \text{kN}, \qquad V_{\max}^{-} = -32\ \text{kN}$$
Shear passes through zero at $x = 7$ m.
Bending moment diagram. Integrating,
$M = 28x - 80 - 2x^{2}$ over the first 8 m. It rises from
$-80\ \text{kN}\cdot\text{m}$ at the wall through exactly zero at the hinge
— the check that the hinge has been located correctly — to a maximum
of $+18\ \text{kN}\cdot\text{m}$ at $x = 7$ m, then falls to
$-96\ \text{kN}\cdot\text{m}$ over the roller and closes to zero at the
loaded right tip:
$$M_{\max}^{+} = \boxed{+18\ \text{kN}\cdot\text{m}}, \qquad
M_{\max}^{-} = \boxed{-96\ \text{kN}\cdot\text{m}}$$
The segments are positive (sagging) between the hinge and roughly $x = 10$ m and
negative (hogging) elsewhere.
Question 2 — reactions and extreme diagram ordinates
Part
Reactions
Shear extremes
Moment extremes
(a)
pin 67 kN, roller 65 kN
$+32$ / $-36$ kN
$+4.06$ / $-64\ \text{kN}\cdot\text{m}$
(b)
pin 60 kN horiz., 30 kN vert.; roller 90 kN
$+66$ / $-70$ kN
$+217.8$ / $-20\ \text{kN}\cdot\text{m}$
(c)
fixed end 28 kN and $80\ \text{kN}\cdot\text{m}$;
roller 60 kN