Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations,
May 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 4, ONE of Questions 5
or 6, and ONE of Questions 7 or 8. Marks are shown in the left margin
(7 + 18 + 15 + 18 + 20 + 22 = 100). All eight questions are solved below,
because the alternatives test different topics and the whole 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, virtual work),
Ch. 11–12 (slope-deflection, 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, 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 a pure analysis paper, so no code clause is needed
to answer it, but every result below is in the SI units those documents use.
Sign conventions used throughout. For a beam, or for one
member of a frame, shear is positive when the resultant of the forces on 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. Truss forces are quoted as
T for tension and C for compression. In every figure applied
loads are red, reactions are blue, and an internal hinge is a red circle.
Given. A gabled frame with unequal legs and unequal
rafter slopes, pinned at both feet and hinged at the crown. Taking the level of
the right-hand support as the datum and the line of the left column as
$x = 0$:
Question 7 — node coordinates and loading
Node
Coordinates (m)
Comment
①
$(0,\ 3)$
pin support, 3 m above the datum
②
$(0,\ 6)$
head of the 3 m left column
③
$(4,\ 9)$
crown, internal hinge
④
$(10,\ 4.5)$
head of the 4.5 m right column
⑤
$(10,\ 0)$
pin support
The rafters carry 10 kN/m over their horizontal projection, that is over the
full 10 m span, giving a total of 100 kN.
Find. All four reaction components, and shear, axial force
and bending moment diagrams for each of the four members with the maximum and
minimum ordinates labelled.
Question 7 — the three-hinged gabled frame. Pins at 1 and 5 and the crown hinge at 3 give four reaction components against three equilibrium equations plus one condition equation, so the frame is determinate. Reactions shown in blue.
Approach. Four unknown reactions are resolved by the
three global equilibrium equations plus the condition that the bending moment
vanishes at the crown hinge, then the internal forces follow by cutting each
member and resolving the running resultant along and normal to it.
Global moment equation. Taking moments about the left pin
①, the 100 kN resultant acts at $x = 5$ m and the right reaction acts
10 m to the right and 3 m below:
$$-500 + 10\,V_{B} + 3\,H_{B} = 0$$
where $V_{B}$ is positive upward and $H_{B}$ positive to the right.
Condition at the crown. Moments about the hinge ③
for the right-hand portion only, which carries 60 kN of the load at $x = 7$ m
and is 6 m to the right of and 9 m below the crown:
$$-180 + 6\,V_{B} + 9\,H_{B} = 0$$
Solve the pair. Eliminating $V_{B}$,
$$7.2\,H_{B} = -120 \;\Rightarrow\;
H_{B} = \boxed{-16.67\ \text{kN, i.e. } 16.67\ \text{kN} \leftarrow}$$
$$V_{B} = 50 - 0.3(-16.67) = \boxed{55.0\ \text{kN} \uparrow}$$
and global equilibrium then gives $V_{A} = 45.0$ kN upward with
$H_{A} = +16.67$ kN, that is 16.67 kN to the right. Both horizontal reactions
point inward, which is the arch thrust one expects.
Check the left half. Moments about the crown for the left
portion, which carries 40 kN at $x = 2$ m:
$$80 - 4(45.0) + 6(16.67) = 80 - 180 + 100 = 0 \ \checkmark$$
Left column ①–②. It carries no load
along its length, so the axial force is 45.0 kN compression, the shear is a
constant 16.67 kN, and the moment grows linearly to
$$M_{2} = 16.67(3) = \boxed{50.0\ \text{kN}\cdot\text{m}}$$
at the knee ②, putting the outside face in tension.
Left rafter ②–③. Cutting at horizontal
station $x$ and taking moments of the left-hand forces,
$$M(x) = 5x^{2} - 32.5x + 50$$
which is $+50.0$ at ②, zero at $x = 2.5$ m and again at the crown, and
reaches its extreme where $dM/dx = 0$, at $x = 3.25$ m:
$$M_{\min} = 5(3.25)^{2} - 32.5(3.25) + 50 = -2.81\ \text{kN}\cdot\text{m}$$
Resolving the running resultant $(16.67,\ 45.0 - 10x)$ along the rafter unit
vector $(0.8,\,0.6)$ and its normal, the axial force falls from 40.3 kN to
16.3 kN compression and the shear from $+26.0$ kN to $-6.0$ kN, crossing zero
at the same $x = 3.25$ m.
Right rafter ③–④. The same construction
from the right-hand pin gives
$$M(x) = 5x^{2} - 57.5x + 150$$
zero at the crown and at $x = 7.5$ m, with
$$M_{\min} = -15.31\ \text{kN}\cdot\text{m} \text{ at } x = 5.75\ \text{m},
\qquad M_{4} = \boxed{+75.0\ \text{kN}\cdot\text{m}}$$
Its unit vector is $(0.8,\,-0.6)$, so the axial force runs from 10.3 kN to
46.3 kN compression and the shear from $+14.0$ kN to $-34.0$ kN.
Right column ④–⑤. Again unloaded along
its length: 55.0 kN compression, a constant 16.67 kN shear, and a moment that
grows from zero at the pin to $16.67(4.5) = 75.0$ kN·m at the knee
④, matching the rafter value and closing the solution.
Question 7 — bending moment along the frame, plotted against the horizontal projection. Positive ordinates put the outside face of the frame in tension. The two knee moments dominate; the rafters carry very little moment because the arch thrust cancels most of the gravity moment.
The result worth carrying away is how small the rafter moments are. A
simply supported 10 m beam under the same 10 kN/m would carry 125 kN·m
at mid-span; here the largest rafter moment is 15.3 kN·m, because the
16.67 kN horizontal thrust generated by the three-hinged geometry cancels most
of the gravity moment. What the frame pays for that is the pair of knee moments
and the horizontal reactions its foundations must resist.
Question 7 — reactions and governing ordinates
Member or point
Axial
Shear
Moment
Reaction at ①
45.0 kN up, 16.67 kN to the right
Reaction at ⑤
55.0 kN up, 16.67 kN to the left
Column ①–②
45.0 kN C
16.67 kN constant
0 to $+50.0$ kN·m
Rafter ②–③
40.3 → 16.3 kN C
$+26.0$ → $-6.0$ kN
$+50.0$; min $-2.81$ at $x = 3.25$ m; 0 at the crown
Rafter ③–④
10.3 → 46.3 kN C
$+14.0$ → $-34.0$ kN
0 at the crown; min $-15.31$ at $x = 5.75$ m; $+75.0$ at ④