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 4: Member forces in two trusses (18 marks)
Given. A 16 m truss in four 4 m panels, 3 m deep, pinned at
L1 and on a roller at L5, carrying 36 kN downward at each
of L2 and L3. The web consists of the end diagonals
L1–U1 and U3–L5, the
verticals under each top joint, and the two inner diagonals
U1–L3 and L3–U3.
Find. The forces in U1–U2,
U1–L3 and L3–U3, with
their sense.
Figure 6 — truss 4(a). All
three required members are cut by a single vertical section between
L2 and L3, or between L3 and
L4.
Approach. Use the method of sections. Each of the three
members can be isolated by a vertical cut that severs exactly three members, and
each unknown then follows from one equation — a vertical resolution for a
diagonal, a moment about the joint where the other two meet for a chord.
Section between L2 and L3. This cut
severs U1–U2 (horizontal),
U1–L3 (a $4:3$ diagonal, so components $0.8$ and
$0.6$) and L2–L3 (horizontal). Only the diagonal has
a vertical component, so resolving vertically on the left-hand portion, which
carries $45 - 36 = 9$ kN of net upward force,
$$ 9 - 0.6\,N_{U_1L_3} = 0 \;\Rightarrow\;
\boxed{N_{U_1L_3} = +15.0\ \text{kN (tension)}} $$
Top chord from the same section. Take moments about
L3, through which both the diagonal and the bottom chord pass:
$$ 3\,N_{U_1U_2} + 45(8) - 36(4) = 0 \;\Rightarrow\;
\boxed{N_{U_1U_2} = -72.0\ \text{kN (compression)}} $$
The negative sign is expected — the top chord of a simply supported truss
is in compression.
Section between L3 and L4. Now the cut
severs U2–U3, L3–U3 and
L3–L4. The left-hand portion carries
$45 - 36 - 36 = -27$ kN net, so resolving vertically,
$$ -27 + 0.6\,N_{L_3U_3} = 0 \;\Rightarrow\;
\boxed{N_{L_3U_3} = +45.0\ \text{kN (tension)}} $$
Both inner diagonals rise towards mid-span from the loaded joint and both are in
tension, which is the expected behaviour of a truss whose diagonals slope
towards the nearer support.
(b) Roof truss with a horizontal load at the apex
Given. A symmetric roof truss of 16 m span in four 4 m
panels; the rafter rises 3 m over the first 8 m to the apex U1, so
the intermediate rafter joints M1 and M2 are 3 m above the
bottom chord and the apex 6 m. The truss is on a roller at L3 (the
centre joint) and pinned at L5. It carries 60 kN downward at
L1, 60 kN downward at L2, and 120 kN horizontally to the
right at the apex U1.
Find. The forces in L2–L3,
L3–L4 and M1–L3.
Figure 7 — truss 4(b). The
supports are inboard: a roller under the centre joint L3 and a pin at
L5, so the whole left-hand half acts as an overhang.
Approach. Find the reactions first — the unusual
support arrangement makes them large and of opposite sense — then take a
section, and finally isolate joint L3 for the sub-strut.
Horizontal equilibrium. The only horizontal restraint is the
pin, so
$$ \boxed{H_{L_5} = 120\ \text{kN acting to the left}} $$
Moments about L5. With the roller 8 m to the left
of the pin, the two 60 kN loads 16 m and 12 m to the left, and the 120 kN load
acting 6 m above the chord,
$$ 8\,V_{L_3} = 60(16) + 60(12) - 120(6) = 960 + 720 - 720 = 960 $$
so that
$$ \boxed{V_{L_3} = 120.0\ \text{kN}\ (\uparrow)} $$
and vertical equilibrium then gives
$V_{L_5} = 120 - 120 = \boxed{0}$: the pin carries no vertical force at all, a
result worth quoting because it is the clearest check available on the
arithmetic.
Section just left of L3. Cut
M1–U1, M1–L3 and
L2–L3 and keep the left-hand portion, which carries
the two 60 kN loads. Taking moments about the point where the rafter and the
sub-strut meet, that is M1 at $(4, 3)$,
$$ 3\,N_{L_2L_3} + 60(4) = 0 \;\Rightarrow\;
\boxed{N_{L_2L_3} = -80.0\ \text{kN (compression)}} $$
The bottom chord of the overhanging half is in compression, the reverse of the
usual simply supported case, because that half hangs from the truss rather than
spanning between supports.
Bottom chord to the right of the support. Take a section
between L3 and L4 and keep the right-hand portion, which
carries only the pin reaction. Moments about M2 at $(12, 3)$ give
$$ 3\,N_{L_3L_4} + 120(3) = 0 \;\Rightarrow\;
\boxed{N_{L_3L_4} = -120.0\ \text{kN (compression)}} $$
the horizontal reaction being the only force involved.
Joint L3 for the sub-strut. Four members meet at
L3: the two bottom chords, the vertical U1–L3
and the sub-strut M1–L3, which runs from $(4,3)$ to
$(8,0)$ and so has direction cosines $0.8$ and $0.6$. (The mirror member
M2–L3 is a zero-force member here, because the whole
right-hand half of the truss is unloaded apart from the pin reaction.)
Horizontal equilibrium at L3 reads
$$ N_{L_3L_4} - N_{L_2L_3} - 0.8\,N_{M_1L_3} = 0 $$
$$ -120 - (-80) - 0.8\,N_{M_1L_3} = 0 \;\Rightarrow\;
\boxed{N_{M_1L_3} = -50.0\ \text{kN (compression)}} $$
Vertical equilibrium at the same joint then returns
$N_{U_1L_3} = -90$ kN, and the roller reaction of 120 kN closes the joint
exactly — $0.6(50) + 90 = 120$ — which is the check that the
sub-strut force is right.
Question 4 — member forces
Truss
Member
Force
Sense
(a)
U1–U2
72.0 kN
Compression
U1–L3
15.0 kN
Tension
L3–U3
45.0 kN
Tension
(b)
L2–L3
80.0 kN
Compression
L3–L4
120.0 kN
Compression
M1–L3
50.0 kN
Compression
Reactions used above: truss (a), 45.0 kN and 27.0 kN upward at L1
and L5; truss (b), 120.0 kN upward at the roller L3, and
at the pin L5 120 kN horizontally to the left with no vertical
component.