Question 4 of 8: Member forces in two trusses by the method of sections
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations,
May 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 + 16 + 18 + 20 + 22 = 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. 3–4 (trusses; internal loadings),
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 (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 after which this exam code is
named; still the clearest source on influence lines for subdivided trusses.
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 inside face of a frame member
or the underside of a beam in tension. Truss forces are quoted as
T for tension and C for compression. Reactions are drawn in
blue and applied loads in red on every figure.
Question 4: Member forces in two trusses by the method of sections (18 marks)
24 m span in four 6 m panels; U1 and U3 8 m above the bottom chord over L2 and L4; apex U2 a further 4.5 m up, over L3
pin at L1, roller at L5
90 kN at L2, 60 kN at L3, 30 kN at L4, all vertical
(b)
36 m span; horizontal top chord U1 to U6 at panel points 0, 6, 12, 20, 28 and 36 m; bottom joints L1 to L5 at heights 2, 10, 12, 6 and 0 m; the bottom chord is interrupted between L2 and L3
pinned at both L1 and L5
72 kN at U3 and U4, 90 kN at U5 and U6, all vertical
Find. Six named member forces, each with its sense stated as
tension or compression.
Truss (a) with the two section cuts used below. Cut 1-1 passes through U1U2, U1L3 and L2L3; cut 2-2 through U2U3, U3L3 and L3L4.
Approach. Take reactions from overall equilibrium, then pass
a section through no more than three unknown members and choose the moment
centre at the intersection of the two members that are not wanted, so each
unknown falls out of a single equation.
Part (a) — reactions. Moments about L1
for the whole truss give
$$R_{L5}(24) = 90(6) + 60(12) + 30(18) = 1800
\;\Rightarrow\; R_{L5} = 75.0\ \text{kN}\ (\uparrow)$$
$$R_{L1} = 180 - 75.0 = 105.0\ \text{kN}\ (\uparrow)$$
Force in L1L2, from joint L1.
Only the end rafter and the bottom chord meet at the pin, and the rafter rises
8 m in 6 m so its length is 10 m. Resolving vertically then horizontally,
$$105.0 + N_{L1U1}\left(\frac{8}{10}\right) = 0
\;\Rightarrow\; N_{L1U1} = -131.25\ \text{kN}$$
$$N_{L1L2} = -N_{L1U1}\left(\frac{6}{10}\right)
= \boxed{78.75\ \text{kN tension}}$$
Force in U1L3, from cut 1-1. Cutting
between L2 and L3 severs U1U2,
U1L3 and L2L3. Taking moments about
L3, through which both U1L3 and
L2L3 pass, isolates the top chord. The member
U1U2 rises 4.5 m in 6 m, length 7.5 m, and its
perpendicular distance from L3 is 10 m, so for the left-hand piece
$$-105.0(12) + 90(6) - 10\,N_{U1U2} = 0
\;\Rightarrow\; N_{U1U2} = -\frac{1260 - 540}{10} = -72.0\ \text{kN}$$
Vertical equilibrium of the same piece then releases the diagonal:
$$105.0 - 90 + \left(\frac{4.5}{7.5}\right)(-72.0)
- \left(\frac{8}{10}\right)N_{U1L3} = 0$$
$$N_{U1L3} = \frac{15.0 - 43.2}{0.8} = \boxed{-35.25\ \text{kN, i.e. }
35.25\ \text{kN compression}}$$
Force in U2U3, from cut 2-2. Cutting
between L3 and L4 and working with the right-hand piece,
moments about L3 again eliminate the diagonal and the bottom chord:
$$-30(6) + 75.0(12) + 10\,N_{U2U3} = 0
\;\Rightarrow\; N_{U2U3} = -\frac{900 - 180}{10}
= \boxed{-72.0\ \text{kN, i.e. } 72.0\ \text{kN compression}}$$
That the two top-chord panels carry the same force is a coincidence of this
particular load pattern, not a symmetry: the loads are 90, 60 and 30 kN and the
truss is not symmetrically loaded. It is nonetheless a useful check, because
both were obtained from independent free bodies.
Part (b) — recognise why both supports can be pins.
Counting the second truss, there are 18 members, 11 joints and 4 reaction
components, so $m + r = 18 + 4 = 22 = 2j$: it is determinate. It can only be so
because the bottom chord is interrupted between L2 and
L3. That gap is the whole point of the arrangement — the truss
behaves as a two-pinned arch-like frame in which the horizontal thrust is
carried by the supports rather than by a tie.
The condition equation the gap provides. Pass a vertical
section anywhere between $x = 12$ m and $x = 20$ m. Because the bottom chord is
missing over that stretch, only two members are cut, U3U4
and U3L3, and both of them radiate from the joint
U3 at $(12,\ 18)$. Moments about U3 for the left-hand
piece therefore contain neither of them, nor the 72 kN load that sits at
U3 itself:
$$\sum M_{U3} = 0:\quad -12\,V_{L1} + 16\,H_{L1} = 0
\;\Rightarrow\; V_{L1} = \tfrac{4}{3}\,H_{L1}$$
which says that the reaction at L1 is directed along the line
L1–U3, a rise of 16 m in a run of 12 m.
Complete the reactions. Moments about L5 at
$(36,\ 0)$ for the whole truss, with L1 at $(0,\ 2)$, give
$$-36\,V_{L1} - 2\,H_{L1} + 72(24) + 72(16) + 90(8) + 90(0) = 0$$
$$-36\left(\tfrac{4}{3}H_{L1}\right) - 2H_{L1} + 3600 = 0
\;\Rightarrow\; 50\,H_{L1} = 3600$$
$$\begin{aligned} H_{L1} &= \boxed{72.0\ \text{kN} \rightarrow}, \\ V_{L1} &= \tfrac{4}{3}(72.0) = \boxed{96.0\ \text{kN} \uparrow} \end{aligned}$$
$$\begin{aligned} \sum F_x &= 0:\ H_{L5} = 72.0\ \text{kN} \leftarrow; \\ \sum F_y &= 0:\ V_{L5} = 324 - 96.0 = 228.0\ \text{kN} \uparrow \end{aligned}$$
The vertical components sum to 324 kN, matching the applied
72 + 72 + 90 + 90 kN, and the horizontal components are equal and opposite as
they must be.
Force in L2U3. Joints U1,
U2 and L1 carry no applied load, and L1,
L2 and U3 are collinear — each step is 6 m across and
8 m up — so L1L2U3 acts as one straight
strut 10 m per panel. Resolving horizontally at the pin L1,
$$72.0 + N\left(\frac{6}{10}\right) = 0 \;\Rightarrow\; N = -120.0\ \text{kN}$$
and vertical equilibrium at the same joint, $96.0 - 120.0(8/10) = 0$, confirms
it while proving that the end post U1L1 is unstressed.
Hence
$$N_{L2U3} = \boxed{120.0\ \text{kN compression}}$$
Force in L3L4. Cut between L3
and L4, severing U4U5,
L3U5 and L3L4, and work with the
right-hand piece. The first two meet at U5 $(28,\ 18)$, so moments
there leave only the bottom chord, whose perpendicular offset from U5
is 9.6 m:
$$90(8) - \left[228.0(8) - 72.0(18)\right] + 9.6\,N_{L3L4} = 0$$
$$720 - 528 + 9.6\,N_{L3L4} = 0 \;\Rightarrow\;
N_{L3L4} = \boxed{-20.0\ \text{kN, i.e. } 20.0\ \text{kN compression}}$$
Force in L3U5. From the same cut, the
top chord U4U5 lies on $y = 18$ and the bottom chord
L3L4 on the line through $(20,\ 12)$ falling 6 m in 8 m;
these intersect at $(12,\ 18)$, the joint U3. Taking moments about
that point for the right-hand piece, with the diagonal again 9.6 m off the
centre,
$$-90(16) - 90(24) + \left[228.0(24) - 72.0(18)\right] - 9.6\,N_{L3U5} = 0$$
$$-3600 + 4176 - 9.6\,N_{L3U5} = 0 \;\Rightarrow\;
N_{L3U5} = \boxed{60.0\ \text{kN tension}}$$
Both members run 8 m across and 6 m vertically, so each is 10 m long. Joint
L3 provides the check: the vertical U4L3
delivers 72 kN of compression from above, and the vertical components of the
three inclined members meeting there — 24.0 kN from
U3L3, 36.0 kN from L3U5 and 12.0 kN
from L3L4 — add to exactly 72 kN upward.
Truss (b). Both supports are pinned; the bottom chord stops at L2 and restarts at L3, which is what keeps a four-reaction structure statically determinate.