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. Bottom-chord joints at 3 m + 6 m + 6 m + 3 m
centres, so L1 at x = 0, L2 at 3 m, L3 at 9 m,
L4 at 15 m and L5 at 18 m, all at the same level.
Given data, truss 4(a)
Quantity
Value
Top-chord joints
U1 (3 m, 4 m), U2 (9 m, 6.5 m), U3 (15 m, 4 m)
Supports
pin at L1, roller at L5
Applied loads
36 kN at U1, 36 kN at U2, 24 kN at U3, all vertical
Web members
verticals U1-L2, U2-L3, U3-L4; diagonals U1-L3 and L3-U3
Count
m = 13, j = 8, r = 3; m + r = 2j = 16, determinate
Find. The forces in L2-L3,
U1-U2 and L3-U3, each stated as
tension or compression.
Truss 4(a): geometry, panel loads and support reactions.
Approach. All three requested members can be reached by the
method of sections, because a single vertical cut just left of L3
severs U1-U2, U1-L3 and
L2-L3, and a second cut just right of L3
severs U2-U3, L3-U3 and
L3-L4; taking moments about the joint where two of the
three cut members meet isolates the third.
Find the reactions. Moments about the pin at
L1, with the loads at x = 3, 9 and 15 m:
$$18 R_{L5} = (36)(3) + (36)(9) + (24)(15) = 108 + 324 + 360 = 792$$
$$R_{L5} = \boxed{44\ \text{kN} \uparrow}, \qquad R_{L1} = 96 - 44 = \boxed{52\ \text{kN} \uparrow}$$
The horizontal reaction at the pin is zero, all loading being vertical.
Cut just left of L3 and take moments about
U1. The left free body contains L1,
L2 and U1. Both U1-U2 and
U1-L3 pass through U1, as does the 36 kN load
applied there, so only the reaction and the bottom chord survive. With
U1 at (3 m, 4 m),
$$\sum M_{U1} = 0: \quad 4\,F_{L2L3} = (52)(3) = 156$$
$$F_{L2L3} = \boxed{+39.0\ \text{kN (T)}}$$
Cut just right of L3 and take moments about
L3. The right free body contains U3,
L4 and L5. Both L3-U3 and
L3-L4 pass through L3, leaving only
U2-U3. Its direction cosine set is
$(-6,\ 2.5)/6.5$ and it acts at U3 (15 m, 4 m), so the moment arm
about L3 (9 m, 0) works out to 6.0 m and
$$6.0\,F_{U2U3} - (24)(6) + (44)(9) = 0$$
$$F_{U2U3} = -42.0\ \text{kN}$$
Convert that to the requested chord. The top chord is
symmetric in geometry but not in loading, so U1-U2 must
be found on its own. Cutting just left of L3 and taking moments about
L3 removes both L2-L3 and
U1-L3 and leaves
$$F_{U1U2} = \boxed{-42.0\ \text{kN}} \equiv 42.0\ \text{kN (C)}$$
The equality of the two top-chord panels either side of the apex is a
consequence of the geometry, not an assumption.
Return to the right-hand free body for the diagonal. With
$F_{U2U3} = -42.0$ kN known, vertical equilibrium of that free body gives
$$-24 + 44 + (-42.0)\left(\frac{2.5}{6.5}\right)
+ F_{L3U3}\left(\frac{-4}{\sqrt{52}}\right) = 0$$
$$F_{L3U3} = \boxed{+6.93\ \text{kN (T)}}$$
(b) Stepped truss on two pinned supports
Given. A stepped truss with joints at
L1 (0, 0), B1 (6 m, 0), U1 (0, 4.5 m),
L2 (6 m, 4.5 m), U2 (6 m, 9 m), L3 (12 m, 9 m),
U3 (12 m, 13.5 m) and L4 (18 m, 9 m). Both
L1 and B1 are drawn as pins. Applied loads are 30 kN at
U1, 60 kN at U2, 60 kN at U3 and 30 kN at
L4, all vertical, totalling 180 kN.
Check: the horizontal line drawn
between L1 and B1 at ground level is a dimension witness
line, not a member — it touches neither joint circle. Reading it as a
bottom chord would give m + r = 17 against 2j = 16 and make the truss
indeterminate, which is not answerable by statics in the marks available. With
no member there, joint B1 carries the single vertical
B1-L2, so its pin can develop no horizontal force and the
two pins between them still leave the truss exactly determinate.
Find. The forces in U1-U2,
L2-L3 and U2-L2, each stated as
tension or compression.
Truss 4(b): geometry, panel loads and the two pinned supports. The long chords L1-L2-L3 and U1-U2-U3 are each straight lines of slope 4.5 : 6.
Approach. Take moments about B1 for the whole
truss to get the hold-down reaction at L1, then walk the joints
outward from L1, which carries only two members and is therefore the
natural starting point.
Reactions from global equilibrium. Both pins sit on the
line y = 0, so their horizontal components have no moment about a point on that
line. Taking moments about B1 (6 m, 0),
$$-6 V_{L1} + (30)(0 - 6) + (60)(6 - 6) + (60)(12 - 6) + (30)(18 - 6) = 0$$
Working through, $-6 V_{L1} = -540$ is wrong by sign inspection; carrying the
downward loads as negative gives $-6 V_{L1} - 540 = 0$ and hence
$$V_{L1} = \boxed{90\ \text{kN downward}}, \qquad V_{B1} = 180 + 90 = \boxed{270\ \text{kN} \uparrow}$$
L1 is a hold-down: the truss cantilevers a long way to the right of
B1, so the left support has to pull the structure down rather than
hold it up.
Confirm that neither pin carries horizontal force.
B1 is attached by the single vertical member
B1-L2, so horizontal equilibrium at that joint gives
$H_{B1} = 0$; global horizontal equilibrium then gives $H_{L1} = 0$ as well.
This is the practical consequence of the witness-line reading flagged
above.
Joint L1. Two members meet here: the vertical
L1-U1 and the diagonal L1-L2, whose
direction cosines are $(0.8,\ 0.6)$. Horizontal equilibrium gives
$$0.8\,F_{L1L2} = 0 \quad\Rightarrow\quad F_{L1L2} = 0$$
and vertical equilibrium then gives
$F_{L1U1} = 90\ \text{kN (T)}$ — the vertical hangs the whole hold-down
force.
Joint U1 gives the first requested member.
Meeting here are U1-L1 (carrying 90 kN tension, pulling
U1 downward), the horizontal U1-L2, the
diagonal U1-U2 with cosines $(0.8,\ 0.6)$, and the 30 kN
load. Vertically,
$$-90 + 0.6\,F_{U1U2} - 30 = 0$$
$$F_{U1U2} = \boxed{+200\ \text{kN (T)}}$$
and horizontally $F_{U1L2} = -0.8(200) = -160\ \text{kN}$, i.e. 160 kN
compression.
Joint L2 gives the other two. Five members meet
at L2: L1-L2 (zero), L2-L3
along $(0.8,\ 0.6)$, U1-L2 (−160 kN),
B1-L2 vertical and L2-U2 vertical.
The vertical from B1 carries the whole 270 kN reaction in
compression, and resolving the joint gives
$$F_{L2L3} = \boxed{-200\ \text{kN}} \equiv 200\ \text{kN (C)}$$
$$F_{L2U2} = \boxed{-150\ \text{kN}} \equiv 150\ \text{kN (C)}$$
Question 4 — requested member forces
Truss
Member
Force
Sense
(a)
L2-L3
39.0 kN
Tension
U1-U2
42.0 kN
Compression
L3-U3
6.93 kN
Tension
(b)
U1-U2
200 kN
Tension
L2-L3
200 kN
Compression
U2-L2
150 kN
Compression
The reactions are RL1 = 52 kN and RL5 = 44 kN for
truss (a), and VL1 = 90 kN downward with VB1 = 270 kN
upward for truss (b).