Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 07-Str-A1 Elementary Structural Analysis,
National Examinations, May 2017. Three hours, CLOSED BOOK (an approved Sharp or
Casio calculator is permitted). Page 1 states that six questions
constitute a complete paper: Questions 1–5 are compulsory and the candidate
answers one only of Questions 6, 7 or 8. All eight questions are worked
below.
Sign conventions used throughout. Sagging bending moment is
positive and is plotted above the axis; shear is the sum of the upward forces on
the portion to the left of the section. Truss member forces are quoted as
T for tension and C for compression. In the slope-deflection
work of Question 7 the member-end moments follow the usual convention —
clockwise on the member end taken as positive — so the sagging moment is
$+M_{ij}$ at the left end of a member and $-M_{ji}$ at its right end. For the
bent members of Questions 2(c) the diagrams are developed: the abscissa
is distance measured along the member axis, not the horizontal projection.
4(a) Three-panel truss with a single panel-point load
Given. Bottom chord $L_1L_2L_3L_4$ at 8 m centres (span
24 m), top chord $U_1U_2U_3$ at 3 m above it with $U_1$ 4 m in from $L_1$ and the
top panels also 8 m. Pin at $L_1$, roller at $L_4$. A single downward load of
90 kN acts at $L_3$. Every web member spans 4 m horizontally and 3 m vertically,
so each is exactly 5 m long — a 3–4–5 triangle.
Find. The forces in $L_2L_3$, $U_2L_3$ and $U_3L_3$,
each with its sense.
4(a): geometry, support conditions and the 90 kN panel load. The section used below cuts $U_2U_3$, $U_2L_3$ and $L_2L_3$.
Approach. Reactions by global moments, then one vertical
section between $U_2$ and $L_3$ (which severs exactly three members) for the
first two forces, and joint equilibrium at $L_3$ for the third.
Determinacy and reactions. Eleven members, seven joints,
three reaction components: $m + r = 14 = 2j$, determinate. Taking moments about
$L_1$ with the load 16 m along the 24 m span,
$$R_{L_4} = \frac{90(16)}{24} = \boxed{60.0\ \text{kN}\ \uparrow},\qquad
R_{L_1} = 90 - 60 = \boxed{30.0\ \text{kN}\ \uparrow}$$
Section for $L_2L_3$ — moments about $U_2$. Cut
vertically between $U_2\,(12,3)$ and $L_3\,(16,0)$; the cut severs $U_2U_3$,
$U_2L_3$ and $L_2L_3$. The first two both pass through $U_2$, so taking moments
there for the left-hand portion leaves only the bottom chord, whose lever arm is
the truss depth:
$$\sum M_{U_2} = 0:\qquad 30.0(12) = F_{L_2L_3}(3)$$
$$F_{L_2L_3} = \frac{360}{3} = \boxed{120.0\ \text{kN\ (T)}}$$
The bottom chord of a simply supported truss under gravity load is in tension,
as expected.
Same section for $U_2L_3$ — vertical equilibrium.
Both chords cut by this section are horizontal, so only the diagonal has a
vertical component. With the diagonal running $(4,-3)$ from $U_2$ to $L_3$, its
vertical direction cosine is $3/5$:
$$\sum F_y = 0:\qquad 30.0 - \tfrac{3}{5}F_{U_2L_3} = 0$$
$$F_{U_2L_3} = \tfrac{5}{3}(30.0) = \boxed{50.0\ \text{kN\ (T)}}$$
Joint $L_3$ for $U_3L_3$. Four members meet at $L_3$: the
two horizontal chords, the diagonal down from $U_2$ and the diagonal up to
$U_3\,(20,3)$. The chords are horizontal, so vertical equilibrium of the joint
involves only the two diagonals and the 90 kN load:
$$\tfrac{3}{5}(50.0) + \tfrac{3}{5}F_{L_3U_3} = 90.0$$
$$F_{L_3U_3} = \frac{90.0 - 30.0}{0.6} = \boxed{100.0\ \text{kN\ (T)}}$$
Check by horizontal equilibrium at $L_3$. With
$F_{L_2L_3} = 120.0$ T,
$$-120.0 + F_{L_3L_4} - \tfrac{4}{5}(50.0) + \tfrac{4}{5}(100.0) = 0
\;\Rightarrow\; F_{L_3L_4} = 80.0\ \text{kN (T)}$$
and a section on the right-hand side, taking moments about $U_3$, gives
$60.0(4) = 3F_{L_3L_4}$, i.e. $80.0$ kN as well. The two independent routes agree,
so the three requested values stand.
Member
Force
Sense
$L_2-L_3$
120.0 kN
Tension
$U_2-L_3$
50.0 kN
Tension
$U_3-L_3$
100.0 kN
Tension
(check) $L_3-L_4$
80.0 kN
Tension
(check) $U_2-U_3$
160.0 kN
Compression
Reactions
$R_{L_1}=30.0$ kN, $R_{L_4}=60.0$ kN
both ↑
4(b) Cantilevered truss pinned to a wall
Given. Joints $U_1(0,6)$, $U_2(4,6)$, $U_3(8,6)$,
$L_1(0,0)$ and $L_2(4,3)$, dimensions in metres. Members: the top chord
$U_1U_2$ and $U_2U_3$, the vertical $U_2L_2$, the diagonal $U_1L_2$, and the
straight run $L_1L_2U_3$ (which is collinear, slope $3{:}4$, so it counts as the
two members $L_1L_2$ and $L_2U_3$). Both $U_1$ and $L_1$ bear on the wall.
Loads: 90 kN down at $U_2$, 90 kN down at $U_3$ and 40 kN to the right at
$U_3$.
Find. The forces in $U_1L_2$, $U_1U_2$ and $L_1L_2$.
4(b): the wall-supported truss. $L_1$, $L_2$ and $U_3$ are collinear on a 3:4 slope, so the long line is two members, not one.
Approach. Start at the joint that carries only two unknown
member forces — $U_3$ — and walk inward: $U_3 \to U_2 \to L_2$, which
delivers all three answers without ever needing the reactions.
Determinacy. Six members, five joints and four reaction
components (both wall bearings are pins):
$m + r = 6 + 4 = 10 = 2j$, determinate. The truss is a cantilever hung off two
wall pins, which is why four reaction components do not make it indeterminate.
Joint $U_3$ — vertical equilibrium. Two members meet
at $U_3$: the horizontal $U_2U_3$ and the inclined $L_2U_3$, the latter running
$(-4,-3)$ from $U_3$ toward $L_2$. With 90 kN down applied there,
$$-\tfrac{3}{5}F_{U_3L_2} - 90.0 = 0 \;\Rightarrow\;
F_{U_3L_2} = -150.0 \quad \text{i.e. } 150.0\ \text{kN (C)}$$
Joint $U_2$. Three members meet here: the two horizontal
chord members and the vertical $U_2L_2$, with 90 kN applied down. Vertically,
$$-F_{U_2L_2} - 90.0 = 0 \;\Rightarrow\; F_{U_2L_2} = 90.0\ \text{kN (C)}$$
and horizontally the two chord members must balance, so
$$F_{U_1U_2} = F_{U_2U_3} = \boxed{160.0\ \text{kN\ (T)}}$$
Joint $L_2$ — two equations, two unknowns. Four
members meet at $L_2\,(4,3)$: $L_2L_1$ in direction $(-4,-3)/5$, $L_2U_1$ in
$(-4,3)/5$, $L_2U_2$ vertically up, and $L_2U_3$ in $(4,3)/5$. There is no load
at $L_2$. Horizontal equilibrium gives
$$-F_{L_2L_1} - F_{L_2U_1} + F_{L_2U_3} = 0
\;\Rightarrow\; F_{L_2L_1} + F_{L_2U_1} = -150.0$$
and vertical equilibrium, after substituting
$F_{L_2U_2} = -90.0$ and $F_{L_2U_3} = -150.0$, gives
$$-F_{L_2L_1} + F_{L_2U_1} = 300.0$$
Solve the pair. Adding and subtracting,
$$F_{U_1L_2} = \frac{-150.0 + 300.0}{2} = \boxed{75.0\ \text{kN\ (T)}}, \qquad
F_{L_1L_2} = -225.0 \;\Rightarrow\; \boxed{225.0\ \text{kN\ (C)}}$$
The long collinear run is therefore in compression next to the wall (225 kN) and
in compression again beyond $L_2$ (150 kN) — the step between them is the
90 kN the vertical brings down.
Reaction check. Resolving the member forces at the two wall
pins gives $L_1: (180.0, 135.0)$ kN and $U_1: (-220.0, 45.0)$ kN. Globally
$\sum F_y = 135.0 + 45.0 = 180.0$ kN, matching the two 90 kN loads, and
$\sum F_x = 180.0 - 220.0 + 40.0 = 0$. Equilibrium closes.
Member
Force
Sense
$U_1-L_2$
75.0 kN
Tension
$U_1-U_2$
160.0 kN
Tension
$L_1-L_2$
225.0 kN
Compression
(check) $U_2-L_2$
90.0 kN
Compression
(check) $L_2-U_3$
150.0 kN
Compression
Check: the two wall bearings in 4(b)
are read as pins. The alternative reading — a horizontal link at $U_1$, a
pin at $L_1$ and a vertical member $U_1L_1$ — is also determinate, and it
returns identical forces in all three requested members (75.0 T,
160.0 T and 225.0 C), with the added member carrying 45.0 kN compression. The
answers above are therefore insensitive to which reading is taken. What is not
tenable is a link at $U_1$ without the vertical member: that leaves
$m+r = 9 < 2j = 10$ and the truss is a mechanism.