Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Professional Examinations — 07-Str-A1
Elementary Structural Analysis; 3 hours, CLOSED BOOK (an approved Casio or Sharp
calculator is permitted). The paper carries eight questions: answer all of
Questions 1–5 (6, 24, 16, 16 and 6 + 10 marks) and one only of
Questions 6, 7 or 8 (22 marks each), for 100 marks. All three optional questions are
worked below, because the complete set is the more useful study resource.
Reference texts. R. C. Hibbeler, Structural Analysis
(Ch. 2 determinacy and stability; Ch. 4 shear and moment diagrams; Ch. 6
influence lines; Ch. 8–9 virtual work; Ch. 11 slope deflection);
A. Kassimali, Structural Analysis (Ch. 3, 5, 8, 13, 16); K. Leet, C.-M. Uang
and A. Gilbert, Fundamentals of Structural Analysis; J. C. McCormac,
Structural Analysis: Using Classical and Matrix Methods. For Canadian practice the
companion documents are the National Building Code of Canada (Part 4, load
combinations) and CSA S16 Design of Steel Structures; this paper is pure
analysis, so no design code is invoked in the answers below.
Check
Three figure readings are stated here once and used throughout. (1) In
Question 2(b) the two hatched load blocks are drawn from the left end of the beam to
the first roller and from the second-last roller to the right end — that is,
0 to 7 m and 13 to 20 m, not merely over the bays named by
the dimension string. (2) In Question 2(c) the upper 20 kN acts leftwards at the
top of the 1 m riser and the lower 20 kN acts rightwards at its foot, so the
applied action is a pure couple and the roller reaction is a hold-down. (3) In
Question 6 the 5 kN/m ruling spans the full 16 m width of the sketch, so it
is a load on the horizontal projection covering both overhangs and the inclined
member. Each reading is the one that makes the arithmetic close on round numbers, which is
the usual confirmation on this paper.
Question 3: Member forces in a Pratt truss (16 marks)
Given. A parallel-chord truss of five 4 m panels, span
20 m, depth 3 m. The bottom chord runs
L1…L6 at 4 m centres; the top chord carries four joints
U1…U4 sitting directly over L2, L3,
L4 and L5. The web has a vertical under every top joint, rising
diagonals in the first three panels (L1U1, L2U2,
L3U3) and falling diagonals in the last two
(U3L5, U4L6). Three 30 kN downward loads
hang at L2, L3 and L4. L1 is a pin and
L6 a roller.
Find. The axial forces in L1U1,
L2L3, L2U2 and L2U1,
each labelled tension or compression.
Question 3 — the truss with its reactions and the four requested member forces. Every panel diagonal is a 3-4-5 triangle, so its direction cosines are 0.8 and 0.6 exactly.
Approach. Confirm determinacy, take the reactions from global
statics, then walk joints L1, U1 and L2 in that order,
because each of them adds only two new unknowns; finally re-derive the bottom chord by a
section cut as an independent check.
Check determinacy and note the geometry. The truss has $m = 17$
members, $j = 10$ joints and $r = 3$ restraint components, so
$$m + r = 20 = 2j$$
and it is statically determinate. Every diagonal spans one 4 m panel over the 3 m
depth, so its length is $\sqrt{4^{2}+3^{2}} = 5$ m exactly and its direction cosines are
$4/5 = 0.8$ horizontally and $3/5 = 0.6$ vertically. That exactness is why the answers
come out as integers.
Reactions from global statics. Taking moments about the pin,
$$\sum M_{L_1} = 0:\qquad 30(4) + 30(8) + 30(12) = 20\,R_{L_6}$$
$$R_{L_6} = \frac{720}{20} = 36\ \text{kN},\qquad R_{L_1} = 90 - 36 = 54\ \text{kN}$$
both upward, and there is no horizontal reaction because there is no horizontal load.
Joint L1 gives the end diagonal. Only two members meet the
pin: the horizontal chord L1L2 and the diagonal
L1U1. Vertical equilibrium involves the diagonal alone,
$$\sum F_y = 0:\qquad 54 + 0.6\,F_{L_1U_1} = 0 \quad\Rightarrow\quad
F_{L_1U_1} = -\frac{54}{0.6} = -90\ \text{kN}$$
$$\boxed{F_{L_1U_1} = 90\ \text{kN compression}}$$
The negative sign means the bar pushes on the joint, which is what an end diagonal rising
away from a support must do. Horizontal equilibrium then gives the first bottom chord,
$F_{L_1L_2} = -0.8(-90) = +72$ kN tension.
Joint U1 gives the vertical. Three members meet there: the
diagonal just found, the vertical down to L2 and the top chord to
U2. The top chord is horizontal, so the vertical equation contains only two
terms,
$$\sum F_y = 0:\qquad 0.6(90) - F_{U_1L_2} = 0$$
$$\boxed{F_{L_2U_1} = 54\ \text{kN tension}}$$
— the vertical simply hangs the whole pin reaction down onto the loaded bottom joint.
Horizontal equilibrium at the same joint returns $F_{U_1U_2} = -72$ kN, i.e. 72 kN
compression in the first top chord.
Joint L2 gives the second diagonal. Four members meet
L2 — the two bottom chords, the vertical (now known) and the rising
diagonal to U2 — and a 30 kN load hangs there. Vertically,
$$\sum F_y = 0:\qquad 54 + 0.6\,F_{L_2U_2} - 30 = 0 \quad\Rightarrow\quad
F_{L_2U_2} = -\frac{24}{0.6} = -40\ \text{kN}$$
$$\boxed{F_{L_2U_2} = 40\ \text{kN compression}}$$
Notice the pattern: a rising diagonal carries the net shear left of its panel
divided by 0.6, and the shear has dropped from 54 to 24 kN across the first
loaded joint.
Horizontal equilibrium at L2 gives the requested chord.
With the diagonal settled,
$$\sum F_x = 0:\qquad -72 + F_{L_2L_3} + 0.8(-40) = 0$$
$$\boxed{F_{L_2L_3} = 104\ \text{kN tension}}$$
as a bottom chord in a simply supported truss must be.
Check the chord independently by a section cut. Cut vertically through
the second panel, severing U1U2, L2U2 and
L2L3, and take moments about U2 for the left-hand piece.
The two cut members that pass through U2 drop out, leaving one equation in one
unknown:
$$\sum M_{U_2} = 0:\qquad -54(8) + 30(4) + 3\,F_{L_2L_3} = 0
\quad\Rightarrow\quad F_{L_2L_3} = \frac{432 - 120}{3} = 104\ \text{kN}$$
which reproduces the joint-walk value exactly. Summing vertical forces on the same free
body returns $0.6\,F_{L_2U_2} = -(54 - 30)$, i.e. $-40$ kN, confirming the diagonal
too.