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07-Str-A1 · December 2016

Question 4 of 8: Truss Member Forces

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.

Reference texts.

Question 4: Truss Member Forces (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

(a) Symmetrically supported roof truss

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)
QuantityValue
Top-chord jointsU1 (3 m, 4 m), U2 (9 m, 6.5 m), U3 (15 m, 4 m)
Supportspin at L1, roller at L5
Applied loads36 kN at U1, 36 kN at U2, 24 kN at U3, all vertical
Web membersverticals U1-L2, U2-L3, U3-L4; diagonals U1-L3 and L3-U3
Countm = 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.

36 kN36 kN24 kNL1L2L3L4L5U1U2U33 m6 m6 m3 m2.5 m4 mR = 52 kNR = 44 kN
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.

  1. 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.
  2. 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), $$\sum M_{U1} = 0: \quad 4\,F_{L2L3} = (52)(3) = 156$$ $$F_{L2L3} = \boxed{+39.0\ \text{kN (T)}}$$
  3. 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 $$6.0\,F_{U2U3} - (24)(6) + (44)(9) = 0$$ $$F_{U2U3} = -42.0\ \text{kN}$$
  4. 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.
  5. 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.

30 kN60 kN60 kN30 kNL1B1U1L2U2L3U3L46 m6 m6 m4.5 m4.5 m4.5 mR = 90 kN downR = 270 kN up
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.

  1. 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.
  2. 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.
  3. 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.
  4. 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.
  5. 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
TrussMemberForceSense
(a)L2-L339.0 kNTension
U1-U242.0 kNCompression
L3-U36.93 kNTension
(b)U1-U2200 kNTension
L2-L3200 kNCompression
U2-L2150 kNCompression

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).