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07-Str-A1 · May 2015

Question 4 of 8: Member forces in two trusses

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Examinations, May 2015 — 07-Str-A1 Elementary Structural Analysis. Three hours, CLOSED BOOK, an approved Sharp or Casio calculator permitted. Six questions constitute a complete paper: 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 exercise quite different methods — slope-deflection, virtual work and the statics of a three-hinged frame — and the complete set is the more useful study resource.

Reference texts.

Check: every support type, hinge and member below was read off the drawings, not off the printed text. In this subject the text carries almost no data: spans, loads, support types and hinge positions exist only in the hand-drawn figures. The classification in Question 1 in particular turns entirely on telling a pin (plain triangle on hatching) from a roller (triangle over two rollers) and a rigid joint from an internal hinge (small open circle).

Question 4: Member forces in two trusses (18 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) Parallel-chord truss, 4 m panels

Given. A 16 m truss in four 4 m panels, 3 m deep, pinned at L1 and on a roller at L5, carrying 36 kN downward at each of L2 and L3. The web consists of the end diagonals L1–U1 and U3–L5, the verticals under each top joint, and the two inner diagonals U1–L3 and L3–U3.

Find. The forces in U1–U2, U1–L3 and L3–U3, with their sense.

L1L2L3L4L5U1U2U336 kN36 kN4 m4 m4 m4 m3 m
Figure 6 — truss 4(a). All three required members are cut by a single vertical section between L2 and L3, or between L3 and L4.

Approach. Use the method of sections. Each of the three members can be isolated by a vertical cut that severs exactly three members, and each unknown then follows from one equation — a vertical resolution for a diagonal, a moment about the joint where the other two meet for a chord.

  1. Reactions. Taking moments about L5, $$ 16\,R_{L_1} = 36(12) + 36(8) = 720 \;\Rightarrow\; \boxed{R_{L_1} = 45.0\ \text{kN}\ (\uparrow)} $$ and vertical equilibrium gives $R_{L_5} = 72 - 45 = \boxed{27.0\ \text{kN}\ (\uparrow)}$.
  2. Section between L2 and L3. This cut severs U1–U2 (horizontal), U1–L3 (a $4:3$ diagonal, so components $0.8$ and $0.6$) and L2–L3 (horizontal). Only the diagonal has a vertical component, so resolving vertically on the left-hand portion, which carries $45 - 36 = 9$ kN of net upward force, $$ 9 - 0.6\,N_{U_1L_3} = 0 \;\Rightarrow\; \boxed{N_{U_1L_3} = +15.0\ \text{kN (tension)}} $$
  3. Top chord from the same section. Take moments about L3, through which both the diagonal and the bottom chord pass: $$ 3\,N_{U_1U_2} + 45(8) - 36(4) = 0 \;\Rightarrow\; \boxed{N_{U_1U_2} = -72.0\ \text{kN (compression)}} $$ The negative sign is expected — the top chord of a simply supported truss is in compression.
  4. Section between L3 and L4. Now the cut severs U2–U3, L3–U3 and L3–L4. The left-hand portion carries $45 - 36 - 36 = -27$ kN net, so resolving vertically, $$ -27 + 0.6\,N_{L_3U_3} = 0 \;\Rightarrow\; \boxed{N_{L_3U_3} = +45.0\ \text{kN (tension)}} $$ Both inner diagonals rise towards mid-span from the loaded joint and both are in tension, which is the expected behaviour of a truss whose diagonals slope towards the nearer support.

(b) Roof truss with a horizontal load at the apex

Given. A symmetric roof truss of 16 m span in four 4 m panels; the rafter rises 3 m over the first 8 m to the apex U1, so the intermediate rafter joints M1 and M2 are 3 m above the bottom chord and the apex 6 m. The truss is on a roller at L3 (the centre joint) and pinned at L5. It carries 60 kN downward at L1, 60 kN downward at L2, and 120 kN horizontally to the right at the apex U1.

Find. The forces in L2–L3, L3–L4 and M1–L3.

L1L2L3L4L5M1M2U160 kN60 kN120 kN4 m4 m4 m4 m3 m3 m
Figure 7 — truss 4(b). The supports are inboard: a roller under the centre joint L3 and a pin at L5, so the whole left-hand half acts as an overhang.

Approach. Find the reactions first — the unusual support arrangement makes them large and of opposite sense — then take a section, and finally isolate joint L3 for the sub-strut.

  1. Horizontal equilibrium. The only horizontal restraint is the pin, so $$ \boxed{H_{L_5} = 120\ \text{kN acting to the left}} $$
  2. Moments about L5. With the roller 8 m to the left of the pin, the two 60 kN loads 16 m and 12 m to the left, and the 120 kN load acting 6 m above the chord, $$ 8\,V_{L_3} = 60(16) + 60(12) - 120(6) = 960 + 720 - 720 = 960 $$ so that $$ \boxed{V_{L_3} = 120.0\ \text{kN}\ (\uparrow)} $$ and vertical equilibrium then gives $V_{L_5} = 120 - 120 = \boxed{0}$: the pin carries no vertical force at all, a result worth quoting because it is the clearest check available on the arithmetic.
  3. Section just left of L3. Cut M1–U1, M1–L3 and L2–L3 and keep the left-hand portion, which carries the two 60 kN loads. Taking moments about the point where the rafter and the sub-strut meet, that is M1 at $(4, 3)$, $$ 3\,N_{L_2L_3} + 60(4) = 0 \;\Rightarrow\; \boxed{N_{L_2L_3} = -80.0\ \text{kN (compression)}} $$ The bottom chord of the overhanging half is in compression, the reverse of the usual simply supported case, because that half hangs from the truss rather than spanning between supports.
  4. Bottom chord to the right of the support. Take a section between L3 and L4 and keep the right-hand portion, which carries only the pin reaction. Moments about M2 at $(12, 3)$ give $$ 3\,N_{L_3L_4} + 120(3) = 0 \;\Rightarrow\; \boxed{N_{L_3L_4} = -120.0\ \text{kN (compression)}} $$ the horizontal reaction being the only force involved.
  5. Joint L3 for the sub-strut. Four members meet at L3: the two bottom chords, the vertical U1–L3 and the sub-strut M1–L3, which runs from $(4,3)$ to $(8,0)$ and so has direction cosines $0.8$ and $0.6$. (The mirror member M2–L3 is a zero-force member here, because the whole right-hand half of the truss is unloaded apart from the pin reaction.) Horizontal equilibrium at L3 reads $$ N_{L_3L_4} - N_{L_2L_3} - 0.8\,N_{M_1L_3} = 0 $$ $$ -120 - (-80) - 0.8\,N_{M_1L_3} = 0 \;\Rightarrow\; \boxed{N_{M_1L_3} = -50.0\ \text{kN (compression)}} $$ Vertical equilibrium at the same joint then returns $N_{U_1L_3} = -90$ kN, and the roller reaction of 120 kN closes the joint exactly — $0.6(50) + 90 = 120$ — which is the check that the sub-strut force is right.
Question 4 — member forces
TrussMemberForceSense
(a)U1–U272.0 kNCompression
U1–L315.0 kNTension
L3–U345.0 kNTension
(b)L2–L380.0 kNCompression
L3–L4120.0 kNCompression
M1–L350.0 kNCompression

Reactions used above: truss (a), 45.0 kN and 27.0 kN upward at L1 and L5; truss (b), 120.0 kN upward at the roller L3, and at the pin L5 120 kN horizontally to the left with no vertical component.