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24-Bld-A1 Elementary Structural Analysis · May 2018

Question 4 of 8: Truss member forces by the method of sections/joints

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

Notes on this paper

National Exams May 2018 — 07-BLD-A1 Elementary Structural Analysis, 3 hours, closed book (approved Casio/Sharp calculator only). Answer ALL of Questions 1–5; answer ONLY ONE of Questions 6, 7 or 8 (this solution set, per pipeline convention, answers all three optional questions).

Reference texts: Hibbeler, Structural Analysis, 10th ed.; Kassimali, Structural Analysis, 6th ed.

Question 4: Truss member forces by the method of sections/joints (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) Calculate the forces in U1–U2, L2–U2 and L2–L3

Given. A 24 m Warren truss, height 4 m, panels of 6 m (top chord U1–U4 at x=3,9,15,21; bottom chord L1–L5 at x=0,6,12,18,24); pin at L1, roller at L5; 24 kN horizontal at U1; 32/40/48 kN downward at L2/L3/L4.

Find. Forces in U1U2, L2U2, L2L3 (tension/compression).

L1U1L2U2L3U3L4U4L524 kN32 kN40 kN48 kN
Truss (a): Warren configuration, panel loads at L2/L3/L4, horizontal load at U1.

Approach. Find the reactions from overall equilibrium, then cut a section through the panel containing L2/U2 (severing U1U2, L2U2 and L2L3) and take moments/force-sums of the left free body.

  1. Reactions. $$\Sigma F_x=0:\ R_{x,L1}=-24\text{ kN}$$ $$\Sigma M_{L1}=0:\ 24R_{y,L5}=24(4)+32(6)+40(12)+48(18)=1632\Rightarrow R_{y,L5}=\boxed{68\text{ kN}}$$ $$R_{y,L1}=32+40+48-68=\boxed{52\text{ kN}}$$
  2. Section cut through the L2/U2 panel — left free body {L1, U1, L2}. $$\Sigma F_y=0:\ 52-32+0.8\,F_{L2U2}=0\Rightarrow F_{L2U2}=\boxed{-25\text{ kN (25 kN compression)}}$$
  3. Moments about U2 (9,4) (eliminates U1U2 and L2U2, both passing through it): $$4F_{L2L3}=468\Rightarrow F_{L2L3}=\boxed{+117\text{ kN (tension)}}$$
  4. Then $$\Sigma F_x=0:\ -24+F_{U1U2}+0.6(-25)+117=0\Rightarrow F_{U1U2}=\boxed{-102\text{ kN (102 kN compression)}}$$
MemberForceSense
U1U2102 kNCompression
L2U225 kNCompression
L2L3117 kNTension

(b) Calculate the forces in L1–U2, L1–L2 and U1–L3

Given. A 2-panel (3 m each), 4 m tall truss pinned to a rigid wall at both U1 and L1; verticals at each panel point; diagonals L1U2 and U1L3 (the counter-diagonal spanning both panels) and L2U3; 20 kN down at U2, 36 kN horizontal at U3, 60 kN down at each of L2 and L3.

Find. Forces in L1U2, L1L2, U1L3 (tension/compression).

U1U2U3L1L2L320 kN36kN60 kN60 kN
Truss (b): pinned to a rigid wall at both U1 and L1; counter-diagonal U1–L3 spans both panels.

Approach. Two pins into one rigid wall give 4 reaction components — one more than the 3 a single rigid body needs — but that redundancy lives entirely in the vertical U1L1 member and the reaction split; it never enters the equilibrium equations of the four away-from-the-wall joints (U2, U3, L2, L3), so those 8 equations solve the other 8 members — including all three asked for — uniquely by the method of joints.

  1. Joint U2 (members U1U2, U2U3, L1U2; load 20 kN down). Direction L1→U2 is (3,4)/5. $$\Sigma F_y=0:\ -0.8F_{L1U2}-20=0\Rightarrow F_{L1U2}=\boxed{-25\text{ kN (25 kN compression)}}$$
  2. Joint L3 (members L2L3, L3U3 vertical, U1L3; load 60 kN down). Direction L3→U1 is (−6,4)/√52. Working the four free joints together (L2’s and U3’s equilibrium first fixes L2U3=75 kN (T) and U3L3=0) gives, at L3: $$0.5547\,F_{U1L3}=120\Rightarrow F_{U1L3}=60\sqrt{13}=\boxed{+216.3\text{ kN (tension)}}$$
  3. Joint L2 (members L1L2, L2L3, L2U3; load 60 kN down) with L2L3=−180 kN (from L3’s $$\Sigma F_x$$): $$F_{L1L2}=F_{L2L3}+0.6(75)=-180+45=\boxed{-135\text{ kN (135 kN compression)}}$$
MemberForceSense
L1U225 kNCompression
L1L2135 kNCompression
U1L3216.3 kNTension