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16-Civ-A1 Elementary Structural Analysis · May 2017

Question 4 of 8: Truss member forces (method of sections)

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

Notes on this paper

Paper: National Exams — May 2017, 16-Civ-A1 Elementary Structural Analysis (closed book, 3 h). Six questions constitute a complete paper: answer Q1–Q5 and one of Q6/Q7/Q8. For completeness all eight questions are worked here.

Reference texts: R.C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy (Ch. 2), joints/sections (Ch. 3), shear & moment diagrams (Ch. 4), influence lines (Ch. 6), virtual-work deflections (Ch. 8–9), moment distribution / slope–deflection (Ch. 11–12); A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound beams, indeterminate frames.

Sign convention: upward reactions positive; sagging bending moment positive (tension on the underside); member tension positive (T), compression negative (C).

These A1 papers are defined entirely by their figures, so every structure has been read from the printed figure and redrawn to scale below.

Question 4: Truss member forces (method of sections) (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.

4(a) Warren truss, 90 kN at $L_3$

Given. Bottom chord $L_1(0,0)\,L_2(8,0)\,L_3(16,0)\,L_4(24,0)$; top $U_1(4,3)\,U_2(12,3)\,U_3(20,3)$; pin $L_1$, roller $L_4$; $90\text{ kN}$ down at $L_3$. Find. $L_2L_3,\,U_2L_3,\,U_3L_3$.

L1L2L3L4U1U2U390 kN8 m8 m8 m3 m
4(a): parallel-chord (Warren) truss, single 90 kN panel load.
  1. Reactions. $\sum M_{L_1}=0:\;R_{L_4}(24)=90(16)\Rightarrow R_{L_4}=60\text{ kN}$; $R_{L_1}=30\text{ kN}$.
  2. Section cutting $U_2U_3,\,U_2L_3\;(=U_3L_3\text{ region})$ and $L_2L_3$. Taking the left free body ($R_{L_1}=30$) and moments about $U_2\,(12,3)$ eliminate the two members through $U_2$: $L_2L_3(3)=30(12)\Rightarrow L_2L_3=\boxed{+120\text{ kN (T)}}$.
  3. Vertical & joint equilibrium. The web diagonals carry the shear: $U_2L_3=\boxed{+50\text{ kN (T)}}$ and the end diagonal $U_3L_3=\boxed{+100\text{ kN (T)}}$ (both diagonals rise toward the loaded panel, so both pull).

4(b) Cantilever truss

Given. $U_1(0,0)\,U_2(4,0)\,U_3(8,0)$ (top), $L_1(0,-6)$, $L_2(4,-3)$; roller at $U_1$ (horizontal reaction), pin at $L_1$; loads $90\text{ kN}\downarrow$ at $U_2$, and $90\text{ kN}\downarrow + 40\text{ kN}\rightarrow$ at $U_3$. Find. $U_1L_2,\,U_1U_2,\,L_1L_2$.

U1U2U3L1L290 kN90 kN / 40 kN90 kN / 40 kN4 m4 m3 m3 m
4(b): wall-mounted cantilever truss (roller at U₁, pin at L₁).
  1. Reactions. $\sum M_{L_1}=0:\;-6U_{1x}=90(4)+90(8)+40(6)\Rightarrow U_{1x}=-220\text{ kN}$ (leftward). Then $L_{1x}=180\text{ kN}$, $L_{1y}=180\text{ kN}$.
  2. Joint / section. Resolving at the joints gives $U_1U_2=\boxed{+160\text{ kN (T)}}$ (top chord tension of the cantilever), the web $U_1L_2=\boxed{+75\text{ kN (T)}}$, and the bottom chord $L_1L_2=\boxed{-225\text{ kN (C)}}$.
(a)Force(b)Force
$L_2L_3$120 kN T$U_1L_2$75 kN T
$U_2L_3$50 kN T$U_1U_2$160 kN T
$U_3L_3$100 kN T$L_1L_2$225 kN C