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16-Civ-A1 Elementary Structural Analysis · May 2015

Question 4 of 8: Member forces by the method of sections

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

Notes on this paper

Reference texts: R.C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy, method of joints/sections, virtual-work deflections, moment distribution / slope–deflection, influence lines; A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound (Gerber) beams and three-hinged frames. Sign convention: sagging bending moment positive; upward reactions positive; member tension positive (T), compression negative (C).

The paper directs candidates to answer Q1–Q5 and then one of Q6/Q7/Q8. For completeness all eight questions are worked here.

Question 4: Member forces by the 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.

Part (a)

L1L2L3L4L5U1U2U336 kN36 kN4 m4 m4 m4 m
Parallel-chord truss, 4 × 4 m, 3 m deep; 36 kN at $L_2$ and $L_3$. Members sought are highlighted.

Given. Span $16$ m (four $4$ m panels), depth $3$ m; $36$ kN down at $L_2$ and $L_3$; pin at $L_1$, roller at $L_5$. Find. $U_1U_2,\;U_1L_3,\;L_3U_3$.

  1. Reactions. $\sum M_{L_1}=0:\;16\,R_{L_5}=36(4)+36(8)=432\Rightarrow R_{L_5}=27$ kN; $R_{L_1}=72-27=45$ kN.
  2. Top chord $U_1U_2$. Section just right of $U_1$ and take moments about $L_3$ (where the two web members meet): $M_{L_3}=45(8)-36(4)=216$; with lever arm $3$ m, $U_1U_2=-216/3=\boxed{72\ \text{kN (C)}}$.
  3. Diagonals meeting at $L_3$. Vertical equilibrium of the cut and geometry (each diagonal rises $3$ over $4$, length $5$) give $U_1L_3=\boxed{15\ \text{kN (T)}}$ and $L_3U_3=\boxed{45\ \text{kN (T)}}$.
MemberForce
$U_1U_2$72 kN C
$U_1L_3$15 kN T
$L_3U_3$45 kN T

Part (b)

L1L2L3L4L5M1M2U160 kN60 kN120 kN4 m4 m4 m4 m
King-post truss: 120 kN horizontal at the apex $U_1$, 60 kN at $L_1$ and $L_2$; pin at $L_3$, roller at $L_5$.

Given. Apex $U_1$ at $(8,6)$, mid-height joints $M_1(4,3),M_2(12,3)$, bottom chord at $4$ m spacing; loads $120$ kN horizontal (right) at $U_1$ and $60$ kN down at $L_1$ and $L_2$; pin at $L_3$, roller at $L_5$. Find. $L_2L_3,\;L_3L_4,\;M_1L_3$.

  1. Reactions. $\sum M_{L_3}=0:\;8\,R_{L_5}=60(4)+60(8)-120(6)=0\Rightarrow R_{L_5}=0$. Then $R_{L_3}=120$ kN ↑ and the pin supplies $120$ kN horizontally (leftward) to balance the applied $120$ kN.
  2. $L_2L_3$. Isolating the left of a vertical section through the left panel and taking moments about $M_1$ gives $L_2L_3=\boxed{80\ \text{kN (C)}}$.
  3. $L_3L_4$. The right half carries no net vertical load ($R_{L_5}=0$), so $L_3L_4=\boxed{0}$.
  4. $M_1L_3$. Vertical equilibrium at the left web (diagonal rises $3$ over $4$, length $5$) gives $M_1L_3=\boxed{50\ \text{kN (C)}}$.
MemberForce
$L_2L_3$80 kN C
$L_3L_4$0 (zero-force here)
$M_1L_3$50 kN C