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04-BS-3 · December 2019

Question 2 of 6: Question 2 (paper Question II) — Plane Truss, Method of Joints (Part A · Statics, equal value)

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

Notes on this paper

National Examination 04-BS-3, Statics and Dynamics — 2019-Dec. Candidates were required to complete 2 questions from PART A (Statics) and 2 questions from PART B (Dynamics); every question is solved below so this paper serves as a complete study resource (Questions 1-3 = paper Part A, I-III; Questions 4-6 = paper Part B, IV-VI).

Reference texts: Hibbeler, Engineering Mechanics: Statics (14th ed.); Hibbeler, Engineering Mechanics: Dynamics (14th ed.).

Check — source reconstruction notes. (2) Question 1's isometric figure gives explicit 1 m / 1.5 m dimensions along the rod, but plotting them on a single straight line makes the six rigid-body equilibrium equations inconsistent (no solution exists). Reading the printed figure, the horizontal run bends twice: A→C is 2 m along the first horizontal direction (with the vertical 1.5 m branch C→D), C→E is 1 m along the perpendicular horizontal direction (this is where the smooth journal bearing sits), and E→F is a further 1.5 m continuing the first horizontal direction to the point that carries the 250 N cylinder. This reading is the only one of the plausible alternatives that returns a statically-determinate, non-degenerate system, and it lands on the clean values reported below — strong corroborating evidence for the reconstruction. (3) Question 4's dimensions place the pin O exactly 90 mm above the floor, equal to the sphere radius (90 mm R); the sphere therefore contacts the floor exactly when the rod is horizontal, which is used as the impact configuration. (4) Question 6 numbers the four-bar linkage O-A-B-C from the source's own 100 mm / 250 mm / 75 mm / 50 mm dimensions; O and C are the fixed pivots, OA and CB are the driven/driving cranks and AB is the coupler.

Question 2 (paper Question II) — Plane Truss, Method of Joints (Part A · Statics, equal value)

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.

Given. Plane truss, pin support at A(0,0), roller support at B(6,0). Joints C(0,3), D(6,3), E(3,7), F(9,7). A vertical 500 N load acts downward at F. Members: AC, CD, AB, CB, CE, ED, DB, DF, EF (9 members, 6 joints, pin+roller = 3 reactions; $m+r=2j=12$, statically determinate).

Find. The force in every member, and whether it is tension (T) or compression (C).

ABCDEF500 NCoordinates in metres; A pin, B roller
Figure 2. Six-joint, nine-member truss; grid units = 1 m; 500 N load at F.

Approach. Find the two support reactions from global equilibrium, then analyze each joint in turn (starting where only two unknown member forces meet), applying $\Sigma F_x=0,\ \Sigma F_y=0$ at every joint.

  1. Support reactions. Taking moments about A: $B_y(6)-500(9)=0\Rightarrow B_y=750$ N. Then $\Sigma F_y=0$: $A_y+750-500=0\Rightarrow A_y=-250$ N (i.e. 250 N downward), and $\Sigma F_x=0\Rightarrow A_x=0$.
  2. Joint A (members AC vertical, AB horizontal): $\Sigma F_x=0\Rightarrow F_{AB}=0$; $\Sigma F_y=0\Rightarrow F_{AC}+A_y=0\Rightarrow F_{AC}=250$ N (T).
  3. Joint B (members AB horizontal, DB vertical, CB diagonal to (0,3), reaction $B_y=750$ up): with $F_{AB}=0$, resolving the diagonal CB (direction cosines $6/6.708,\,3/6.708$) and DB against $B_y$ gives $F_{CB}=0$ and $F_{DB}=-750$ N (i.e. 750 N C).
  4. Joint C (AC, CD, CB, CE meeting): with $F_{AC}=250$ (T) and $F_{CB}=0$, resolving CD (horizontal) and CE (direction cosines to E(3,7): $3/6.083,\,4/6.083$) gives $F_{CE}=312.5$ N (T) and $F_{CD}=-187.5$ N (i.e. 187.5 N C).
  5. Joint D (CD, ED, DB, DF meeting): with $F_{CD}=-187.5$, $F_{DB}=-750$ known, resolving ED (to E(3,7): dir. $-3/5,\,4/5$) and DF (to F(9,7): dir. $3/5,\,4/5$) gives $F_{ED}=-312.5$ N (312.5 N C) and $F_{DF}=-625$ N (625 N C).
  6. Joint F (EF horizontal, DF diagonal, 500 N load) — check: $\Sigma F_y=0$: $-0.8F_{DF}-500=0\Rightarrow F_{DF}=-625$ N ✓; $\Sigma F_x=0$: $-F_{EF}-0.6F_{DF}=0\Rightarrow F_{EF}=375$ N (T) ✓, matching the independent joint-E check.
Final Results — Question 2 (member forces, T = tension, C = compression)
MemberForceSense
AB0 Nzero-force member
AC250 NT
CB0 Nzero-force member
CD187.5 NC
CE312.5 NT
ED312.5 NC
DB750 NC
DF625 NC
EF375 NT