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16-Civ-A1 Elementary Structural Analysis · December 2018

Question 8 of 8: Three-hinged gable frame (answer one of Q6/Q7/Q8)

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

Notes on this paper

Paper: National Exams — December 2018, 16-Civ-A1 Elementary Structural Analysis (closed book, 3 h; approved Casio/Sharp calculator permitted). 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), method of joints & sections (Ch. 3), shear & moment diagrams (Ch. 4), influence lines (Ch. 6), virtual-work deflections (Ch. 8–9), moment distribution (Ch. 11); A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound (Gerber) beams, three-hinged & indeterminate frames.

Sign convention. Upward reactions positive; sagging bending moment positive (tension on the underside), hogging negative; member axial force tension positive (T), compression negative (C).

These A1 papers are defined entirely by their figures, so every structure is redrawn to scale below.

Question 8: Three-hinged gable frame (22 marks) (answer one of Q6/Q7/Q8)

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. Symmetric gable: pins at feet $1(0,0)$ and $5(24,0)$, eaves $2(0,7)$ and $4(24,7)$, crown hinge $3(12,12)$; $span 24\text{ m}$, eave $7\text{ m}$, apex rise $5\text{ m}$. UDL $8.45\text{ kN/m}$ (vertical, on the horizontal projection) over the left rafter and UDL $4.26\text{ kN/m}$ (horizontal, $\rightarrow$) over the left column. Find. Reactions and the SFD/BMD (max/min ordinates).

crown hinge8.45 kN/m4.261234512 m12 m5 m7 m
Question 8 — three-hinged gable frame (pins at 1,5; crown hinge at 3).
  1. Loads. The rafter UDL over its $12\text{ m}$ horizontal projection totals $8.45(12)=101.4\text{ kN}\downarrow$ at $x{=}6$; the column UDL totals $4.26(7)=29.82\text{ kN}\rightarrow$ at $y{=}3.5$.
  2. Global equilibrium. $\sum M_{1}=0:\;V_5(24)=101.4(6)+29.82(3.5)\Rightarrow \boxed{V_5=29.7\text{ kN}}$, so $\boxed{V_1=71.7\text{ kN}}$.
  3. Crown-hinge condition. $M=0$ at the crown; taking the right half (crown to support 5, no applied load), $\sum M_{3}=0$ gives $\boxed{H_5=-29.7\text{ kN}}$ (i.e.\ $29.7\text{ kN}\leftarrow$), and horizontal equilibrium leaves $\boxed{H_1\approx0}$ — the wind thrust is reacted almost entirely at support 5.
  4. Member moments. The left column, pinned at $1$ and loaded by its UDL, hogs to $\boxed{-103.5\text{kN}\cdot\text{m}}$ at the eave $2$; the crown is a hinge ($M=0$); and the largest moment is at the right eave $4$, $\boxed{|M_4|=207.9\text{kN}\cdot\text{m}}$ ($=H_5\times7$).

Check: The rafter load is taken per horizontal projection ($w\cos\theta$ along the member $=7.8\text{ kN/m}$), the standard reading for a horizontally-banded UDL over a sloped rafter; the crown moment computes to $0$ to machine precision, confirming the three-hinge geometry and load reading.

QuantityValue
Support 1 (pin)$H_1\approx0,\;V_1=71.7\text{ kN}$
Support 5 (pin)$H_5=-29.7,\;V_5=29.7\text{ kN}$
$M$ at left eave (2)$-103.5\text{kN}\cdot\text{m}$
$M$ at crown (3)$0$ (hinge)
$M$ at right eave (4)$207.9\text{kN}\cdot\text{m}$ (max)
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