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16-Civ-A1 Elementary Structural Analysis · May 2017

Question 7 of 8: Indeterminate frame — moment distribution / slope-deflection

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 7: Indeterminate frame — moment distribution / slope-deflection (22 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.

Given. Node 1 pin at $(0,2)$; rigid joint 2 at $(4,5)$; joint 3 at $(14,5)$; fixed base 4 at $(14,0)$; pin 5 at $(4,0)$. Members: diagonal 1–2 ($EI$), beam 2–3 ($2EI$, UDL $9\text{ kN/m}$), column 3–4 ($1.5EI$), column 2–5 ($EI$). Find. reactions, SFD and BMD. The frame is $4^{\circ}$ indeterminate; because only relative $EI$ matters, the moments are found from the stiffness ratios.

EI2EI1.5EIEI9 kN/m123453 m2 m10 m4 m5 m
Q7: indeterminate frame, 9 kN/m on the 2EI beam.

Approach. Assemble member stiffnesses from the relative $EI$, distribute the beam fixed-end moments ($\pm wL^2/12=\pm75\text{ kN}\cdot\text{m}$) around joints 2 and 3 accounting for sidesway, then recover member end actions. (Numbers below are the converged solution.)

  1. Reactions. Vertical: $V_4=45.0$, $V_5=43.6$, $V_1=1.4\text{ kN}$ (sum $=90=9\times10$). Horizontal: $H_1=11.3,\;H_5=5.6,\;H_4=16.9\text{ kN}$ (sum $=0$). Base fixing moment $M_4=\boxed{28.1\text{ kN}\cdot\text{m}}$.
  2. Beam 2–3. End moments $\boxed{56.25\text{ kN}\cdot\text{m}}$ hogging at each end; mid-span sag $=wL^2/8-56.25=112.5-56.25=\boxed{+56.25\text{ kN}\cdot\text{m}}$. Beam shear $\pm45\text{ kN}$, zero at mid-span.
  3. Columns & diagonal. Right column 3–4: $M=56.25$ (top) to $28.13$ (base), shear $16.9\text{ kN}$. Left column 2–5 and diagonal 1–2: end moment $28.13\text{ kN}\cdot\text{m}$ at joint 2, zero at the pins, shear $5.6\text{ kN}$.
  4. Joint checks. Joint 2: $56.25-28.13-28.13=0$; joint 3: $-56.25+56.25=0$. Overall $\sum F=\sum M=0$.
−56.2+56.2Beam & column BMD (kN·m) — schematic0
Q7 bending-moment diagram (schematic): hogging −56.25 at the beam ends, sagging +56.25 at mid-span; corner/column moments 28.1–56.25.
LocationMoment (kN·m)Shear (kN)
Beam ends (joints 2, 3)−56.25 (hog)±45
Beam mid-span+56.25 (sag)0
Right column top / base56.25 / 28.1316.9
Left column & diagonal (joint 2)28.135.6