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16-Civ-A1 Elementary Structural Analysis · December 2019

Question 6 of 8: Indeterminate frame by moment distribution (22 marks)

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

Notes on this paper

Paper: National Exams — December 2019, 16-Civ-A1 Elementary Structural Analysis (closed book, 3 h; approved Casio or 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 and stability (Ch. 2), method of joints and sections (Ch. 3), shear and 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 frames; J. C. McCormac, Structural Analysis: Using Classical and Matrix Methods (4th ed., Wiley) — Maxwell’s reciprocal theorem. Canadian practice for these actions is codified in CSA S16 and CSA S6, but this paper is pure analysis and invokes no code clauses.

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

Check — figure reading. Support types are read from the printed symbols: rollers are a triangle over two wheels, pins a plain triangle, and internal hinges open circles.

Question 6 — Indeterminate frame by moment distribution (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. A frame whose horizontal member runs from a free tip at joint 1 through joint 2 to joint 3 and on to joint 4. A 12 m column drops from joint 3 to a fixed base at joint 5.

Span 1–23 mUDL 24 kN/m; joint 1 is a free tip
Support at 2—pin
Span 2–39 m112 kN point load at midspan (4.5 m)
Span 3–49 mUDL 24 kN/m
Support at 4—roller
Column 3–512 mfixed base at 5; no load along its length

Find. Shear-force and bending-moment diagrams for every member, with the maximum and minimum ordinates labelled.

24 kN/m24 kN/m112 kN123453 m9 m9 m4.5 m12 m
Q6 — frame: free overhang 1–2, pin at 2, rigid joint 3 with a 12 m fixed-base column, roller at 4. All members share the same EI and are inextensible.

Approach. Check the degree of indeterminacy and whether sidesway can occur, compute fixed-end moments, then distribute and carry over at the two rotating joints until the unbalanced moments vanish; finally recover member shears from free-body equilibrium.

With $m=4$, $j=5$, $r = 2+1+3 = 6$ and no releases, $\mathrm{DSI} = 3(4)+6-3(5) = 3$. The pin at joint 2 and the fixed base at joint 5 both block horizontal translation of the beam, so there is no sidesway and the distribution runs on joint rotations alone. The 3 m overhang is statically determinate and simply applies a known moment at joint 2.

  1. Reduce the overhang. The cantilever 1–2 carries the UDL directly to joint 2: $$M_{21} = -\frac{wL^{2}}{2} = -\frac{24(3)^{2}}{2} = \boxed{-108\ \text{kN}\cdot\text{m}}$$ together with a shear of $24(3) = 72\ \text{kN}$. This moment is fixed and takes no part in the distribution; it simply has to be balanced by span 2–3.
  2. Fixed-end moments for the loaded spans. For the central point load on span 2–3 and the UDL on span 3–4, $$\mathrm{FEM}_{23} = \pm\frac{PL}{8} = \pm\frac{112(9)}{8} = \pm126\ \text{kN}\cdot\text{m}$$ $$\mathrm{FEM}_{34} = \pm\frac{wL^{2}}{12} = \pm\frac{24(9)^{2}}{12} = \pm162\ \text{kN}\cdot\text{m}$$ The column carries no transverse load, so its fixed-end moments are zero.
  3. Distribution factors. With equal $EI$ throughout, relative stiffnesses are $I/L$: span 2–3 gives $1/9$, span 3–4 gives $1/9$ (modified to $\tfrac{3}{4}(1/9)$ because joint 4 is a roller, a pinned far end) and the column gives $1/12$. At joint 3 these yield distribution factors of roughly 0.42 to span 2–3, 0.32 to span 3–4 and 0.26 to the column; joint 2 distributes wholly into span 2–3 because the overhang moment is fixed.
  4. Distribute and carry over. Balancing joints 2 and 3 in turn, carrying over one half to each fixed far end and iterating until the residuals fall below 0.1 kN·m, the final member end moments settle at $$M_{23} = +108, \quad M_{32} = -171, \quad M_{34} = +207, \quad M_{43} = 0, \quad M_{35} = -36, \quad M_{53} = +18$$ all in kN·m. Joint 3 balances exactly: $-171 + 207 - 36 = 0$.
  5. Member shears from free bodies. Span 2–3 carries end shears of $+49$ kN and $-63$ kN either side of the 112 kN load; span 3–4 runs from $+131$ kN at joint 3 to $-85$ kN at the roller; the column carries a constant $4.5$ kN. Summing at the supports, $$R_2 = 72 + 49 = \boxed{121\ \text{kN}}, \quad R_4 = \boxed{85\ \text{kN}}, \quad R_5 = 63 + 131 = \boxed{194\ \text{kN}}$$ with a horizontal thrust of 4.5 kN at the base opposed by the pin at joint 2, and a base moment of 18 kN·m. Total vertical reaction is $121+85+194 = 400\ \text{kN}$, matching the applied $72+112+216 = 400\ \text{kN}$.
-7249-63131-85Shear force (kN)
Q6 shear-force diagram along the beam 1–2–3–4 (the column carries a constant 4.5 kN shear).
  1. Locate the sagging peak in span 3–4. Measuring $s$ from joint 3, the shear $131 - 24s$ vanishes at $s = 5.458\ \text{m}$, where $$M = -207 + 131(5.458) - 12(5.458)^{2} = \boxed{+150.5\ \text{kN}\cdot\text{m}}$$ and the moment returns to zero at the roller, as it must.
  2. Read the step at joint 3. The beam moment is $-171$ kN·m just left of joint 3 and $-207$ kN·m just right of it. The difference of 36 kN·m is exactly the moment carried away down the column — the visible signature of joint equilibrium on a bending-moment diagram. Along the column the moment runs linearly from 36 kN·m at the top to 18 kN·m of opposite sense at the base, passing through zero 4 m above the foundation.
-108112.5-1712070Bending moment (kN·m)
Q6 bending-moment diagram. The step at joint 3 (−171 to +207) is exactly the 36 kN·m carried away by the column, so the joint moment-balances.
Question 6 — results
MemberMoment ordinates (kN·m)Shear ordinates (kN)
1–2 (overhang)0 at the tip to −108 at joint 20 to −72
2–3−108, +112.5 under the load, −171 at joint 3+49 then −63
3–4−207, +150.5 at 5.46 m, 0 at the roller+131 to −85
Column 3–536 at the top, 18 at the base (opposite sense)4.5 constant
Reactions$R_2 = 121$ kN, $R_4 = 85$ kN, $R_5 = 194$ kN with $H_5 = 4.5$ kN and $M_5 = 18$ kN·m
Check — the non-round answers are correct. Final moments such as −171 and +207 kN·m and a peak of +150.5 kN·m look untidy for an examination, but the distribution converges on exactly these values and an independent direct-stiffness solve reproduces them to four figures. Do not round the distribution short in the hope of recovering neat numbers.