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16-Civ-A1 Elementary Structural Analysis · December 2019

Question 3 of 8: Truss deflection by virtual work (14 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 3 — Truss deflection by virtual work (14 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 truss cantilevered from a wall, pinned to it at both $U_1$ and $L_1$. Taking $L_1$ as the origin, the joint coordinates in metres are:

$L_1$$(0,\ 0)$pinned to the wall
$U_1$$(0,\ 6.5)$pinned to the wall
$L_2$$(7.8,\ 0)$mid bottom-chord joint
$U_2$$(7.8,\ 3.25)$40 kN applied downward
$U_3$$(15.6,\ 0)$free tip

The six members are $U_1U_2$, $U_2U_3$, $L_1L_2$, $L_2U_3$, $U_2L_2$ and $L_1U_2$, with $AE = 84.5\times10^{3}\ \text{kN}$ throughout. The top chord $U_1$–$U_2$–$U_3$ is straight, so $U_1U_2$ and $U_2U_3$ each have length $\sqrt{7.8^{2}+3.25^{2}} = 8.45\ \text{m}$.

Find. (a) the vertical deflection of $U_3$ under the 40 kN load at $U_2$; (b) the vertical deflection of $U_2$ when that same load is moved to $U_3$.

U1U2U3L1L240 kN3.25 m3.25 m7.8 m7.8 m
Q3 — truss pinned to the wall at U1 and L1. The 40 kN load acts at U2; part (a) asks for the vertical deflection at U3.

Approach. Use the unit-load (virtual work) method, $\delta = \sum NnL/AE$, solving the truss twice — once for the real 40 kN load and once for a unit load at the joint and in the direction of the required deflection — and then answer part (b) by Maxwell’s reciprocal theorem rather than by re-analysing.

Determinacy first: $m=6$ members, $n=5$ joints and $r=4$ (two pins), so $m+r-2n = 6+4-10 = 0$ and the truss is statically determinate, as the virtual-work method requires.

  1. Real forces $N$ under the 40 kN load at $U_2$. Only two members meet at $U_2$ other than the unloaded pair towards $U_3$ and $L_2$, and joint equilibrium at $U_2$ resolves the load entirely into the two members running back to the wall. With direction cosines $7.8/8.45 = 0.923$ and $3.25/8.45 = 0.385$, $$N_{U_1U_2} = \frac{40 \times 8.45}{2(3.25)} = +52\ \text{kN (T)}, \qquad N_{L_1U_2} = -52\ \text{kN (C)}$$ and every other member carries zero. Joints $U_3$ and $L_2$ are unloaded and each connects only to zero-force members, which confirms the result.
  2. Virtual forces $n$ for a unit downward load at $U_3$. Repeating the joint analysis with 1 kN at the tip gives $$n_{U_1U_2} = +2.6, \quad n_{U_2U_3} = +2.6, \quad n_{L_1L_2} = n_{L_2U_3} = -2.4, \quad n_{U_2L_2} = n_{L_1U_2} = 0$$ A quick global check: the wall couple is resisted over the 6.5 m depth, and $1 \times 15.6 / 6.5 = 2.4$, consistent with the chord forces above.
  3. Form the sum $\sum NnL/AE$. A product $Nn$ is non-zero only where both systems load the member. Here that happens for $U_1U_2$ alone: $U_2U_3$ has $n=2.6$ but $N=0$, while $L_1U_2$ has $N=-52$ but $n=0$. So a single term survives:
Virtual-work tabulation (only non-zero contributions shown)
Member$N$ (kN)$n$ (kN/kN)$L$ (m)$NnL/AE$ (mm)
$U_1U_2$+52+2.68.4513.52
$U_2U_3$0+2.68.450
$L_1U_2$−5208.450
$L_1L_2$, $L_2U_3$, $U_2L_2$0——0
Sum13.52
  1. Evaluate the deflection. $$\delta_{U_3} = \sum \frac{NnL}{AE} = \frac{(52)(2.6)(8.45)}{84.5\times10^{3}} = \frac{1142.44}{84\,500} = 0.01352\ \text{m}$$ $$\delta_{U_3} = \boxed{13.52\ \text{mm downward}}$$ The positive sign means the deflection is in the same direction as the assumed unit load, so $U_3$ moves down.
  2. Part (b) by reciprocity. Maxwell’s reciprocal theorem states that for a linearly elastic structure the deflection at $j$ caused by a load at $k$ equals the deflection at $k$ caused by the same load applied at $j$: $$\delta_{jk} = \delta_{kj}$$ Part (a) is exactly $\delta_{U_3 U_2}$ — the deflection at $U_3$ due to 40 kN at $U_2$. Part (b) asks for $\delta_{U_2 U_3}$, the deflection at $U_2$ due to 40 kN at $U_3$. These are the same number: $$\delta_{U_2} = \boxed{13.52\ \text{mm downward}}$$ No second analysis is needed. (Carrying one out anyway reproduces 13.52 mm to the last digit.)
Question 3 — results
Determinacy check$m+r-2n = 6+4-10 = 0$ (determinate)
$N_{U_1U_2}$ / $N_{L_1U_2}$ (real)+52 kN (T) / −52 kN (C)
$n_{U_1U_2}$ (unit load at $U_3$)+2.6
(a) $\delta_{U_3}$13.52 mm downward
(b) $\delta_{U_2}$13.52 mm downward (by Maxwell’s reciprocal theorem)