NivaarExam PrepOfficial exam papers ↗

07-Str-A1 · May 2016

Question 7 of 8: Vertical Deflection of a Frame by Virtual Work

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

Notes on this paper

Paper format. National Exams, May 2016 — 07-Str-A1 Elementary Structural Analysis, 3 hours, CLOSED BOOK (an approved Sharp or Casio calculator is permitted). Six questions constitute a complete paper: Questions 1–5 are compulsory and one only of Questions 6, 7 or 8 is attempted, for 100 marks (6 + 18 + 15 + 18 + 21 + 22). Marks are shown in the left margin. All eight questions are worked below, because the three alternatives exercise three different methods — slope deflection, virtual work and three-hinged-frame statics — and the complete set is the more useful study resource.

Every structure on this paper is defined by a hand-drawn figure and nothing else: the printed text gives the task, the drawing gives the geometry, the loads and the support types.

Sign conventions used throughout. Shear force is positive when the resultant of the forces to the left of a section acts upwards; bending moment is positive when it sags the member (tension on the underside), and sagging ordinates are plotted above the axis in every diagram. Truss member forces are quoted as T for tension and C for compression. In the slope-deflection work of Question 6 the member-end moments follow the usual convention, clockwise on the member end taken as positive.

Reference texts.

Question 7: Vertical Deflection of a Frame by Virtual Work (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.

QuantityValue
Node coordinates (m)$1(0,0)$, $2(0,3)$, $3(4,3)$, $4(5,3)$, $5(4,0)$
Supportspins at nodes 1 and 5
Internal hingenode 2, where column 1–2 meets the beam
Loading$w = 6\ \text{kN}/\text{m}$ over the 4 m span 2–3
Overhang$1\ \text{m}$ from node 3 to the free end 4
Flexural rigidity$EI = 2\,000\ \text{kN}\cdot\text{m}^2$, all members

Find. The vertical deflection of node 4, with its direction.

Approach. Confirm the frame is determinate, solve the real system, then apply a unit vertical load at node 4 and evaluate $\delta_4 = \int Mm\,\mathrm{d}s/EI$ over every member. Almost all of that work disappears once it is noticed which members carry no moment at all.

  1. Check determinacy, and notice the hinge. With $m = 4$ members, $j = 5$ joints, $r = 4$ reaction components and $c = 1$ release at the node-2 hinge, $$i = 3m + r - 3j - c = 12 + 4 - 15 - 1 = 0$$ so the frame is statically determinate. The hinge at node 2 is what makes it so, and it also makes column 1–2 a two-force member: it is pinned at node 1, hinged at node 2 and carries no load between, so it transmits a purely vertical force and no moment.
  2. Solve the real system. Since column 1–2 can deliver only a vertical force at node 2, there is no horizontal reaction anywhere, and the beam 2–3–4 is simply supported at nodes 2 and 3 with an unloaded overhang. Taking moments about node 3, $$V_1(4) = 6(4)(2) = 48 \;\Longrightarrow\; \boxed{V_1 = V_5 = 12.0\ \text{kN}\ \uparrow}$$
  3. Write the real bending moments. On the span, with $x$ from node 2, $$M(x) = 12x - 3x^2, \qquad 0 \le x \le 4$$ which peaks at $M(2) = 12.0\ \text{kN}\cdot\text{m}$ and returns to zero at node 3. The overhang carries nothing, so $M = 0$ there; the moment is therefore continuous and zero through node 3, which leaves column 3–5 with no end moment either, and column 1–2 has none because it is a two-force member. The entire real moment diagram lives on the single 4 m span.
  4. Apply the unit load and write the virtual moments. A unit downward load at node 4 acts 1 m beyond node 3, so moments about node 3 give $$v_1 = -\frac{1(1)}{4} = -0.25 \quad(\text{i.e. }0.25\ \text{kN downward at node 1}),\qquad v_5 = +1.25\ \text{kN}$$ Along the span, $m(x) = -0.25x$, reaching $m = -1.0\ \text{kN}\cdot\text{m}$ at node 3, which is exactly the hogging moment the 1 m overhang delivers there. On the overhang the virtual moment runs from $0$ at node 4 to $-1.0$ at node 3, and both columns again carry no moment.
  5. Evaluate the single surviving integral. Only span 2–3 has both $M \ne 0$ and $m \ne 0$: $$\int_0^4 M m\,\mathrm{d}x = -0.25\int_0^4\left(12x^2 - 3x^3\right) \mathrm{d}x = -0.25\left[4x^3 - \tfrac{3}{4}x^4\right]_0^4 = -16.0$$ in $\text{kN}^2\cdot\text{m}^3$.
  6. Divide by $EI$ and state the direction. $$\delta_4 = \frac{-16.0}{2\,000} = -0.0080\ \text{m}$$ $$\boxed{\delta_4 = 8.0\ \text{mm}\ \text{UPWARD}}$$
  7. Confirm it geometrically. The overhang is rigid and unloaded, so node 4 simply follows the rotation of node 3. For a simply supported span under a uniform load that end rotation is $$\theta_3 = \frac{wL^3}{24EI} = \frac{6(4)^3}{24(2\,000)} = 0.0080\ \text{rad}$$ and the tip rises by $\theta_3 \times 1\ \text{m} = 8.0\ \text{mm}$, reproducing the virtual-work result exactly.
Q7 — frame geometry, loading and the hinge at node 26 kN/m123454 m1 m3 mEI = 2000 kN·m²
Q7. The blue circle at node 2 is an internal hinge; node 3 is a rigid T-joint. That single release is what makes the frame determinate and reduces column 1–2 to a vertical two-force strut.
Check: the small open circle where column 1–2 meets the beam at node 2 is read as an internal hinge, while the junction at node 3 shows no such circle and is taken as rigid. That reading is what makes the frame determinate; treating node 2 as rigid instead would leave the structure once indeterminate and put the question beyond the reach of a bare virtual-work calculation, which the wording plainly does not intend.
ResultValue
Degree of static indeterminacy$3(4) + 4 - 3(5) - 1 = 0$ — determinate
Vertical reactions$V_1 = V_5 = 12.0\ \text{kN}\ \uparrow$
Horizontal reactionszero at both pins
Peak real moment$+12.0\ \text{kN}\cdot\text{m}$ at mid-span of 2–3
Virtual moment at node 3$-1.0\ \text{kN}\cdot\text{m}$
Virtual work integral$\int Mm\,\mathrm{d}s = -16.0\ \text{kN}^2\cdot\text{m}^3$
Rotation of node 3$\theta_3 = 0.0080\ \text{rad}$
Deflection at node 4$\delta_4 = 8.0\ \text{mm}\ \textbf{upward}$