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.
$EI = 2\,000\ \text{kN}\cdot\text{m}^2$, 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.
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.
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,
$$V_1(4) = 6(4)(2) = 48 \;\Longrightarrow\;
\boxed{V_1 = V_5 = 12.0\ \text{kN}\ \uparrow}$$
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.
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.
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 $\text{kN}^2\cdot\text{m}^3$.
Divide by $EI$ and state the direction.
$$\delta_4 = \frac{-16.0}{2\,000} = -0.0080\ \text{m}$$
$$\boxed{\delta_4 = 8.0\ \text{mm}\ \text{UPWARD}}$$
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. 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.
Result
Value
Degree of static indeterminacy
$3(4) + 4 - 3(5) - 1 = 0$ — determinate
Vertical reactions
$V_1 = V_5 = 12.0\ \text{kN}\ \uparrow$
Horizontal reactions
zero at both pins
Peak real moment
$+12.0\ \text{kN}\cdot\text{m}$ at mid-span of 2–3