Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations,
May 2015 — 07-Str-A1 Elementary Structural Analysis. Three hours,
CLOSED BOOK, an approved Sharp or Casio calculator permitted. Six questions
constitute a complete paper: answer ALL of Questions 1 to 5 and ONE of
Questions 6, 7 or 8. Marks are shown in the left margin
(6 + 18 + 16 + 18 + 20 + 22 = 100). All eight questions are solved below,
because the three alternatives exercise quite different methods —
slope-deflection, virtual work and the statics of a three-hinged frame —
and the complete set is the more useful study resource.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 2
(determinacy and stability), Ch. 3–5 (trusses, internal loadings, frames),
Ch. 6 (influence lines), Ch. 8–9 (deflections and virtual work),
Ch. 11 (slope-deflection).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3
(equilibrium and determinacy), Ch. 4 (plane trusses), Ch. 5 (beams and frames),
Ch. 7 (deflections by the method of virtual work), Ch. 8–9 (influence
lines), Ch. 16 (slope-deflection).
K. Leet, C.-M. Uang and A. Gilbert, Fundamentals of Structural
Analysis, 5th ed. — a parallel treatment of the same syllabus.
C. H. Norris, J. B. Wilbur and S. Utku, Elementary Structural
Analysis, 4th ed. — the classical text this exam code is named
after.
Check: every support type, hinge and member below
was read off the drawings, not off the printed text. In this subject the text carries almost no data: spans, loads, support types and hinge positions exist only in the hand-drawn figures. The classification in Question 1 in particular turns
entirely on telling a pin (plain triangle on hatching) from a roller (triangle
over two rollers) and a rigid joint from an internal hinge (small open
circle).
Given. A gable frame pinned at node 1 and at node 5, with an
internal hinge at the apex node 3. Taking node 1 as the origin, node 2 is 4 m
above it, the apex node 3 is at $(12,\,9)$, node 4 at $(21,\,5.25)$ and the
right-hand base node 5 at $(21,\,-3)$, that is 3 m below the level of node 1.
Both rafters have the slope 5 in 12. A uniform load of 2.5 kN/m acts vertically
over the horizontal projection of the left rafter, and a 30 kN horizontal force
acts to the left on the right column, 3 m above node 5.
Given data — Question 8
Node
Coordinates (m)
Note
1
(0, 0)
pin
2
(0, 4)
left knee
3
(12, 9)
apex hinge
4
(21, 5.25)
right knee
5
(21, −3)
pin, 3 m below node 1
Loads: 2.5 kN/m on the projection 0–12 m (30 kN total);
30 kN horizontal, acting leftward, at (21, 0)
Find. The four reaction components and the shear force and
bending moment diagrams for all four members, with the extreme ordinates.
Figure 12 — the three-hinged
gable frame and its bending moment, developed along each half of the frame.
Ordinates are plotted against distance measured along the member axis, so the
continuity of moment through each rigid corner is visible as a single
curve.
Approach. Four unknown reaction components need four
equations: the three of overall equilibrium plus the condition that the bending
moment at the apex hinge is zero, written as moments about the hinge for the
right-hand portion alone.
Confirm determinacy. Two pins give $r = 4$; the apex hinge
supplies one equation of condition, so $i = 4 - (3 + 1) = 0$ and statics alone
suffices. The 2.5 kN/m acting over the 12 m projection totals 30 kN, applied
through $x = 6$ m.
Moments about node 1 for the whole frame. The 30 kN
horizontal force acts at the level of node 1, so it has no moment about that
point; the right-hand reaction acts at $(21, -3)$. Hence
$$ 21V_5 + 3H_5 = 30(6) = 180 . $$
Moments about the apex hinge for the right-hand portion. The
right-hand portion carries only the 30 kN force and the reaction at node 5:
$$ 9V_5 + 12H_5 = 30(9) = 270 . $$
Solve the pair.
$$ \boxed{V_5 = 6.0\ \text{kN}\ (\uparrow), \qquad
H_5 = 18.0\ \text{kN}\ (\rightarrow)} $$
and the two remaining equilibrium equations give
$$ \boxed{V_1 = 24.0\ \text{kN}\ (\uparrow), \qquad
H_1 = 12.0\ \text{kN}\ (\rightarrow)} $$
The horizontal check is $12 + 18 = 30$ kN, balancing the applied force, and the
vertical check is $24 + 6 = 30$ kN, balancing the roof load.
Left column 1–2. It carries no transverse load, so the
shear is the constant 12 kN and the moment grows linearly from zero at the pin to
$$ M_2 = 12(4) = \boxed{48.0\ \text{kN}\!\cdot\!\text{m}} $$
with tension on the outer (left) face. The axial force is a constant 24 kN
compression.
Left rafter 2–3. Taking the free body below and to the
left of a section whose horizontal coordinate is $x$, and remembering that the
distributed load acts on the projection,
$$ M(x) = 48 - 19x + 1.25x^{2} $$
which is $+48$ kN·m at the knee, zero at the apex as the hinge demands,
and stationary where $\mathrm{d}M/\mathrm{d}x = -19 + 2.5x = 0$, that is at
$x = 7.6$ m, where
$$ M = \boxed{-24.2\ \text{kN}\!\cdot\!\text{m}} $$
with tension on the inner (under) face. Resolving the net force
$(12,\ 24-2.5x)$ perpendicular to the rafter, whose direction cosines are
$12/13$ and $5/13$, the shear runs from $+17.54$ kN at the knee to $-10.15$ kN at
the apex, vanishing at the same $x = 7.6$ m; the axial force runs from
20.31 kN to 8.77 kN compression.
Right column 5–4. Below the applied force the shear is
the constant 18 kN and the moment grows to
$$ M = 18(3) = \boxed{54.0\ \text{kN}\!\cdot\!\text{m}} $$
at the point of application, with tension on the inner (left) face. Above it the
net horizontal force is $18 - 30 = -12$ kN, so the shear reverses to 12 kN and
$M = 54 - 12y$ measured from that level, passing through zero 4.5 m above node 5
and reaching
$$ M_4 = \boxed{-9.0\ \text{kN}\!\cdot\!\text{m}} $$
at the knee, now with tension on the outer (right) face. The axial force in the
column is 6 kN compression throughout.
Right rafter 4–3. With no load on it the moment is
linear, and $M = 12 - x$ in terms of the horizontal coordinate, so it runs from
$-9.0$ kN·m at the knee to zero at the apex hinge, confirming the previous
step from the other side. Its length is
$\sqrt{9^2 + 3.75^2} = 9.75$ m, so the shear is the constant
$9/9.75 = 0.92$ kN and the axial force is 13.39 kN compression.
Assemble the diagrams. The bending moment is zero at both
pins and at the apex hinge, peaks at $+54$ kN·m where the 30 kN force is
applied, reaches $+48$ kN·m at the left knee and dips to
$-24.2$ kN·m on the left rafter. Those are the maximum and minimum
ordinates of the whole frame.