Question 1 of 8: Stability and determinacy of seven structures
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations,
May 2014 — 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 4, ONE of Questions 5
or 6, and ONE of Questions 7 or 8. Marks are shown in the left margin
(7 + 18 + 15 + 18 + 20 + 22 = 100). All eight questions are solved below,
because the alternatives test different topics and the whole 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, virtual work),
Ch. 11–12 (slope-deflection, moment distribution).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3
(equilibrium and determinacy), Ch. 4 (plane trusses), Ch. 5 (beams and frames),
Ch. 7 (deflections by virtual work), Ch. 8–9 (influence lines),
Ch. 16–17 (slope-deflection, moment distribution).
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 after which this exam code is
named.
Canadian design context: CSA S16 Design of Steel Structures,
CSA A23.3 Design of Concrete Structures and the National Building
Code of Canada. This is a pure analysis paper, so no code clause is needed
to answer it, but every result below is in the SI units those documents use.
Sign conventions used throughout. For a beam, or for one
member of a frame, shear is positive when the resultant of the forces on the
left of (or below) a section acts upward, and bending moment is positive when
it sags the member — that is, when it puts the underside of a beam, or
the inside face of a frame member, in tension. Truss forces are quoted as
T for tension and C for compression. In every figure applied
loads are red, reactions are blue, and an internal hinge is a red circle.
Question 1: Stability and determinacy of seven structures (7 marks)
Given. Seven plane assemblies. Structures (a) to (e)
are built from flexural (beam-type) members, so each member end carries axial
force, shear and moment unless a release says otherwise; (f) and (g) are
pin-jointed trusses in which the crossing diagonals pass one another without
being connected, so each crossing diagonal is a separate two-force member.
Find. For each structure, one of “unstable”,
“statically determinate” or “statically indeterminate to
degree n”.
[Figure not reproduced: Question 1 — the seven structures, redrawn from the examination paper. (a)–(e) are beam-type assemblies; (f) and (g) are pin-jointed trusses whose crossing diagonals are not connected where they cross. Hatching denotes a fixed base, a triangle on hatching a pin, a triangle on rollers a r. See the official exam paper.]
Approach. Count first, then look: for a beam-type
assembly use $i = 3m + r - 3j - c$ and for a pin-jointed truss use
$i = m + r - 2j$, then confirm that the members and reactions are actually
arranged so as to restrain every degree of freedom, because a
satisfactory count proves nothing on its own.
State the two counting rules. For a plane assembly of
flexural members,
$$i = 3m + r - 3j - c$$
where $m$ is the number of members, $j$ the number of joints (support points
included), $r$ the number of reaction components and $c$ the number of released
conditions (one per moment release in a two-member joint; $n-1$ if a pin joins
$n$ members). For a pin-jointed truss the corresponding count is
$$i = m + r - 2j .$$
A negative $i$ means a mechanism; $i = 0$ with a sound arrangement means
determinate; $i > 0$ means indeterminate to that degree.
(a) Fixed end, one internal hinge, two rollers. The
reaction components are $r = 3 + 1 + 1 = 5$ and the hinge supplies one
condition equation, so
$$i = 5 - 3 - 1 = \boxed{1}$$
Horizontal restraint comes from the fixed end and travels through the hinge as
an axial force, so the beam is properly restrained: statically
indeterminate to the first degree.
(b) Beam carried on the apex pin of a two-legged fixed-base
frame. Each leg is built in at its base, so each leg on its own already
fixes the apex; pinning the two legs together there adds two redundant
constraints. The beam, however, touches the rest of the structure only at that
one pin, and a pin transmits no moment. Taking moments about the apex for the
beam alone leaves its rotation completely unrestrained, so the beam can spin
about the apex: the assembly is unstable. (The gross count,
ten constraints against nine degrees of freedom, gives $+1$; that is two
redundancies in the legs less one mechanism in the beam, and is exactly the
case where a count must not be trusted.)
(c) Beam on two inclined pin-ended links and two fixed-base
columns. Counting the beam in three segments, $m = 7$, $j = 8$,
$r = 2 + 2 + 3 + 3 = 10$ and $c = 4$ (one moment release where each link and
each column meets the beam), so
$$i = 3(7) + 10 - 3(8) - 4 = \boxed{3}$$
The check is quicker the other way round: the beam pinned to two fixed-base
columns is already a rigid, once-redundant frame, and each of the two inclined
two-force links adds one more constraint. Indeterminate to the third
degree.
(d) Upper beam bearing on a lower beam. The upper beam has
a pin and a roller onto the lower beam, so three interface unknowns; the lower
beam has a pin and a roller to ground, so three external unknowns. Six unknowns
against six equations (three per beam) gives
$$i = 6 - 6 = \boxed{0}$$
The upper beam is solved first and its interface forces then load the lower
beam: statically determinate.
(e) Beam hung from two inclined links. Ground, two links
and the beam form a four-bar linkage. With $m = 3$, $j = 4$, $r = 4$ and
$c = 2$,
$$i = 3(3) + 4 - 3(4) - 2 = -1$$
so there is one degree of freedom left: the beam can swing. Symmetric loading
happens to be in equilibrium, but the structure is a mechanism and is
unstable.
(f) Trapezoidal truss with crossed diagonals in the centre
panel. Counting members: three bottom-chord panels, one top chord, two
end inclined members, two verticals and the two unconnected diagonals give
$m = 10$; there are $j = 6$ joints and $r = 3$, so
$$i = 10 + 3 - 2(6) = \boxed{1}$$
Every panel is triangulated, so the arrangement is sound:
indeterminate to the first degree — the second diagonal
of the centre panel is the redundant.
(g) Two-panel rectangular truss on two pins. Here
$m = 8$ (two top-chord panels, two bottom-chord panels, the middle and right
verticals, and the two diagonals; there is no member on the left face between
the two supports), $j = 6$ and $r = 4$, so
$$i = 8 + 4 - 2(6) = \boxed{0}$$
Stability has to be demonstrated because the right-hand panel carries no
diagonal of its own. Build the truss up joint by joint from the two pinned
joints: the upper middle joint is fixed by the upper-left chord and the
diagonal from the lower-left pin; the lower middle joint then follows from the
bottom chord and the middle vertical; the lower right joint follows from the
bottom chord and the long diagonal from the upper-left pin; and the upper right
joint follows from the top chord and the right vertical. All eight members and
all four joints are used exactly once, so the truss is rigid:
statically determinate.
Two of the seven are therefore mechanisms and, in an examination, they are
the marks most often lost: both (b) and (e) pass or nearly pass a numerical
count and fail on arrangement. Writing one sentence that names the free motion
— “the beam rotates about the apex pin”, “the linkage
swings” — is what earns the mark.
Question 1 — classification
Structure
Count
Classification
(a)
$r - 3 - c = 5 - 3 - 1 = 1$
Indeterminate, 1st degree
(b)
2 redundancies, 1 mechanism
Unstable (beam free to rotate about the apex pin)
(c)
$3m + r - 3j - c = 21 + 10 - 24 - 4 = 3$
Indeterminate, 3rd degree
(d)
$6 - 6 = 0$
Statically determinate
(e)
$9 + 4 - 12 - 2 = -1$
Unstable (four-bar linkage, one degree of freedom)