16-Civ-B1 Advanced Structural Analysis · December 2019
Question 1 of 9: Statical indeterminacy and the minimum number of structural degrees of freedom
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examination, December 2019 —
16-Civ-B1 Advanced Structural Analysis, 3 hours, CLOSED BOOK (an
approved Casio or Sharp calculator only). Nine questions on seven pages:
Questions 1 and 2 are compulsory (8 and 12 marks); the candidate then answers
TWO of Questions 3, 4 or 5 (18 marks each) and TWO of Questions 6, 7, 8 or 9
(22 marks each), so six questions make a complete paper of 100 marks. Because
this set is a study resource, all nine questions are solved
here.
Reference texts. R. C. Hibbeler, Structural
Analysis, 10th ed. (Pearson) — Ch. 6 influence lines, Ch. 8–9
deflections and virtual work, Ch. 10 force (flexibility) method, Ch. 11
slope-deflection, Ch. 12 moment distribution, Ch. 15–16 matrix stiffness.
A. Kassimali, Structural Analysis, 6th ed. (Cengage) — Ch. 7
Castigliano and least work, Ch. 8 influence lines, Ch. 13 slope-deflection,
Ch. 17–18 matrix stiffness. A. Ghali, A. M. Neville and T. G. Brown,
Structural Analysis: A Unified Classical and Matrix Approach, 7th ed.
(CRC). Canadian context for the settlement question: NBC 2020 Part 4 and
CSA S6:19 treat differential support settlement as an imposed deformation to be
combined with the permanent loads, so the self-equilibrating moment set computed
in Question 6 is a real design action, not a curiosity.
Sign convention used throughout.
End moments are written counter-clockwise-positive on the member, which is the
convention that matches the standard six-degree-of-freedom element stiffness
matrix; the slope-deflection equation is then
$M_{ij} = \dfrac{2EI}{L}\left(2\theta_i + \theta_j - 3\psi_{ij}\right) +
\mathrm{FEM}_{ij}$ with $\psi$ the counter-clockwise chord rotation and, for a
downward UDL, $\mathrm{FEM}_{ij} = +wL^2/12$, $\mathrm{FEM}_{ji} = -wL^2/12$.
Ordinary sagging bending moments, which is what every diagram below
plots, are recovered as $M_{\text{sag}}(i) = -M_{ij}$ and
$M_{\text{sag}}(j) = +M_{ji}$. Mixing this with the clockwise-positive
convention of some textbooks produces clean-looking integers that are wrong.
Question 1: Statical indeterminacy and the minimum number of structural
degrees of freedom (8 marks)
Given. The three structures as drawn, all members
inextensible and rigidly jointed except where an internal hinge is shown; the
loading on each is as printed. No numerical dimensions are supplied —
none are needed, because both counts are purely topological.
Find. For each structure, the degree of statical
indeterminacy $r$ and the minimum number $k$ of joint displacements that a
slope-deflection analysis must carry.
Approach. Count $r$ from
$r = 3m + R - 3j - (\text{releases})$ on the rigid-jointed frame, then count
$k$ as (independent joint rotations that survive after every zero-moment end is
eliminated by a modified stiffness) plus (independent joint translations of the
inextensible bar linkage), reducing the second group by symmetry or antisymmetry
wherever the loading permits.
Set out the two counting rules once. For a planar
rigid-jointed structure with $m$ members, $j$ joints (support joints included)
and $R$ independent reaction components,
$$r = 3m + R - 3j - n_{\text{rel}}$$
where $n_{\text{rel}}$ is the number of released moments (one per internal
hinge between two members). For the kinematic count, the independent
translations are the mobility of the linkage formed by treating every
inextensible member as a rigid bar,
$$n_{\Delta} = 2n_{j} - \operatorname{rank}\!\left[\mathbf{C}\right],$$
$n_j$ being the number of joints free to translate and $\mathbf{C}$ the matrix
holding one compatibility row per bar (its unit-vector row) plus one row per
restrained support component acting on those joints. The independent
rotations are one per joint, less every end whose moment is known to be
zero — a pin or roller end of a member, an internal hinge, a free tip
— because such an end is condensed out with the modified stiffness
$3EI/L$ rather than carried as an unknown.
Structure (I): the hinge makes the beam determinate, but one
rotation still remains. The beam has a pin, two rollers and one
internal hinge: $m = 3$, $j = 4$, $R = 2 + 1 + 1 = 4$ and $n_{\text{rel}} = 1$,
so
$$r = 3(3) + 4 - 3(4) - 1 = \boxed{0}$$
— statically determinate. The kinematic count is not zero,
however. Rotations are eliminated at the pin support A (a member end with
$M = 0$), on both faces of the hinge H, and at the free-rotating roller end C.
The segment A–H then has zero moment at both ends, so it is a
simple span that merely delivers a shear to H, and the only unknown left is the
rotation of the interior roller B:
$$k_{\text{(I)}} = \boxed{1}$$
Structure (I): pin, internal hinge and two rollers under a full-length UDL. Determinate (r = 0), yet one joint rotation survives.
Structure (II): a stepped frame with three independent sways.
Numbering the joints 1 (left roller), 2 (left column head), 3 and 5 (the ends of
the lower connecting member), 4 and 8 (the fixed bases), 6 (right column head)
and 7 (right roller), there are $m = 7$ members, $j = 8$ joints and
$R = 1 + 3 + 1 + 3 = 8$ reaction components with no releases:
$$r = 3(7) + 8 - 3(8) = \boxed{5}$$
For the kinematics, six joints (1, 2, 3, 5, 6, 7) may translate; seven
inextensible bars and the two roller components give
$n_{\Delta} = 2(6) - 7 - 2 = \boxed{3}$. Physically those three are the sway of
the lower storey ($u_3 = u_5$) and the two independent horizontal movements of
the column heads 2 and 6, each of which drags its own overhanging beam and its
roller with it. Rotations survive at joints 2, 3, 5 and 6 — the moment is
zero at the roller ends 1 and 7, so those two are condensed out. Hence
$$k_{\text{(II)}} = 4 + 3 = \boxed{7}$$
Structure (II): stepped two-column frame, fixed bases, roller-ended upper beams. Five times redundant, seven degrees of freedom.
Structure (III): symmetry kills every translation. With
$m = 9$ members, $j = 10$ joints and four pinned bases ($R = 8$),
$$r = 3(9) + 8 - 3(10) = \boxed{5}$$
The bare linkage has $n_{\Delta} = 3$ independent translations (the three
horizontal movements $u_a = u_b$, $u_c = u_d$ and $u_e = u_f$, every vertical
being locked by an inextensible column). But the structure and the
loading are symmetric about the centre line, so every translation must be
antisymmetric: $u_c = u_d$ together with $u_c = -u_d$ forces $u_c = u_d = 0$,
and the same argument then zeroes the outer pair. No sway degree of freedom
survives. The six joint rotations pair off antimetrically
($\theta_f = -\theta_a$, $\theta_e = -\theta_b$, $\theta_d = -\theta_c$),
leaving three, and the four pinned bases are condensed out with $3EI/L$:
$$k_{\text{(III)}} = \boxed{3}$$
Structure (III): symmetric raised-centre frame on four pinned bases under symmetric UDLs. Symmetry removes every sway.
Marking the answer sheet. On (I) draw one curved arrow at
the interior roller. On (II) draw curved arrows at the four rigid joints 2, 3,
5 and 6 and three straight arrows: one on the lower member and one at each
column head. On (III) draw curved arrows at the three joints of the left-hand
half only, and write “symmetric — no sway, right half by
antimetry” beside it.