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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)

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. 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.

  1. 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.
  2. 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: $$k_{\text{(I)}} = \boxed{1}$$
  3. wAHBCinternal hinge at H r = 0 (determinate), k = 1
    Structure (I): pin, internal hinge and two rollers under a full-length UDL. Determinate (r = 0), yet one joint rotation survives.
  4. 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 $$k_{\text{(II)}} = 4 + 3 = \boxed{7}$$
  5. w2wP2P123567r = 5 k = 4 rotations + 3 sways = 7
    Structure (II): stepped two-column frame, fixed bases, roller-ended upper beams. Five times redundant, seven degrees of freedom.
  6. 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 $3EI/L$: $$k_{\text{(III)}} = \boxed{3}$$
  7. wwwacdfsymmetric structure + symmetric load: r = 5, k = 3
    Structure (III): symmetric raised-centre frame on four pinned bases under symmetric UDLs. Symmetry removes every sway.
  8. 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.
StructureStatical indeterminacy r RotationsTranslations (sways) Minimum d.o.f. k
(I) continuous beam with one hinge0 (determinate) 101
(II) stepped two-column frame543 7
(III) symmetric raised-centre frame530 3
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