Question 8 of 9: Slope-deflection analysis of a sway frame (22 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 07-Str-A4 Advanced Structural Analysis, National Examination, December 2014 — 3 hours, closed book (approved Sharp or Casio calculator permitted). Nine questions over six pages: Questions 1 and 2 are compulsory (12 and 8 marks), then any two of Questions 3, 4, 5 (18 marks each) and any two of Questions 6, 7, 8, 9 (22 marks each). Six questions constitute a complete paper and total 100 marks; marks are printed in the left margin. All nine questions are solved here, because the set is a study resource rather than a three-hour sitting.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 6 (influence lines), Ch. 9 (deflections by energy methods), Ch. 10 (force/flexibility method), Ch. 11 (slope-deflection).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3 (determinacy and stability), Ch. 8 (influence lines for floor-beam systems), Ch. 13 (least work), Ch. 15–16 (slope-deflection with and without sidesway).
A. Ghali, A. M. Neville and T. G. Brown, Structural Analysis: A Unified Classical and Matrix Approach, 7th ed. — Ch. 4 (force method), Ch. 5 (lack of fit and support movement).
W. McGuire, R. H. Gallagher and R. D. Ziemian, Matrix Structural Analysis, 2nd ed. — Ch. 4–5 (member stiffness, assembly, kinematic constraints).
CSA S6:19 Canadian Highway Bridge Design Code and NBCC 2020 — the Canadian codes that these analysis methods feed; no code check is required by this paper.
Sign convention used throughout. End moments are counter-clockwise positive, the convention that matches the standard six-degree-of-freedom stiffness element. In it the slope-deflection equation is
the chord rotation is $\psi_{ij}=\bigl[(\mathbf{d}_j-\mathbf{d}_i)\cdot\mathbf{e}_2\bigr]/L$ with $\mathbf{e}_2$ the member axis turned $+90^\circ$, the fixed-end moment of a downward UDL is $\mathrm{FEM}_{i}=+wL^{2}/12$ and $\mathrm{FEM}_{j}=-wL^{2}/12$, and the ordinary sagging bending moment is recovered as $M_{\text{sag}}(i)=-M_{ij}$ and $M_{\text{sag}}(j)=+M_{ji}$. Every translation degree of freedom is closed with the virtual-work statement
in which $\mathbf{F}$ are the equivalent nodal loads and $\mathbf{d}^{*}$, $\psi^{*}$ belong to the unit sway pattern. Mixing this with the clockwise-positive convention of some textbooks produces clean-looking but wrong answers, which is the single most common failure on this subject.
All work below uses the drawing.
Question 8: Slope-deflection analysis of a sway frame (22 marks)
Given. A three-member frame built in at joints (1) and (4), with two inclined members and one vertical member, loaded only at the joints.
Given data
Quantity
Value
Joint (1)
fixed; take as the origin
Joint (2)
6 m across, 2.5 m below (1)
Joint (3)
6.5 m directly below (2)
Joint (4)
fixed, 6.5 m below (1)
Member lengths
all three are 6.5 m ($6$–$2.5$–$6.5$ triangles)
Loads
20 kN downward at (2); 7.2 kN horizontal at (2) and at (3)
Find. Shear force and bending moment diagrams for all three members, with extreme ordinates labelled.
Question 8: all loads act at joints, so there are no fixed-end moments; every ordinate arises from the sway and the two joint rotations.
Approach. Use inextensibility to reduce six joint displacements to one sway parameter, write the three chord rotations in terms of it, and close the system with two joint equations and one virtual-work sway equation.
Reduce the kinematics. Both inclined members are parallel (each rises 2.5 m over 6 m), so each forces its joint to move perpendicular to itself: $v_2=2.4u_2$ and $v_3=2.4u_3$. The vertical member is inextensible, so $v_2=v_3$ and hence $u_2=u_3=\Delta$. Three unknowns remain:
$$\boxed{\Delta,\ \theta_2,\ \theta_3}$$
Chord rotations. Resolving the joint displacements onto each member's transverse axis,
$$\psi_{12}=\psi_{43}=\frac{2.6\Delta}{6.5}=0.4\Delta,\qquad \psi_{23}=\frac{u_3-u_2}{6.5}=0$$
The vertical member has no chord rotation at all — a useful simplification that follows from $u_2=u_3$.
Slope-deflection equations. Writing $k=2EI/6.5$ and $X=3\psi_{12}$, and remembering $\theta_1=\theta_4=0$ and zero fixed-end moments,
$$M_{12}=k(\theta_2-X),\quad M_{21}=k(2\theta_2-X),\quad M_{23}=k(2\theta_2+\theta_3)$$
$$M_{32}=k(2\theta_3+\theta_2),\quad M_{43}=k(\theta_3-X),\quad M_{34}=k(2\theta_3-X)$$
Joint equilibrium. $M_{21}+M_{23}=0$ and $M_{32}+M_{34}=0$ give
$$4\theta_2+\theta_3=X,\qquad 4\theta_3+\theta_2=X$$
Subtracting shows $\theta_2=\theta_3=\theta$, and then $5\theta=X$, so $\theta=X/5$.
Sway equation by virtual work. Give the frame a unit sway ($\Delta^{*}=1$, so $\mathbf{d}^{*}_2=\mathbf{d}^{*}_3=(1,\,2.4)$ and $\psi^{*}_{12}=\psi^{*}_{43}=0.4$). The applied loads do virtual work
$$\sum \mathbf{F}\cdot\mathbf{d}^{*}=(7.2)(1)+(-20)(2.4)+(7.2)(1)=-33.6$$
and the end moments do internal work $\bigl[(M_{12}+M_{21})+(M_{43}+M_{34})\bigr](0.4)=0.8k(3\theta-2X)$, so
$$0.8k(3\theta-2X)-33.6=0$$
Solve. Substituting $\theta=X/5$ makes $3\theta-2X=-1.4X$, hence
$$-1.12\,kX=33.6\;\Longrightarrow\;\boxed{kX=-30\ \text{kN}\cdot\text{m}}$$
The rotations and sway themselves are not required for the diagrams, because every end moment is a multiple of $kX$.
End moments. Back-substituting $\theta=0.2X$,
$$M_{12}=-0.8kX=+24.0,\quad M_{21}=-0.6kX=+18.0,\quad M_{23}=+0.6kX=-18.0$$
$$M_{32}=-18.0,\quad M_{34}=+18.0,\quad M_{43}=+24.0\ \text{kN}\cdot\text{m}$$
$$\boxed{\text{base moments }24.0\ \text{kN}\cdot\text{m at (1) and (4)};\quad \text{joint moments }18.0\ \text{kN}\cdot\text{m at (2) and (3)}}$$
Member shears. No member carries a span load, so each shear is constant and equal to the sum of its end moments divided by its length:
$$V_{12}=V_{43}=\frac{24.0+18.0}{6.5}=6.4615\ \text{kN},\qquad V_{23}=\frac{18.0+18.0}{6.5}=5.5385\ \text{kN}$$
Reactions and global checks. Resolving the member end forces at the two fixed bases,
$$\text{At (1): } H=12.7385\ \text{kN (leftward)},\ V=12.3077\ \text{kN},\ M=24.0\ \text{kN}\cdot\text{m}$$
$$\text{At (4): } H=1.6615\ \text{kN (leftward)},\ V=7.6923\ \text{kN},\ M=24.0\ \text{kN}\cdot\text{m}$$
$$\textstyle\sum F_x:\;-12.7385-1.6615+7.2+7.2=0,\qquad \sum F_y:\;12.3077+7.6923-20=0\quad\checkmark$$
Both fixed bases finish with the same moment, 24.0 kN·m, and both interior joints with 18.0 kN·m. That is a consequence of the frame's point symmetry about the mid-point of member (2)–(3): the geometry maps onto itself under a half-turn, so the two inclined members must respond identically.
Question 8: bending moment, member by member (sagging positive within each member's own axis). Every ordinate is either 24.0 or 18.0 kN·m.
Question 8: member shears. Each is constant because no member carries a load along its length.