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16-Civ-B1 Advanced Structural Analysis · December 2014

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. National Examination, December 2014, 98-Civ-B1 Advanced Structural Analysis — 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.

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

$$M_{ij}=\frac{2EI}{L}\bigl(2\theta_i+\theta_j-3\psi_{ij}\bigr)+\mathrm{FEM}_{ij}$$

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

$$\sum_{\text{members}}\bigl(M_{ij}+M_{ji}\bigr)\,\psi^{*}_{ij}\;+\;\sum \mathbf{F}\cdot\mathbf{d}^{*}=0$$

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)

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. 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
QuantityValue
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 lengthsall three are 6.5 m ($6$–$2.5$–$6.5$ triangles)
Loads20 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.

20 kN 7.2 kN 7.2 kN (1) (2) (3) (4) 6.5 m 6.5 m 6 m 2.5 m
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.

  1. 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: $$\boxed{\Delta,\ \theta_2,\ \theta_3}$$
  2. 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 $u_2=u_3$.
  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, $$M_{12}=k(\theta_2-X),\quad M_{21}=k(2\theta_2-X),\quad M_{23}=k(2\theta_2+\theta_3)$$ $$M_{32}=k(2\theta_3+\theta_2),\quad M_{43}=k(\theta_3-X),\quad M_{34}=k(2\theta_3-X)$$
  4. 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 $\theta=X/5$.
  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 $$0.8k(3\theta-2X)-33.6=0$$
  6. 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 $kX$.
  7. End moments. Back-substituting $\theta=0.2X$, $$M_{12}=-0.8kX=+24.0,\quad M_{21}=-0.6kX=+18.0,\quad M_{23}=+0.6kX=-18.0$$ $$M_{32}=-18.0,\quad M_{34}=+18.0,\quad M_{43}=+24.0\ \text{kN}\cdot\text{m}$$ $$\boxed{\text{base moments }24.0\ \text{kN}\cdot\text{m at (1) and (4)};\quad \text{joint moments }18.0\ \text{kN}\cdot\text{m at (2) and (3)}}$$
  8. 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: $$V_{12}=V_{43}=\frac{24.0+18.0}{6.5}=6.4615\ \text{kN},\qquad V_{23}=\frac{18.0+18.0}{6.5}=5.5385\ \text{kN}$$
  9. 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.

Bending moment, member by member (sagging +, kN·m) (1)-(2) | (2)-(3) | (4)-(3) M -24.00 +18.00 -18.00 +18.00
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.
Member shear (constant on each member, kN) (1)-(2) | (2)-(3) | (4)-(3) V +6.4615 -5.5385 +6.4615
Question 8: member shears. Each is constant because no member carries a load along its length.
Question 8 — complete results
MemberLengthMoment at the first endMoment at the second endShearAxial
(1)–(2)6.5 m24.0 kN·m at (1)18.0 kN·m at (2)6.4615 kN16.49 kN compression
(2)–(3)6.5 m18.0 kN·m at (2)18.0 kN·m at (3)5.5385 kN7.69 kN tension
(4)–(3)6.5 m24.0 kN·m at (4)18.0 kN·m at (3)6.4615 kN4.49 kN compression
Reaction at (1)$H=12.7385$ kN, $V=12.3077$ kN, $M=24.0$ kN·m
Reaction at (4)$H=1.6615$ kN, $V=7.6923$ kN, $M=24.0$ kN·m