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07-Str-A4 · May 2014

Question 8 of 9: Slope-deflection with sidesway

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, May 2014 — 3 hours, closed book (approved Sharp or Casio calculator permitted). Nine questions over seven pages: Questions 1 and 2 are compulsory (8 and 12 marks), then any two of Questions 3, 4, 5 (16 marks each) and any two of Questions 6, 7, 8, 9 (24 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.

Throughout this paper end moments are quoted with the counter-clockwise-positive sign convention, the one that matches the standard six-degree-of-freedom stiffness element. In that convention 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 $M_{\text{sag}}(i)=-M_{ij}$, $M_{\text{sag}}(j)=+M_{ji}$. Mixing this with the clockwise-positive convention of some textbooks is the single most common source of clean-looking but wrong answers on this paper.

Question 8: Slope-deflection with sidesway (24 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 single beam carried by two 6 m columns, one hanging below the beam from an encastré base and one rising above it to an encastré head, with free overhangs at both ends and a UDL over the entire beam.

Given data
ItemValue
Beam ⑤–②–③–⑥2 m + 6 m + 2 m = 10 m, free at ⑤ and ⑥
Column ①–②6 m below the beam, encastré at ①
Column ③–④6 m above the beam, encastré at ④
Uniformly distributed load12 kN/m over the full 10 m
Flexural rigiditythe same $EI$ everywhere, inextensible
Sideswaynot prevented

Find. The member end moments, the sway, and the shear and bending moment diagrams with their extreme ordinates.

12 kN/m1234562 m6 m2 m6 m6 m
Question 8: sway frame with one column below and one above the beam.

Approach. Replace each overhang by the force and couple it applies to its joint, write slope-deflection equations for the beam and the two columns in terms of $\theta_2$, $\theta_3$ and the sway $\Delta$, and close the system with the storey-shear equation. Exploiting the frame’s point symmetry cuts the work in half.

  1. Convert the overhangs to joint actions. Each 2 m overhang carries $12(2)=24$ kN whose centroid is 1 m outboard, so it applies 24 kN downward and a 24 kN·m couple to its joint — counter-clockwise at ② and clockwise at ③.
  2. Identify the point symmetry. Rotating the frame $180^\circ$ about the beam mid-point maps ② onto ③ and ① onto ④, so the structure is symmetric under that map while the gravity load is anti-symmetric. The response is therefore anti-symmetric: $\theta_3=-\theta_2$ and $M_{34}=-M_{21}$.
  3. Write the slope-deflection equations. With $h=L=6$ m, the beam gives $M_{23}=\tfrac{2EI}{6}(2\theta_2+\theta_3)+36$ and the columns give $M_{21}=\tfrac{2EI}{6}(2\theta_2+3\Delta/6)$ and $M_{34}=\tfrac{2EI}{6}(2\theta_3-3\Delta/6)$, the opposite signs arising because one column hangs down and the other rises up.
  4. Impose the storey-shear equation. No horizontal load acts, so the two column shears must cancel: $M_{12}+M_{21}=M_{34}+M_{43}$. With $\theta_3=-\theta_2$ this collapses to $\theta_2=-2\Delta/h$ — and it also makes each column shear identically zero, so both columns carry a constant moment.
  5. Solve joint ②. Substituting $\theta_2=-2\Delta/h$ into $M_{21}+M_{23}=+24$ gives $2EI\Delta/h^{2}+4EI\Delta/(Lh)=\mathrm{FEM}-M_{\text{stub}}=36-24=12$, so with $L=h=6$ m, $M_{12}=2EI\Delta/h^{2}=4.0$ kN·m and $EI\Delta=72$ kN·m$^{3}$.
  6. Back-substitute. The beam end moments follow as $M_{23}=+28.0$ and $M_{32}=-28.0$ kN·m, and joint equilibrium checks: $-4.0+28.0=24.0$, the stub couple.

The sway and the joint rotations come out as

$$EI\Delta=72\ \text{kN}\cdot\text{m}^{3},\qquad EI\theta_2=-24\ \text{kN}\cdot\text{m}^{2}=-EI\theta_3$$

and the end moments are

$$\boxed{M_{12}=+4.0,\ M_{21}=-4.0,\ M_{23}=+28.0,\ M_{32}=-28.0,\ M_{34}=+4.0,\ M_{43}=-4.0\ \text{kN}\cdot\text{m}}$$

Because $M_{12}+M_{21}=0$ in both columns, neither column carries any shear and both horizontal reactions are zero: the frame sways 72/EI to one side yet transmits no horizontal force to the ground. The columns instead carry a constant 4.0 kN·m and an axial force of 60 kN — compression in the lower column, tension in the upper one, which literally hangs the right-hand end of the beam.

Bending moment along the beam 5-2-3-6 (sagging +ve)kN·m-28.0+26.0-28.05236
Question 8: bending moment along the beam, sagging positive.

On the beam the shear runs from $+36$ kN just right of ② to $-36$ kN just left of ③, with the 24 kN overhang shears outboard of each. The moment hogs $-24$ kN·m at each joint from the overhang alone, steps by the 4.0 kN·m column moment to $-28.0$ kN·m inside the main span, and reaches $-28.0+12(6)^{2}/8=+26.0$ kN·m at mid-span.

ResultValue
Sway of the beam$\Delta = 72/EI$ (rightwards)
Joint rotations$\theta_2=-24/EI$, $\theta_3=+24/EI$
Column moments (constant)4.0 kN·m in each
Column shears / horizontal reactions0
Column axial forces60 kN (lower in compression, upper in tension)
Beam end moments−28.0 kN·m at ② and ③
Maximum sagging moment+26.0 kN·m at mid-span
Maximum beam shear±36.0 kN at ② and ③
Overhang ordinates−24.0 kN·m and 24.0 kN shear at each stub root