16-Civ-B1 Advanced Structural Analysis · May 2014
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Examination, May 2014, 98-Civ-B1 Advanced Structural Analysis — 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 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.
| Item | Value |
|---|---|
| Beam ⑤–②–③–⑥ | 2 m + 6 m + 2 m = 10 m, free at ⑤ and ⑥ |
| Column ①–② | 6 m below the beam, encastré at ① |
| Column ③–④ | 6 m above the beam, encastré at ④ |
| Uniformly distributed load | 12 kN/m over the full 10 m |
| Flexural rigidity | the same $EI$ everywhere, inextensible |
| Sidesway | not prevented |
Find. The member end moments, the sway, and the shear and bending moment diagrams with their extreme ordinates.
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.
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.
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.
| Result | Value |
|---|---|
| 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 reactions | 0 |
| Column axial forces | 60 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 |