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 symmetric-looking gable frame with equal rafters, propped at its apex by a fixed-base column, with short free stubs beyond each springing and a UDL over the right-hand half.
| Item | Value |
|---|---|
| Stub ①–② and ④–⑤ | 2 m each (free ends at ① and ⑤) |
| Rafter horizontal projection ②–③ and ③–④ | 6 m each |
| Apex rise above the springing level | 2.5 m |
| Rafter length | $\sqrt{6^{2}+2.5^{2}}=6.5$ m |
| Apex ③ to the fixed base ⑥ | 6.5 m (4.0 m below the springing level) |
| Support at ② | roller (vertical only) |
| Support at ④ | pin |
| Support at ⑥ | encastré |
| UDL from ③ to ⑤ | 20 kN/m on the horizontal projection (8 m) |
| Flexural rigidity | the same $EI$ in every member |
Find. All member end moments, hence the shear force and bending moment diagrams with their maximum and minimum ordinates.
Approach. Prove first that inextensibility forbids sway, so the analysis carries only joint rotations; replace the two free stubs by their statically equivalent joint actions; then write slope-deflection equations for the rafters and the column and solve the two independent joint-moment equations.
The fixed-end moment of the loaded rafter is
$$\mathrm{FEM}_{34}=\frac{w\,L_{\text{proj}}^{2}}{12}=\frac{20(6)^{2}}{12}=+60\text{ kN}\cdot\text{m},\qquad \mathrm{FEM}_{43}=-60\text{ kN}\cdot\text{m}$$and solving the two joint equations gives the end moments
$$\boxed{M_{32}=-21.0,\quad M_{34}=+49.0,\quad M_{36}=-28.0,\quad M_{43}=-40.0,\quad M_{63}=-14.0\ \text{kN}\cdot\text{m}}$$Converted to ordinary sagging moments, rafter ②–③ runs from zero at the roller to $-21.0$ kN·m at the apex, while rafter ③–④ starts at $-49.0$ kN·m on the other side of the same joint. The 28.0 kN·m step between them is the column moment, and that step is joint equilibrium rather than an error. Between the two ends the rafter carries the free parabola of the projected UDL, peaking at $+45.6$ kN·m at $x=11.08$ m.
The reactions follow from member equilibrium and confirm the analysis: $R_2=-3.50$ kN (a hold-down at the roller), $V_4=101.2$ kN, $H_4=-6.46$ kN, and at the column base $V_6=62.3$ kN, $H_6=+6.46$ kN with $M_6=-14.0$ kN·m. Vertical equilibrium closes on the applied $20(8)=160$ kN and the two horizontal reactions cancel, as they must under purely vertical loading.
| Member | End moment (CCW +ve) | Comment |
|---|---|---|
| ②–③ | $M_{23}=0$, $M_{32}=-21.0$ | moment-free at the roller (stub carries nothing) |
| ③–④ | $M_{34}=+49.0$, $M_{43}=-40.0$ | loaded rafter; max sagging $+45.6$ at $x=11.08$ m |
| ③–⑥ (column) | $M_{36}=-28.0$, $M_{63}=-14.0$ | shear $6.46$ kN, axial $62.3$ kN |
| ④–⑤ (stub) | $M_{45}=+40.0$, $M_{54}=0$ | determinate cantilever, shear 40 kN |
| Reactions | $R_2=-3.50$, $V_4=101.2$, $V_6=62.3$ kN | $\sum V=160$ kN = $20(8)$ |