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 beam of constant $EI$, roller-supported at ① and encastré at ③, with an unloaded span ①–② and a uniformly distributed load over ②–③.
| Quantity | Symbol | Value |
|---|---|---|
| Unloaded span, roller to point ③/2 | $a$ | 3 m |
| Loaded span, point ② to the fixed end | $b$ | 6 m |
| Total span | $L=a+b$ | 9 m |
| Uniformly distributed load on $b$ | $w$ | 1.8 kN/m |
| Flexural rigidity | $EI$ | constant |
Find. The bending moment and the shear force carried by the beam at the built-in support ③.
Approach. The beam has four reaction components and three equations, so it is once redundant. Take the roller reaction $R_1$ as the redundant, write $M(x)$ in terms of it, and impose the least-work condition $\partial U/\partial R_1=0$, which is exactly the statement that the roller does not deflect.
The least-work condition is
$$\frac{\partial U}{\partial R_1}=\int_0^{L}\frac{M}{EI}\frac{\partial M}{\partial R_1}\,\mathrm{d}x=0\;\Longrightarrow\;R_1\int_0^{L}x^{2}\,\mathrm{d}x=\int_a^{L}\frac{w}{2}(x-a)^{2}x\,\mathrm{d}x$$and substituting the two evaluated integrals,
$$R_1=\frac{486}{243}=\boxed{2.00\text{ kN}\ \uparrow}$$With the redundant known the remaining actions follow from statics alone. At the built-in end,
$$M_3=R_1L-\frac{wb^{2}}{2}=2.00(9)-0.9(36)=\boxed{-14.4\text{ kN}\cdot\text{m}}$$ $$V_3=R_1-wb=2.00-10.8=\boxed{-8.8\text{ kN}}$$The negative signs mean hogging and a downward-to-the-left shear respectively, i.e. the support hogs the beam by 14.4 kN·m and carries 8.8 kN of the 10.8 kN applied. Along the span the moment peaks at $+7.11$ kN·m at $x=4.11$ m and passes through zero at $x=6.92$ m.
| Result | Value |
|---|---|
| Redundant roller reaction $R_1$ | 2.00 kN upward |
| Reaction at the fixed end $R_3$ | 8.80 kN upward |
| Bending moment at ③ | −14.4 kN·m (hogging) |
| Shear on the beam at ③ | −8.80 kN (8.80 kN magnitude) |
| Moment at ② | +6.00 kN·m sagging |
| Maximum sagging moment | +7.11 kN·m at $x=4.11$ m |
| Point of contraflexure | $x=6.92$ m from the roller |