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16-Civ-B1 Advanced Structural Analysis · May 2013

Question 6 of 9: Two-span beam with a settled central support

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. 98-Civ-B1 Advanced Structural Analysis, National Examinations, May 2013 — 3 hours, closed book (an approved Sharp or Casio calculator is permitted). Nine questions are printed. The candidate must answer Question 1 and Question 2, then two of Questions 3–5 and two of Questions 6–9 — six questions constitute a complete paper (8 + 12 + 2 × 16 + 2 × 24 = 100 marks). Marks are shown in the left margin of the paper. All nine questions are solved below, because the set is intended as a study resource rather than as a three-hour sitting.

Reference texts.

Sign conventions used throughout. Slope-deflection end moments $M_{ij}$ are the moments the joint applies to the member, clockwise positive; joint rotations $\theta$ are clockwise positive; the chord rotation $\psi_{ij}=\Delta/L$ is positive when the member chord rotates clockwise. Bending moment diagrams are plotted with sagging positive, so that the sagging moment at end $i$ of member $ij$ is $+M_{ij}$ and at end $j$ it is $-M_{ji}$. All members are inextensible unless stated otherwise, so axial deformation contributes nothing to the compatibility equations.

Question 6: Two-span beam with a settled central support (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.

Given data
Span 1–28 m, carrying $w_1 = 4\text{ kN/m}$
Span 2–38 m, carrying $w_2 = 8\text{ kN/m}$
Supportspin at 1, roller at 2, roller at 3; ends 1 and 3 are simple, so $M_1=M_3=0$
Support movementsupport 2 sits $\delta = 64\text{ mm} = 0.064\text{ m}$ below supports 1 and 3
Flexural rigidity$EI = 2.0\times10^{4}\ \text{kN}\cdot\text{m}^{2}$

Find. The bending moment over the central support, the three reactions, and the shear and bending moment diagrams with the maximum and minimum ordinates in each span.

4 kN/m 8 kN/m 8 m 8 m 1 2 3 64 mm low SFD +17.500 -14.500 +30.500 -33.500 BMD +38.28 +70.14 +12.00
Q6 — two-span beam, its shear force diagram and its bending moment diagram. The 64 mm settlement is large enough to remove the hogging moment at the central support entirely.

Approach. Superpose two effects that the slope-deflection equations handle in one pass: the fixed-end moments from the two distributed loads, and the chord rotations produced by the 64 mm settlement. Impose $M_{12}=M_{32}=0$ at the simple ends and $M_{21}+M_{23}=0$ at the central support.

  1. Chord rotations and fixed-end moments. With $v_2=-0.064\text{ m}$ and $v_1=v_3=0$, $$\psi_{12}=\frac{v_1-v_2}{8}=+0.008,\qquad \psi_{23}=\frac{v_2-v_3}{8}=-0.008 .$$ The fixed-end moments for a uniformly loaded span are $\mp wL^{2}/12$: $$\text{FEM}_{12}=-\frac{4(8)^{2}}{12}=-21.33,\quad \text{FEM}_{21}=+21.33,\quad \text{FEM}_{23}=-\frac{8(8)^{2}}{12}=-42.67,\quad \text{FEM}_{32}=+42.67\ \text{kN}\cdot\text{m}.$$
  2. Assemble the three equations. With $k=2EI/8=5000\ \text{kN}\cdot\text{m}$, $$M_{12}=k\!\left(2\theta_1+\theta_2-0.024\right)-21.33=0,\qquad M_{32}=k\!\left(2\theta_3+\theta_2+0.024\right)+42.67=0,$$ $$M_{21}+M_{23}=k\!\left(2\theta_2+\theta_1-0.024\right)+21.33 +k\!\left(2\theta_2+\theta_3+0.024\right)-42.67=0 .$$
  3. Solve for the rotations. The two end conditions give $\theta_1=\tfrac12(0.028267-\theta_2)$ and $\theta_3=\tfrac12(-0.032533-\theta_2)$; substituting into the joint equation leaves $15000\,\theta_2 = 32.0$, so $$\boxed{\theta_2 = +0.002133\ \text{rad},\qquad \theta_1=+0.013067,\qquad \theta_3=-0.017333\ \text{rad}.}$$
  4. Find the moment over the central support. $$M_{21}=5000\!\left(0.004267+0.013067-0.024\right)+21.33=-12.0\ \text{kN}\cdot\text{m},$$ and $M_{23}=+12.0\ \text{kN}\cdot\text{m}$, so the two balance as required. In the sagging-positive convention the bending moment over support 2 is $$\boxed{M_2 = -M_{21} = +12.0\ \text{kN}\cdot\text{m}\quad\text{(sagging).}}$$ It is worth separating the two contributions: the loads alone would give $M_2=-(w_1+w_2)L^{2}/16=-48.0\ \text{kN}\cdot\text{m}$ (hogging), while the settlement alone gives $+3EI\delta/L^{2}=+60.0\ \text{kN}\cdot\text{m}$ (sagging). The settlement therefore reverses the sign of the support moment.
  5. Reactions from span statics. Taking moments on each span with the end moments known, $$R_1=\frac{w_1L^{2}/2+M_2}{L}=\frac{128+12}{8}=17.50\ \text{kN},\qquad V_{2}^{-}=w_1L-R_1=14.50\ \text{kN},$$ $$V_{2}^{+}=\frac{w_2L^{2}/2-M_2}{L}=\frac{256-12}{8}=30.50\ \text{kN},\qquad R_3=w_2L-V_2^{+}=33.50\ \text{kN},$$ so $R_2 = 14.50+30.50 = 45.00\ \text{kN}$. Check: $17.50+45.00+33.50 = 96.0\ \text{kN} = 4(8)+8(8)$.
  6. Locate the zero-shear points and the sagging peaks. In span 1–2, $V=17.50-4x=0$ at $x=4.375\text{ m}$, where $$M_{\max}=17.50(4.375)-2(4.375)^{2}=\boxed{+38.28\ \text{kN}\cdot\text{m}} .$$ In span 2–3, measuring $x'$ from support 2, $V=30.50-8x'=0$ at $x'=3.8125\text{ m}$, where $$M_{\max}=12.0+30.50(3.8125)-4(3.8125)^{2}=\boxed{+70.14\ \text{kN}\cdot\text{m}} .$$
  7. Read off the extreme ordinates. Because the support moment has become sagging, the bending moment is positive over the whole 16 m: there is no point of contraflexure anywhere, and the minimum bending moment in each span is the zero at its outer simple support. The shear extremes are $+17.50$ and $-14.50\text{ kN}$ in span 1–2, and $+30.50$ and $-33.50\text{ kN}$ in span 2–3.
Final results — Question 6
QuantitySpan 1–2Span 2–3
Maximum shear+17.50 kN at support 1+30.50 kN at support 2
Minimum shear−14.50 kN at support 2−33.50 kN at support 3
Zero-shear station4.375 m from support 13.8125 m from support 2
Maximum bending moment+38.28 kN·m+70.14 kN·m
Minimum bending moment0 at support 10 at support 3
Bending moment over support 2+12.0 kN·m sagging (−48.0 from load, +60.0 from settlement)
Reactions$R_1 = 17.50$, $R_2 = 45.00$, $R_3 = 33.50$ kN