16-Civ-A1 Elementary Structural Analysis · December 2018
Question 3 of 8: Vertical deflections of a non-prismatic beam
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper: National Exams — December 2018, 16-Civ-A1 Elementary Structural Analysis (closed book, 3 h; approved Casio/Sharp calculator permitted). Six questions constitute a complete paper: answer Q1–Q5 and one of Q6/Q7/Q8. For completeness all eight questions are worked here.
Reference texts: R. C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy (Ch. 2), method of joints & sections (Ch. 3), shear & moment diagrams (Ch. 4), influence lines (Ch. 6), virtual-work deflections (Ch. 8–9), moment distribution (Ch. 11); A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound (Gerber) beams, three-hinged & indeterminate frames.
Sign convention. Upward reactions positive; sagging bending moment positive (tension on the underside), hogging negative; member axial force tension positive (T), compression negative (C).
These A1 papers are defined entirely by their figures, so every structure is redrawn to scale below.
Question 3: Vertical deflections of a non-prismatic beam (18 marks)
Given. Beam $A(0)\!-\!B(6)\!-\!C(12)\!-\!D(13.5\text{ m})$: pin at $A$, roller at $C$, free tip at $D$. Stiffness $A\!-\!B=EI_0$ and $B\!-\!C\!-\!D=2EI_0$ with $EI_0=18\,000\text{kN}\cdot\text{m}^2$; a single $24\text{ kN}\downarrow$ at the overhang tip $D$. Find. The vertical deflections $\delta_B$ and $\delta_D$.
Question 3 — simple span $A\!-\!C$ with a $1.5\text{ m}$ loaded overhang (heavier line $=2EI_0$).
Reactions (determinate). $\sum M_{A}=0:\;R_{C}(12)=24(13.5)\Rightarrow \boxed{R_C=27\text{ kN}}$; then $\boxed{R_A=24-27=-3\text{ kN}}$ — the pin at $A$ pulls down (uplift), because the overhang load lifts the back span.
Real moment diagram. $M(x)=-3x$ on $[0,12]$ (so $M_B=-18,\;M_C=-36\text{kN}\cdot\text{m}$, all hogging) and $M=24x-324$ on the overhang, returning to $0$ at $D$.
Unit-load (virtual-work) integrals, split at every $EI$ break. $\delta=\displaystyle\int \frac{M\,m}{EI(x)}\,dx$. For $\delta_B$ place a unit load at $B$: $\int_0^6\frac{(-3x)(0.5x)}{EI_0}+\int_6^{12}\frac{(-3x)(6-0.5x)}{2EI_0}=\frac{-108-108}{EI_0}$.
Deflection at $B$. $\displaystyle \delta_B=\frac{-216}{18\,000}=-0.0120\text{ m}=\boxed{12\text{ mm }\uparrow}$ — the negative sign means the back span rises, consistent with the uplift reaction.
Deflection at $D$. With a unit load at the tip, $m=-0.125x$ on $[0,12]$ and $m=x-13.5$ on the overhang; the three integrals give $\dfrac{27+94.5+13.5}{EI_0}=\dfrac{135}{18\,000}=0.0075\text{ m}=\boxed{7.5\text{ mm }\downarrow}$.