16-Civ-A1 Elementary Structural Analysis · May 2018
Question 5 of 8: Influence lines
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper: National Exams — May 2018, 16-Civ-A1 Elementary Structural Analysis (closed book, 3 h; 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 / slope–deflection (Ch. 11–12); A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound (Gerber) beams, 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 5: Influence lines (20 marks)
5(a) — Influence lines for a propped, hinged frame (9 marks)
Given. Top beam $A(0)\!-\!B(1)\!-\!C(3)\!-\!D(9\text{ m})$ with a free left overhang $A\!-\!B$, an internal hinge at $C$ and a pin (roller-type vertical support) at $D$; a $2\text{ m}$ column $B\!-\!E$ rigidly built into the beam at $B$ and pinned at $E$. Find. the three influence lines.
Q5(a) — frame; unit load travels along $A\!-\!D$.
Approach. With the hinge at $C$ and pins at $D$ and $E$ the frame is determinate, so each influence line is piecewise-linear; place a unit load at the control points ($A,B,C,D$) and solve by statics.
Moment just right of $B$. Zero on the overhang and at $B$ and $D$; it peaks when the load sits at the hinge $C$ (lever $C\!-\!B=2\text{ m}$): $$\boxed{(\text{IL }M)_{\max}=+2.0\text{ m at }C}$$
Shear just right of $B$. Zero for load on the overhang, a unit step at $B$, then $+1$ across $B\!-\!C$ falling linearly to zero at $D$: $$(\text{IL }V)_{\max}=+1.0.$$
Horizontal reaction at $E$. The overhang bends the column ($H_E=-0.5$ with the load at $A$); the maximum occurs with the load at $C$, where the moment $2\text{ kN}\cdot\text{m}$ over the $2\text{ m}$ column gives $$\boxed{(\text{IL }H_E)_{\max}=1.0\;(\text{load at }C)}.$$
Given. Deck truss, five bottom panels of $6\text{ m}$ (pin $L_1$, roller $L_5$), height $5\text{ m}$; the long diagonal $L_1\!-\!U_2$ crosses the vertical $U_1\!-\!L_2$ without connecting. Find. IL ordinates and the extreme member forces.
Q5(b) — truss; the studied member $L_1\!-\!U_2$ is highlighted.
Q5(b) — influence line for $L_1\!-\!U_2$ (ordinates in kN per unit load).
IL ordinates. A vertical section between $L_2$ and $L_3$ cuts the horizontal chords and $L_1\!-\!U_2$ (vertical component $5/13$); $\Sigma F_y$ of the left free body gives, panel by panel: $$\boxed{\eta_{L_1},\eta_{L_2},\eta_{L_3},\eta_{L_4},\eta_{L_5}=0,\;+0.65,\;-1.30,\;-0.65,\;0}$$ (tension +). The line crosses zero at $x=8\text{ m}$.
Maximum compression. Cluster the two $100\text{ kN}$ loads over the negative lobe near $L_3$ (at $x=12$ and $14\text{ m}$) with the $50\text{ kN}$ trailing at $20\text{ m}$: $$F=100(-1.30)+100(-1.083)+50(-0.433)=\boxed{-260\text{ kN}\;(260\text{ kN compression})}.$$
Maximum tension. Place the two $100\text{ kN}$ loads over the positive lobe near $L_2$ ($x=4$ and $6\text{ m}$), the $50\text{ kN}$ off the effective span: $$F=100(0.433)+100(0.65)\approx\boxed{+108\text{ kN}\;(108\text{ kN tension})}.$$
Check: the schematic influence line printed on the exam paper is a qualitative guide; the ordinates above (and the two extreme positions).