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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)

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. 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.

ABCDE1 m2 m6 m2 m
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.

0@A0@B+2.0 @C0@DIL: bending moment just right of B0+1.00@DIL: shear just right of B-0.5 @A0@B+1.0 @C0@DIL: horizontal reaction at E
  1. 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 $C\!-\!B=2\text{ m}$): $$\boxed{(\text{IL }M)_{\max}=+2.0\text{ m at }C}$$
  2. 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 $D$: $$(\text{IL }V)_{\max}=+1.0.$$
  3. 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 $$\boxed{(\text{IL }H_E)_{\max}=1.0\;(\text{load at }C)}.$$

5(b) — Moving vehicle on a truss (11 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. 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.

L1L2L3L4L5U1U2U3
Q5(b) — truss; the studied member $L_1\!-\!U_2$ is highlighted.
0+0.65 (T)-1.3 (C)-0.65 (C)0IL for force in L₁-U₂ (tension +, compression -)
Q5(b) — influence line for $L_1\!-\!U_2$ (ordinates in kN per unit load).
  1. 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 $x=8\text{ m}$.
  2. 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 $20\text{ m}$: $$F=100(-1.30)+100(-1.083)+50(-0.433)=\boxed{-260\text{ kN}\;(260\text{ kN compression})}.$$
  3. 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).