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16-Civ-A1 Elementary Structural Analysis · May 2014

Question 6 of 8: Influence lines

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

Notes on this paper

Reference texts: R.C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy, method of joints/sections, virtual-work deflections, moment distribution, slope–deflection, influence lines; A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges and compound structures. Sign convention: sagging bending moment positive; upward reactions positive; tension member forces positive (T), compression negative (C).

The paper directs candidates to answer Q1–Q4, then one of Q5/Q6 and one of Q7/Q8. For completeness all eight questions are worked here.

Question 6: Influence lines (20 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.

6(a) — Truss influence lines (top-chord loading)

U₁L₁U₂L₂U₃6 m6 m6 m6 m6(a): Warren truss, 4.5 m deep, top panel points U₁,U₂,U₃ at 12 m spacing; unit load travels the top chord.

Given. Truss $U_1(0,4.5),L_1(6,0),U_2(12,4.5),L_2(18,0),U_3(24,4.5)$ m; pin at $U_1$, roller at $U_3$; a unit downward load moves along the top chord (applied at $U_1,U_2,U_3$).

Find. Influence lines and peak coefficients for $U_1U_2$ and $U_2L_2$.

  1. Method. Place the unit load at each top panel point and solve the truss; the ordinate is linear between panel points. Load at $U_1$ or $U_3$ (over a support) gives zero in both bars.
  2. $U_1U_2$. Ordinate at $U_2$ $= -0.667$; peak $|\eta| = \boxed{0.667\ \text{(C)}}$ at mid-span.
  3. $U_2L_2$. Ordinate at $U_2$ $= -0.833$; peak $|\eta| = \boxed{0.833\ \text{(C)}}$ at mid-span.
IL U₁U₂-0.667 (C) IL U₂L₂-0.833 (C)

6(b) — Shear influence line + moving vehicle

2 m6 m9 m2 m6(b): pin at 2 m, roller at 17 m, 2 m overhangs; section A–A at 8 m (6 m right of the pin).

Section A–A is marked at $x=8$ m. Vehicle: 100 kN — 1.5 m — 100 kN — 3 m — 50 kN.

Given. Beam with pin at $x=2$, roller at $x=17$, free 2 m overhangs each end; shear wanted at A–A, $x=8$ m. Idealised vehicle 100, 100, 50 kN at 1.5 m and 3 m spacing crosses the span.

Find. Influence line for $V_{A}$ and the maximum shear at A–A as the vehicle crosses.

  1. Influence line. With span $a=15$ m between supports and A–A 6 m right of the pin, $\eta_V = +0.6$ just right of A and $-0.4$ just left of A, zero at each support, and $\pm0.133$ at the overhang tips.
  2. Position for maximum. Place the two 100 kN axles on the steep positive branch just right of A: at $x=8,\,9.5$ ($\eta=0.600,0.500$) and the 50 kN at $x=12.5$ ($\eta=0.300$).
  3. Maximum shear. $V_A = 100(0.600)+100(0.500)+50(0.300) = \boxed{125\ \text{kN}}$. (The largest negative, loads on the left branch, is only $-50$ kN.)
IL shear at A-A+0.60-0.40+0.13-0.13
QuantityValue
6(a) $U_1U_2$ peak IL0.667 (C) at mid-span
6(a) $U_2L_2$ peak IL0.833 (C) at mid-span
6(b) IL$_{V}$ at A–A$+0.60$ (right) / $-0.40$ (left)
6(b) max shear at A–A125 kN