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16-Civ-A1 Elementary Structural Analysis · May 2015

Question 5 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, compound (Gerber) beams and three-hinged frames. Sign convention: sagging bending moment positive; upward reactions positive; member tension positive (T), compression negative (C).

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

Question 5: Influence lines (20 marks)

Part (a) — determinate Gerber beam

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.

123hinge2 m6 m2 m4 m2 m
Gerber beam: pin at 1 ($x=2$), rollers at 2 ($x=8$) and 3 ($x=14$), internal hinge at $x=10$, free ends at $x=0,16$.

Given. Supports at points 1 ($x=2$), 2 ($x=8$) and 3 ($x=14$); an internal hinge at $x=10$; free overhangs at both ends. Find. Three influence lines and their peak coefficients.

Approach. Place a unit load at position $p$, solve the determinate beam (using $M=0$ at the hinge as the fourth equation), and read the required response — the ordinate at each $p$ traces the influence line. Every influence line is piecewise-linear with break points at the supports, the hinge and the section.

  1. (i) Moment at point 2. Zero while the load is anywhere between supports 1 and 2, it grows linearly to $-2.0$ when the load sits over the hinge ($x=10$), returns to zero at support 3, and reaches $+1.0$ at the free right end. Peak $|\eta|=\boxed{2.0\ \text{m}}$.
  2. (ii) Moment at mid-span of 1–2 ($x=5$). A triangle peaking at $+1.5$ m under the section, negative ($-1.0$) over the overhangs and the hinge. Peak $|\eta|=\boxed{1.5\ \text{m}}$.
  3. (iii) Shear just left of support 2. Rises to $-1.0$ as the load approaches the section from the span side and falls off over the rest of the beam. Peak $|\eta|=\boxed{1.0}$.
−2.0+1.012h3IL — bending moment at point 2 (m); peak −2.0 at hinge
IL for bending moment at point 2.
+1.5−1.01mid23IL — bending moment at mid-span 1–2 (m); peak +1.5
IL for bending moment at mid-span of 1–2.
−1.0+0.3312h3IL — shear just left of support 2; peak magnitude 1.0
IL for shear just left of support 2.
ResponseMax $|\eta|$
$M$ at point 22.0 m (at the hinge)
$M$ at mid-span 1–21.5 m
$V$ just left of support 21.0

Part (b) — moving vehicle on a truss

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.

L1L2L3L4L5L6U1U2U3U44 m4 m4 m4 m4 m-0.583+0.5+0.333+0.167Influence line for U1–L3
Cambered truss loaded on the bottom chord; the influence line for member $U_1L_3$ is drawn below.

Given. Six bottom joints at $4$ m spacing (span $20$ m); the diagonal $U_1L_3$; a three-axle group $18$–$18$–$8$ kN with $4$ m then $2$ m spacing. Find. IL ordinates and the maximum $U_1L_3$ force.

  1. Ordinates. Placing a unit load successively at each bottom joint and solving for $U_1L_3$: $\eta_{L_1}=0,\ \eta_{L_2}=-\tfrac{7}{12}=-0.583,\ \eta_{L_3}=+0.500,\ \eta_{L_4}=+0.333,\ \eta_{L_5}=+0.167,\ \eta_{L_6}=0$; the line is linear between joints.
  2. Position for maximum tension. Slide the group so the two 18 kN axles straddle the peak: $18$ kN at $L_3$ ($\eta=0.500$), $18$ kN at $L_4$ ($\eta=0.333$) and $8$ kN at $x=14$ ($\eta=0.250$).
  3. Maximum force. $F_{\max}=18(0.500)+18(0.333)+8(0.250)=9+6+2=\boxed{17.0\ \text{kN (T)}}$. The largest compression the group can produce (over the negative lobe at $L_2$) is only $-10.5$ kN, so tension governs.
QuantityValue
IL ordinates $\eta_{L_2},\eta_{L_3},\eta_{L_4},\eta_{L_5}$−0.583, +0.500, +0.333, +0.167
Maximum force in $U_1L_3$17.0 kN tension