NivaarExam PrepOfficial exam papers ↗

24-Bld-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

National Exams May 2018 — 07-BLD-A1 Elementary Structural Analysis, 3 hours, closed book (approved Casio/Sharp calculator only). Answer ALL of Questions 1–5; answer ONLY ONE of Questions 6, 7 or 8 (this solution set, per pipeline convention, answers all three optional questions).

Reference texts: Hibbeler, Structural Analysis, 10th ed.; Kassimali, Structural Analysis, 6th ed.

Question 5: 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.

(a) Influence lines for the frame at B, and the horizontal reaction at E

Given. Top beam A–B–C–D with A at 1 m left of B (free tip), C a hinge 2 m right of B, D a pin 6 m further right (8 m from B); a vertical leg drops 2 m from B to pin E. A unit load travels along A–D.

Find. Influence lines for the moment and shear just right of B, and for the horizontal reaction at E; the peak ordinate of each.

ABCDE1 m2 m6 m2 m
Frame (a): overhang A–B, hinge at C, pin at D; leg B–E to a pin support.

Approach. With a hinge at C, split into body 1 (A–B–C–leg–E) and body 2 (C–D); solve each body’s reactions as a function of the unit-load position $$x$$ (measured from B), then cut just right of B for V and M.

  1. Load on A–C $$(-1\le x\le2)$$: body 2 (C–D, unloaded, pin at D only) forces zero vertical hinge shear, so $$R_{y,E}=1$$ (constant) and, taking moments of body 1 about E(0,−2): $$R_{x,E}=x/2$$.
  2. Load on C–D $$(2\le x\le8)$$: body 2 alone (simple span C–D=6 m) gives the hinge shear $$=(8-x)/6$$, which becomes $$R_{y,E}=R_{x,E}=(8-x)/6$$ from body 1 (no load on it, so its own moment sum about E must vanish, forcing $$R_{x,E}=R_{y,E}$$).
  3. Horizontal reaction at E — influence line. Linear from $$-0.5$$ at A $$(x=-1)$$ up to $$\boxed{+1.0}$$ at C $$(x=2)$$, then back down to 0 at D $$(x=8)$$. Maximum $$|R_{x,E}|=\boxed{1.0}$$, at C.
  4. Shear/moment just right of B — cutting the A–B overhang + leg free body: with $$R_{y,E}=1$$ whenever the load sits on A–C, $$V_{B^+}=0$$ for $$x<0$$ (load left of B not yet in this free body) and $$V_{B^+}=-1$$ for $$0, tapering linearly to 0 at D. $$M_{B^+}$$ runs linearly from $$\boxed{-2}$$ at A, through 0 at B, up to $$\boxed{+2}$$ at C, back down to 0 at D.
Influence lineShapeMax |ordinate|
Rx,E−0.5 (A) → +1.0 (C) → 0 (D)1.0, at C
V just right of B0 (A–B) → −1.0 (B–C) → 0 (D)1.0, from B to C
M just right of B−2 (A) → 0 (B) → +2 (C) → 0 (D)2.0, at A and at C

(b) Influence line for L1–U2 and the critical vehicle position

Given. A 24 m simply-supported truss, pin at L1, roller at L5; panels of 6 m, height 5 m; the diagonal L1U2 spans 2 panels (a counter-diagonal). Idealized vehicle: 100 kN, 100 kN, 50 kN, spaced 2 m then 6 m, travelling left to right.

Find. The influence-line ordinates for L1U2, and the maximum compression and tension it experiences as the vehicle crosses.

L1L2L3L4L5U1U2U3idealized vehicle: 100 kN, 100 kN, 50 kN (2 m, 6 m spacing) →
Truss (b): pin–roller span with the counter-diagonal L1–U2 whose influence line is requested.

Approach. Cut the panel between U1/L2 and U2, severing U1U2, L2L3 and L1U2. With a unit load anywhere on the span, use whichever free body (left of the cut or right of it) does not contain the load, so only the known reaction appears; the influence line is then a straight line between panel points 0–6–12–24.

  1. Unit load at 0≤x≤6 (right free body, unloaded): $$F_{L1U2}=\dfrac{13}{5}R_{L5}=\dfrac{13}{5}\cdot\dfrac{x}{24}=\dfrac{13x}{120}$$ giving $$F(0)=0,\ F(6)=\boxed{+0.65}$$ (tension).
  2. Unit load at 12≤x≤24 (left free body, unloaded): $$F_{L1U2}=-\dfrac{13}{5}R_{L1}=-\dfrac{13}{5}\cdot\dfrac{24-x}{24}$$ giving $$F(12)=\boxed{-1.30}$$ (compression), $$F(24)=0$$. Between x=6 and x=12 the influence line is the straight line joining these two panel-point values.
  3. Sweep the vehicle (100–100–50 kN, spacings 2 m/6 m) across the span, evaluating $$\Sigma(\text{load}\times\text{ordinate})$$ at every position where a wheel sits on a panel point (the governing positions for a piecewise-linear IL). Placing the 50 kN wheel at x=6 (ordinate +0.65) and the middle 100 kN wheel at x=12 (ordinate −1.30) simultaneously — possible because those panel points are exactly the vehicle’s 6 m axle spacing apart — with the lead 100 kN at x=14 (ordinate $$-13(10)/120=-1.083$$): $$F_{max,C}=100(-1.083)+100(-1.30)+50(0.65)=\boxed{-205.8\text{ kN (compression)}}$$
  4. Maximum tension: keep the vehicle’s rear wheel off the (only 6 m wide) positive zone: lead 100 kN at x=6 (+0.65), middle 100 kN at x=4 $$(13(4)/120=+0.433)$$, rear 50 kN at x=−2 (off the span, no contribution): $$F_{max,T}=100(0.65)+100(0.433)=\boxed{+108.3\text{ kN (tension)}}$$
QuantityValue
IL peak (tension), at x=6 m+0.65
IL peak (compression), at x=12 m−1.30
Max compression, L1U2205.8 kN
Max tension, L1U2108.3 kN