16-Civ-A1 Elementary Structural Analysis · December 2019
Question 5 of 8: Influence lines and a moving vehicle (18 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper: National Exams — December 2019, 16-Civ-A1 Elementary Structural Analysis (closed book, 3 h; approved Casio or 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 and stability (Ch. 2), method of joints and sections (Ch. 3), shear and moment diagrams (Ch. 4), influence lines (Ch. 6), virtual-work deflections (Ch. 8–9), moment distribution (Ch. 11); A. Kassimali, Structural Analysis (6th ed., Cengage) — internal hinges, compound (Gerber) beams, three-hinged frames; J. C. McCormac, Structural Analysis: Using Classical and Matrix Methods (4th ed., Wiley) — Maxwell’s reciprocal theorem. Canadian practice for these actions is codified in CSA S16 and CSA S6, but this paper is pure analysis and invokes no code clauses.
Sign convention. Upward reactions positive; sagging bending moment positive (tension on the underside), hogging negative; member axial force tension positive (T), compression negative (C).
Check — figure reading. Support types are read from the printed symbols: rollers are a triangle over two wheels, pins a plain triangle, and internal hinges open circles.
Question 5 — Influence lines and a moving vehicle (18 marks)
Given. A 20 m compound beam with a pin at A $(x=0)$, an internal hinge at C $(x=8)$, and rollers at D $(x=10)$ and E $(x=20)$. Point B is at $x=4$ m. Spacings are A–B 4 m, B–C 4 m, C–D 2 m and D–E 10 m. A unit load travels from A to E.
Find. Influence lines for $M_B$, for shear immediately left of C, and for $M_D$, each with its largest absolute ordinate.
Q5(a) — 20 m compound beam: pin at A, internal hinge at C, rollers at D and E.
Approach. Split the beam at the hinge into two determinate parts and track how each carries a unit load. Segment 1 (A to C) is effectively a simple span propped by the pin at A and by the hinge; segment 2 (C to E) is a beam on rollers at D and E with a 2 m overhang reaching back to the hinge.
With $r = 2+1+1 = 4$ and one hinge, $\mathrm{DSI} = 4-3-1 = 0$, so the beam is determinate and every influence line is made of straight segments.
(i) Influence line for $M_B$. When the unit load stands at $a$ on segment 1, that segment behaves as a simple span of 8 m between A and the hinge, so $$\eta_{M_B}(a) = \frac{a(8-4)}{8} = \frac{a}{2} \ (a \le 4), \qquad \eta_{M_B}(a) = \frac{4(8-a)}{8} \ (4 \le a \le 8)$$ When the load stands beyond the hinge, segment 1 carries nothing at all — the load is taken entirely by the rollers at D and E — so the ordinate is zero from C to E. The peak sits under B: $$\eta_{\max} = \frac{4 \times 4}{8} = \boxed{2.00\ \text{m}}$$
IL for the bending moment at B: a simple-span triangle on A–C only; the whole of C–E is zero because the load is then carried entirely by the D–E segment.
(ii) Influence line for shear immediately left of C. For a load at $a$ on segment 1, the reaction at A is $(8-a)/8$ and the section at $x=8^-$ has the whole unit load to its left, so $$\eta_{V}(a) = \frac{8-a}{8} - 1 = -\frac{a}{8}$$ This falls linearly from 0 at A to $-1$ immediately left of the hinge. Once the load passes the hinge the ordinate drops instantly to zero and stays there. The largest absolute value is $$|\eta|_{\max} = \boxed{1.00}$$ reached with the load standing just to the left of C.
IL for shear just left of C. It falls linearly to −1 at C and is identically zero beyond the hinge.
(iii) Influence line for $M_D$. D is a support, so the only way to bend it is to load the 2 m overhang between the hinge and D, or to load segment 1, which delivers its hinge reaction onto the tip of that overhang. For a unit load at $a$ on segment 1 the hinge force is $a/8$ pressing down at $x=8$, giving $$\eta_{M_D}(a) = -\frac{a}{8}(10-8) = -\frac{a}{4}$$ which reaches $-2$ when $a=8$. Between C and D the load acts directly on the overhang, and $\eta_{M_D} = -(10-a)$, running from $-2$ at C back to 0 at D. Beyond D the ordinate is zero, because the stretch between the hinge and D is then unloaded. The extreme value is $$\eta_{\max} = \boxed{-2.00\ \text{m}}$$ and the influence line is entirely negative — $M_D$ can only ever hog.
IL for the bending moment at D: purely hogging, peaking at −2 m when the load stands at the hinge C.
5(b)
Given. A 16 m compound beam: pin at A $(x=0)$, roller at C $(x=8)$, internal hinge at D $(x=10)$ and roller at E $(x=16)$. Point B lies 6 m from A, that is 2 m to the left of C. The vehicle is three point loads — 40 kN, 40 kN and 20 kN — spaced 2 m between the two 40 kN axles and 4 m between the second 40 kN axle and the 20 kN axle, travelling left to right.
Find. The influence line for shear at B, and the largest shear the vehicle can produce there.
Q5(b) — 16 m compound beam. B (6 m from A) is the section whose shear is required.
Approach. Build the influence line segment by segment, then place the axles so the sum $\sum P_i\eta_i$ is greatest — for a shear influence line with a unit step, that means putting the heaviest axle immediately on the steeper side of the section.
Ordinates for a load on span A–C. Segment 1 spans A to the hinge D with supports at A and C, so with the load at $a$ the reaction $R_A = (8-a)/8$ and $$\eta_{V_B}(a) = \frac{8-a}{8} - 1 = -\frac{a}{8} \ (a < 6), \qquad \eta_{V_B}(a) = \frac{8-a}{8} \ (a > 6)$$ Immediately left of B the ordinate is $-6/8 = -0.75$ and immediately right of it $+2/8 = +0.25$, the unit step across the section. It falls to zero at the roller C.
Ordinates for a load on the overhang and the suspended span. Between C and the hinge D the ordinate continues linearly to $-0.25$ at D. Beyond the hinge, a unit load at $a$ on D–E delivers $(16-a)/6$ down onto the tip of the overhang at $x=10$, which gives $$\eta_{V_B}(a) = -\frac{1}{4}\cdot\frac{16-a}{6}$$ running from $-0.25$ at D back to zero at E. The governing ordinate is $\boxed{-0.75}$ just left of B.
IL for shear at B, showing the unit step across the section and the reversed lobe produced by the suspended span D–E.
Position the vehicle for maximum effect. The influence line is negative almost everywhere and steepest approaching B from the left, so the worst case puts a 40 kN axle exactly at B (just on its left, where $\eta = -0.75$) and the other axles where the ordinates are still negative. Testing every position, the governing arrangement has the leading 20 kN axle at $x = 10$ m, so the two 40 kN axles stand at $x=4$ m and $x=6$ m.
Evaluate the shear. Reading the ordinates $\eta(4) = -0.50$, $\eta(6^-) = -0.75$ and $\eta(10) = -0.25$, $$V_B = \sum P_i \eta_i = 40(-0.50) + 40(-0.75) + 20(-0.25)$$ $$V_B = -20 - 30 - 5 = \boxed{-55.0\ \text{kN}}$$ so the largest shear at B is 55 kN, acting in the negative sense. Sweeping the vehicle numerically across the whole structure confirms no other position beats it.