Question 2 of 9: Influence lines for the shear immediately left of support B
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Examinations — December 2018. 07-Str-A4, Advanced Structural
Analysis. Three hours, closed book (approved Casio or Sharp calculator only).
Nine questions on seven pages: Questions 1 and 2 are compulsory (12 and 8 marks);
the candidate then answers TWO of Questions 3, 4 or 5 (18 marks each) and TWO of
Questions 6, 7, 8 or 9 (22 marks each), so six questions make a complete paper of
100 marks. Because this set is a study resource, all nine questions are
solved here.
Reference texts. R. C. Hibbeler, Structural Analysis,
10th ed. (Pearson) — Ch. 6 influence lines, Ch. 8–9 deflections and
virtual work, Ch. 10 force (flexibility) method, Ch. 11 slope-deflection, Ch. 12
moment distribution, Ch. 15–16 matrix stiffness. A. Kassimali,
Structural Analysis, 6th ed. (Cengage) — Ch. 7 Castigliano and
least work, Ch. 8 influence lines, Ch. 13 slope-deflection, Ch. 17–18 matrix
stiffness. A. Ghali, A. M. Neville and T. G. Brown, Structural Analysis: A
Unified Classical and Matrix Approach, 7th ed. (CRC). Canadian context for
the support-settlement questions: NBC 2020 Part 4 and CSA S6:19 treat differential
settlement as an imposed deformation to be combined with the permanent loads, so
the self-equilibrating moment sets computed in Questions 1(c), 5 and 7 are real
design actions, not curiosities.
Check: representative dimensions in Questions 1
and 2. The source prints no dimensions on any of the five
structures in Questions 1 and 2 — they are labelled “schematically
show”. Every shape, every zero and every discontinuity below is
dimension-independent and is what the marker is looking for. To put real numbers
on the ordinates, representative dimensions have been adopted in the drawn
proportions and are stated with each part; they are declared here rather than
presented as data read off the paper.
Question 2: Influence lines for the shear immediately left of support B (8 marks)
Given. Two three-support beams of the same overall layout.
In (a) an internal hinge is drawn between A and B, which makes the beam
determinate; (b) has no hinge and is one degree indeterminate. No dimensions are
printed; for the ordinates below the drawn proportions are taken as span AB = 10 m
with the hinge 7.0 m from A, and span BC = 10 m.
Find. The influence line for the shear force on the section
immediately to the left of support B in each beam, and the ordinate of
largest absolute value on each.
Structure (a) — roller, internal hinge, roller, pin. The hinge is what makes the beam determinate.
Approach. Work from first principles rather than from a
remembered picture: the shear just left of B equals the sum of the upward forces
acting to the left of that section, which for both beams is
\(V = R_{A} - 1\) when the unit load stands left of the section and
\(V = R_{A}\) when it stands right of it. Everything then follows from the
influence line for \(R_{A}\).
(a) Split the determinate beam at the hinge. Segment A–H
is a simple span carried by the roller at A and by the hinge force at H; segment
H–B–C is a beam on B and C with the overhang H–B. The decisive
consequence is that a load anywhere to the right of the hinge delivers nothing
to A: with no load on A–H the hinge force is zero, so
\(R_{A} = 0\).
(a) Unit load between A and the hinge. The simple span gives
\(R_{A} = (x_{h} - x)/x_{h}\), so
$$\eta(x) = R_{A} - 1 = -\dfrac{x}{x_{h}}$$
a straight line from 0 at A to \(\boxed{-1.000}\) at the hinge.
(a) Unit load between the hinge and B. Now \(R_{A} = 0\) and
the load is still left of the section, so \(\eta = 0 - 1 = -1.000\) for every
position: the influence line runs flat at −1.000 from
the hinge to B. This plateau is the feature that distinguishes the determinate
answer, and it is the part most often drawn as a continuing ramp.
(a) Unit load in span BC. The load is now right of the section
and \(R_{A}\) is still zero, so \(\eta \equiv 0\) throughout BC. The
influence line jumps by exactly 1.000 across support B, as it must for a section
adjacent to a support.
Influence line (a). Maximum absolute ordinate 1.000, held constant from the hinge to the section; identically zero in span BC.
Structure (b) — the same supports without the hinge, so one degree indeterminate.
(b) Choose the redundant. Take the interior reaction
\(R_{B}\) as the redundant on a simple beam of span \(S = L_{1} + L_{2}\). With
\(\delta_{BB} = L_{1}^{2}L_{2}^{2}/(3EIS)\) and the standard mid-point deflection
formula for \(\delta_{Bx}\), the reaction influence line comes out in closed
form. For the load in span AB, with \(\xi = x/L\) and equal spans,
$$R_{A}(\xi) = 1 - \tfrac{5}{4}\xi + \tfrac{1}{4}\xi^{3}$$
(b) Convert to shear. Left of the section
\(\eta = R_{A} - 1 = -\tfrac{5}{4}\xi + \tfrac{1}{4}\xi^{3}\), a cubic that
falls monotonically from 0 at A to
$$\eta(B^{-}) = \boxed{-1.000}$$
That value is exact for any span ratio: with the unit load standing directly over B
the reaction at A vanishes, so the shear just left of the section is
\(0 - 1\).
(b) The far span reverses. Loading BC lifts the far end, so
\(R_{A}\) — and with it \(\eta\) — goes negative again. Writing
\(s\) for the distance from C and \(\sigma = s/L_{2}\),
$$\eta = \dfrac{L_{2}^{2}}{2L_{1}S}\left(\sigma^{3} - \sigma\right)$$
which for equal spans reduces to \(\tfrac{1}{4}(\sigma^{3}-\sigma)\) and
reaches its extremum at \(\sigma = 1/\sqrt{3}\):
$$\eta_{\min,BC} = -0.0962 \ \text{at}\ 0.577L_{2} = 5.77\ \text{m from C}$$
(b) Compare the two answers. Both beams give the same
governing ordinate, −1.000 immediately left of B, because that
value is a statement of statics at the section and cannot depend on the
redundancy. What the redundancy changes is the shape: (a) is piecewise
straight with a plateau and a dead span, (b) is cubic everywhere and spills a small
reversed lobe into the far span. Reporting only the number without that
distinction throws away most of the eight marks.
Influence line (b). The cubic reaches −1.000 at the section and carries a small secondary lobe of −0.0962 into span BC.