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07-Str-A4 · December 2017

Question 2 of 9: Schematic shear force and bending moment diagrams (12 marks)

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

Notes on this paper

Paper format. National Examinations, December 2017 — 07-Str-A4 Advanced Structural Analysis. Three hours, CLOSED BOOK (an approved Sharp or Casio calculator is the only aid). Nine questions: answer BOTH #1 and #2, then ONLY TWO of #3, #4 or #5, and ONLY TWO of #6, #7, #8 or #9 — six questions constitute a complete paper. Marks are printed in the left margin: 8, 12, 16, 16, 16, 24, 24, 24, 24. All nine questions are worked below, because the complete set is the study resource rather than a sitting.

Reference texts. R. C. Hibbeler, Structural Analysis, 10th ed. (Pearson) — Ch. 4 shear and moment diagrams, Ch. 9–10 the force (flexibility) method, Ch. 11 slope-deflection, Ch. 14–16 the stiffness method; A. Kassimali, Structural Analysis, 6th ed. (Cengage) — Ch. 7 deflections by work and energy (Castigliano and least work), Ch. 13 slope-deflection, Ch. 16 sidesway frames; W. McGuire, R. H. Gallagher and R. D. Ziemian, Matrix Structural Analysis, 2nd ed., for the planar frame element stiffness matrix used as the independent check on every answer below. Member sizing that would follow such an analysis is governed in Canada by CSA A23.3:19, CSA S16:19 and CSA O86:19, with load combinations from NBCC 2020.

Check: sign convention, stated once and used throughout. End moments $M_{ij}$ are counter-clockwise positive on the member end — the convention that matches the six-degree-of-freedom planar frame element, so every result below can be reproduced by a direct-stiffness solution. The chord rotation is $\psi_{ij}=\left[(\mathbf{D}_{j}-\mathbf{D}_{i})\cdot\mathbf{n}\right]/L$ with $\mathbf{n}$ the member axis turned $+90^\circ$; the fixed-end moment of a downward UDL is $\mathrm{FEM}_{ij}=+wL^{2}/12$ at the $i$ end; and the ordinary sagging moment is $M_{\text{sag}}(i)=-M_{ij}$, $M_{\text{sag}}(j)=+M_{ji}$. Mixing this with the clockwise-positive convention produces clean-looking integers that are wrong.

Question 2: Schematic shear force and bending moment diagrams (12 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.

Given. Structure (a) is a beam with an $L/4$ overhang at each end carrying a tip load $P=wL/4$, a pin at A, a roller at B one span $L$ away with a UDL $w$ over that span only, and a rigid joint C a further $L$ along, propped by a fixed-base column of height $L/2$. Structure (b) is a symmetric portal on fixed bases whose beam is lifted at mid-span by a jack; no dimensions are printed on it.

Question 2(a) — data as printed
ItemValue
Overhang at each end$L/4$
Tip load at each end$P=wL/4$ downward
Span A–B, carrying the UDL $w$$L$
Span B–C, unloaded$L$
Column C–D, fixed at D$L/2$

Find. The shape of the shear force and bending moment diagrams for both structures, with the maximum and minimum ordinates marked.

w P = wL/4 P = wL/4 L/4 L L L/4 L/2 A B C D
Q2(a): pin at A, roller at B, rigid joint C propped by a fixed-base column of height L/2; UDL w between A and B and tip loads P = wL/4 on both overhangs.

Approach. Show first that neither structure can sway, so each reduces to a small slope-deflection problem in joint rotations alone; the ordinates then follow from statics on each member.

  1. (a) Show that nothing translates. The beam is horizontal and inextensible and A is a pin, so $u_{C}=u_{A}=0$; the column is vertical and inextensible on a fixed base, so $v_{C}=0$. With the roller holding B the only unknowns are $\theta_{A},\theta_{B},\theta_{C}$, and the frame behaves as a continuous beam carrying a rotational spring $4EI/(L/2)=8EI/L$ at C.
  2. (a) Remove the overhangs as determinate cantilevers. Each delivers a known end moment to the beam line: $$M_{\text{overhang}}=-P\,\frac{L}{4}=-\frac{wL}{4}\cdot\frac{L}{4}=-\frac{wL^{2}}{16}$$ that is, $wL^{2}/16$ hogging at A and again at C.
  3. (a) Solve the three joint equations. Writing $M_{ij}=(2EI/L_{ij})(2\theta_{i}+\theta_{j})+\mathrm{FEM}_{ij}$ for the four members and imposing $\sum M_{ij}=0$ at A, B and C gives end moments that are exact fractions of $wL^{2}$: $$M_{\text{sag}}(A)=-\frac{wL^{2}}{16},\qquad M_{\text{sag}}(B)=-\frac{3wL^{2}}{64},\qquad M_{\text{sag}}(C)^{-}=0$$
  4. (a) Locate the peak sagging moment. The shear in span A–B starts at $33wL/64$ and falls at rate $w$, so it vanishes $33L/64$ from A and $$M_{\max}=-\frac{wL^{2}}{16}+\frac{33wL}{64}\cdot\frac{33L}{64}-\frac{w}{2}\left(\frac{33L}{64}\right)^{2}=\boxed{0.0704\,wL^{2}}$$

One feature of structure (a) deserves to be pointed out rather than smoothed over. The bending moment in span B–C falls to exactly zero at joint C, because the column absorbs the whole $wL^{2}/16$ delivered by the right-hand overhang. The diagram therefore steps at C from zero on the beam side to $wL^{2}/16$ hogging on the overhang side, and that step is the column moment — a diagram drawn without it will not satisfy joint equilibrium. The column also pushes horizontally, so the pin at A carries a $3wL/16$ horizontal reaction even though every applied load is vertical.

SFD BMD wL/4 33wL/64 31wL/64 3wL/64 wL/4 wL^2/16 0.0704 wL^2 3wL^2/64 wL^2/16 zero at C
Q2(a): shear force and bending moment diagrams for the beam line, as multiples of wL and wL squared (sagging plotted below the axis).

Structure (b) is easier, because a jack under mid-span is statically equivalent to an upward force $P$ there, and both structure and load are symmetric.

  1. (b) Reduce by symmetry. Symmetry forbids sway and gives $\theta_{C}=-\theta_{B}$, so the beam term collapses to $2EI\theta_{B}/L$ and the single joint equation at B reads $$\left(\frac{4EI}{h}+\frac{2EI}{L}\right)\theta_{B}=\frac{PL}{8}$$
  2. (b) Recover the ordinates. Substituting back, $$M_{BA}=\boxed{\frac{PL^{2}}{4(2L+h)}},\qquad M_{AB}=\frac{M_{BA}}{2},\qquad M_{\text{mid}}=\frac{PL}{4}-M_{BA}$$ with column shear $V=(M_{AB}+M_{BA})/h=3PL^{2}/[8h(2L+h)]$ and beam shear $P/2$ either side of the jack.

No dimensions are printed on structure (b), so the closed forms above are the real answer. The numerical illustration on the sketch adopts the drawn proportions $L=6$ m and $h=4$ m; the shapes, the zeros and the point of contraflexure at one third of the column height above the base do not depend on that choice at all.

JACK LIFTS BEAM P L h B C A D
Q2(b): symmetric portal on fixed bases; a jack under mid-span lifts the beam, which is equivalent to an upward force P at mid-span.
0.9375P (hogging) 0.5625P 0.28125P beam shear ±0.5P, column shear 0.2109P
Q2(b): bending moment diagram plotted on the tension side. The beam ends and column tops carry 0.5625P (L = 6 m, h = 4 m adopted), mid-span 0.9375P hogging, bases 0.28125P.
Check: adopted dimensions in 2(b). The source figure carries no dimensions and no jack travel, so the answer is given as closed forms in $L$, $h$ and the jack force $P$, with $L=6$ m and $h=4$ m used only to put numbers on the sketch. If the jack travel $\Delta$ is the known quantity instead, the same analysis gives $\Delta=1.96875\,P/EI$ for those proportions, so $P=0.5079\,EI\Delta$.
Question 2 — diagram ordinates
LocationShearBending moment (sagging positive)
(a) left overhang$-wL/4$$0$ at the tip to $-wL^{2}/16$ at A
(a) span A–B$+33wL/64$ falling to $-31wL/64$$-wL^{2}/16$, peak $+0.0704\,wL^{2}$, $-3wL^{2}/64$ at B
(a) span B–C$+3wL/64$ constant$-3wL^{2}/64$ at B to $0$ at C
(a) right overhang$+wL/4$$-wL^{2}/16$ at C to $0$ at the tip
(a) column C–D$3wL/16$ constant$wL^{2}/16$ at C and $wL^{2}/32$ at D, on opposite faces
(a) reactions$R_{A}=49wL/64$, $R_{B}=17wL/32$, $R_{D}=13wL/64$, with a $3wL/16$ horizontal pair and $M_{D}=wL^{2}/32$
(b) beam$\pm P/2$ends $+PL^{2}/[4(2L+h)]$; mid-span $PL/4$ less that value, hogging
(b) columns$3PL^{2}/[8h(2L+h)]$top $PL^{2}/[4(2L+h)]$, base half of it, on opposite faces