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07-Str-A4 · May 2018

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 Examination, May 2018, 07-Str-A4 Advanced Structural Analysis — 3 hours, CLOSED BOOK (an approved Casio or Sharp calculator is permitted). Nine questions: #1 and #2 are compulsory (8 and 12 marks), then TWO of #3, #4, #5 (16 marks each) and TWO of #6, #7, #8, #9 (24 marks each); six questions constitute a complete paper (100 marks). All nine are solved here, because the set is a study resource rather than a timed sitting.

Reference texts.

Sign convention used throughout. Member end moments $M_{ij}$ are counter-clockwise positive on the member end, which is the convention that matches the standard 6-degree-of-freedom element stiffness matrix and the counter-clockwise-positive joint rotations that Question 9 asks for. With that convention the fixed-end moment of a downward uniform load is $M^{F}_{ij}=+wL^{2}/12$ at the near end, the chord rotation is $\psi_{ij}=\left[(\mathbf{D}_{j}-\mathbf{D}_{i})\cdot\mathbf{e}_{2}\right]/L$ with $\mathbf{e}_{2}$ the member axis turned $+90^{\circ}$, and the ordinary sagging moments plotted on the diagrams are $M_{\text{sag}}(i)=-M_{ij}$ and $M_{\text{sag}}(j)=+M_{ji}$. Where a step of the working is quicker in the clockwise-positive (Hibbeler) form the sign is stated explicitly.

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. Two unloaded-dimension “schematic” structures. Part (a) carries the bay lengths listed below; part (b) prints no dimensions at all, so the drawn proportions are adopted.

Given data — Question 2(a)
Stationx (m)Feature
left tip0free end of a 3 m overhang, UDL w
roller3vertical restraint only
hinge8internal moment release ("TYPICAL HINGE")
column A head10rigid joint; column pinned at its base
column B head18rigid joint; column pinned at its base; UDL w runs from 10 m to 18 m
built-in end24fixed support

Find. The shear force and bending moment diagrams of both structures, with the ordinates that the shapes turn on.

wwhinge3 m5 m2 m8 m6 mh
Question 2(a): the hinge at x = 8 m splits a determinate front end from a four-times indeterminate frame behind it.
Check: the two columns in part (a) are drawn without a dimension. Scaling the printed figure against the 3 m bay gives about 4.8 m, so h = 5 m is adopted and every ordinate quoted for the indeterminate part is stated as a multiple of $w$ on that basis. Nothing on the determinate front end (0 m to 8 m) depends on $h$. Part (b) prints no dimensions either; the drawn proportions give a height within 8 % of the span, so h = L is adopted and the answer is given in closed form so that any other ratio can be substituted.

Approach. Use the hinge to peel off the statically determinate front end by hand, then carry the remaining four-times indeterminate frame with the displacement method; for (b) apply the slope-deflection equations to the prescribed support movement.

  1. (a) Count the indeterminacy. The frame has no closed loop, so $$\text{DSI}=r-3-c=(1+3+2+2)-3-1=4,$$ with $r$ the roller, the built-in end and the two pinned column bases, and $c=1$ the moment condition at the hinge. Four redundants means the back half must be solved by a stiffness (or flexibility) analysis — but the front half need not be.
  2. (a) The hinge isolates a determinate front end. Take the free body from the tip to the hinge and set the moment there to zero. The overhang resultant $3w$ acts $6.5\text{ m}$ from the hinge and the roller is $5\text{ m}$ from it: $$R_{3}(5)-3w(6.5)=0\;\Rightarrow\;\boxed{R_{3}=3.90\,w}$$ so this reaction, and everything to the left of the hinge, is independent of the column height.
  3. (a) Front-end ordinates. The shear grows linearly to $V(3^{-})=-3.00\,w$ and jumps to $V=+0.90\,w$ at the roller, holding that value all the way to the hinge; the moment reaches $M(3)=-w(3)^{2}/2=-4.50\,w$ at the roller and climbs linearly to zero at the hinge, $$M(8)=-4.50\,w+0.90\,w(5)=0\;\checkmark$$ The hinge therefore hands a shear of $0.90\,w$ (and no moment) to the frame behind it.
  4. (a) Solve the four-times indeterminate remainder. With $h=5$ m the stiffness solution gives the beam moments $+1.80\,w$ just left of the first column and $-2.65\,w$ just right of it — a genuine step of $4.45\,w$, which is exactly the moment carried into the column head. The same thing happens at the second column: $-5.15\,w$ on the left, $-2.71\,w$ on the right, a step of $2.44\,w$. The largest sagging moment in the loaded 8 m bay is $$M_{\max}=+4.15\,w \text{ at } x=13.68\text{ m},$$ and the built-in end finishes at $+1.36\,w$.
  5. (a) Assemble the diagrams. The shear runs $0\to-3.00\,w$ over the overhang, jumps to $+0.90\,w$ at the roller and stays there through the hinge to the first column, jumps to $+3.69\,w$ where that column delivers its reaction, falls linearly under the UDL to $-4.31\,w$ at the second column, and jumps to a constant $+0.68\,w$ over the last bay. Every jump equals the reaction or column force applied there, and the vertical reactions sum to $11\,w$, the total load — the arithmetic check worth doing before the diagram is drawn.
  6. (b) Kinematics of the settling portal. The columns are vertical and inextensible, so $v_{B}=v_{A}=0$ and $v_{C}=v_{D}=-\Delta$; the beam is horizontal and inextensible, so $u_{B}=u_{C}=\delta$, one unknown sway. Writing $\rho=\delta/L$ and $\tau=\Delta/L$, the chord rotations in the clockwise-positive form are $\psi_{AB}=\psi_{DC}=\rho$ and $\psi_{BC}=\tau$.
  7. (b) Slope-deflection and joint equilibrium. With $k=2EI/L$ and $\theta_{A}=\theta_{D}=0$ (both bases are fixed and neither rotates), joint equilibrium at $B$ and $C$ reads $$4\theta_{B}+\theta_{C}=3(\rho+\tau),\qquad 4\theta_{C}+\theta_{B}=3(\rho+\tau),$$ whose difference gives $\theta_{B}=\theta_{C}=\theta$ and therefore $\theta=\tfrac{3}{5}(\rho+\tau)$.
  8. (b) The storey-shear equation closes it. There is no horizontal load, so the two column shears must sum to zero, which requires $(M_{AB}+M_{BA})+(M_{DC}+M_{CD})=0$, i.e. $\theta=2\rho$. Combining with the joint result, $$1.4\rho=0.6\tau\;\Rightarrow\;\rho=\tfrac{3}{7}\tau,\qquad \theta=\tfrac{6}{7}\tau.$$
  9. (b) Back-substitute. Every one of the six end moments comes out with the same magnitude, $$\boxed{|M|=\frac{6EI\Delta}{7L^{2}}\approx 0.857\,\frac{EI\Delta}{L^{2}}}$$ and because $M_{AB}=-M_{BA}$ in each column the column shear is exactly zero — there is no horizontal reaction at either base. The beam carries the whole effect as a constant shear $$V_{BC}=\frac{12EI\Delta}{7L^{3}},$$ which is also the axial force in each column and the (equal and opposite) vertical reactions.
  10. (b) Diagram shapes. The bending moment diagram is a straight line on every member: each column runs from $+6EI\Delta/7L^{2}$ at one end to $-6EI\Delta/7L^{2}$ at the other with the contraflexure point at mid-height; the beam is a straight line of constant slope between the two joints, with no point of contraflexure. The shear diagram is zero on both columns and a constant $12EI\Delta/7L^{3}$ on the beam.
-3.0 w0.90 w3.69 w-4.31 w0.68 wshear force diagram (multiples of w)-4.50 whinge M = 01.80 w-2.65 w4.15 w-5.15 w-2.71 w1.36 wbending moment diagram (sagging +, multiples of w)column heads: 4.45 w at x = 10 m, -2.44 w at x = 18 m
Question 2(a): shear force and bending moment diagrams, plotted as multiples of w for the adopted 5 m column height.
Δthis base moves down, no rotationLh = LABCD
Question 2(b): the right-hand fixed base settles Δ without rotating.
6EIΔ/7L²6EIΔ/7L²6EIΔ/7L²all six end moments equal; columns carry NO shear
Question 2(b): all six end moments are equal in magnitude and the columns carry no shear at all.
Question 2 — controlling ordinates
LocationShearBending moment (sagging +)
(a) x = 3 m, left of the roller−3.00 w−4.50 w
(a) x = 3 m to 8 m (to the hinge)+0.90 w−4.50 w → 0
(a) x = 10 m, left / right of column A+0.90 w / +3.69 w+1.80 w / −2.65 w (step 4.45 w)
(a) x = 13.68 m0+4.15 w (maximum sagging)
(a) x = 18 m, left / right of column B−4.31 w / +0.68 w−5.15 w / −2.71 w (step 2.44 w)
(a) x = 24 m, built-in end+0.68 w+1.36 w
(b) every column end06EIΔ/7L²
(b) beam12EIΔ/7L³±6EIΔ/7L² at the two joints