NivaarExam PrepOfficial exam papers ↗

16-Civ-B1 Advanced Structural Analysis · May 2013

Question 2 of 9: Schematic shear force and bending moment diagrams

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

Notes on this paper

Paper format. 98-Civ-B1 Advanced Structural Analysis, National Examinations, May 2013 — 3 hours, closed book (an approved Sharp or Casio calculator is permitted). Nine questions are printed. The candidate must answer Question 1 and Question 2, then two of Questions 3–5 and two of Questions 6–9 — six questions constitute a complete paper (8 + 12 + 2 × 16 + 2 × 24 = 100 marks). Marks are shown in the left margin of the paper. All nine questions are solved below, because the set is intended as a study resource rather than as a three-hour sitting.

Reference texts.

Sign conventions used throughout. Slope-deflection end moments $M_{ij}$ are the moments the joint applies to the member, clockwise positive; joint rotations $\theta$ are clockwise positive; the chord rotation $\psi_{ij}=\Delta/L$ is positive when the member chord rotates clockwise. Bending moment diagrams are plotted with sagging positive, so that the sagging moment at end $i$ of member $ij$ is $+M_{ij}$ and at end $j$ it is $-M_{ji}$. All members are inextensible unless stated otherwise, so axial deformation contributes nothing to the compatibility equations.

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. Three structures of uniform $EI$ with inextensible members.

Given data
StructureGeometryAction
(a)free tip, $L/3$ overhang, roller, span $L$, roller, $L/3+L/3+L/3$, roller, span $L$, built-in end$w$ on the overhang; two point loads $P$ at $L/3$ centres in the third bay
(b)three columns of height $1.5L$ at $L$ centres; hinged outer bases, fixed centre base; continuous beam over both bayshorizontal $P$ at the top of the left-hand column
(c)single-bay portal, height $h$, span $L$; right-hand base fixed; left-hand base on a horizontal guideleft-hand base translated a distance $\Delta$ to the left after construction, with zero rotation of that joint

Find. The shape of the shear force and bending moment diagrams for each structure, with the discontinuities, the points of zero shear and the points of contraflexure located correctly.

w P P L/3 L L/3 L/3 L/3 L SFD 0.955 −1.045 BMD +0.205 −0.113 −0.158
Q2(a) — three-times statically indeterminate continuous beam. Ordinates are shown for the illustrative case $wL = P$; the shapes are independent of that choice.
  1. (a) Establish the shape rules before computing anything. The beam has three rollers plus a built-in end, so with five vertical/moment reaction components and two equations of equilibrium it is three times statically indeterminate. Whatever the redundants turn out to be, the diagrams must satisfy $$V=\frac{dM}{dx},\qquad \frac{dV}{dx}=-w .$$ Hence: the shear is linear under the distributed load on the overhang and constant everywhere else; it steps down by $P$ at each point load and steps up by the reaction at each support. The moment is parabolic on the overhang and piecewise linear elsewhere, is zero at the free tip, and is continuous at every support (there is no applied couple anywhere).
  2. (a) Fix the ordinates. Solving the three-fold redundancy (illustrative case $w=P/L$, so $wL=P$) gives hogging peaks over the second and fourth supports, a sagging peak under the first point load and a small sagging moment at the built-in end because the last span carries no load and the fixed end must hold the beam down: $$M_{\text{sag,max}} \approx +0.205\,PL,\qquad M_{\text{hog}} \approx -0.113\,PL \text{ and } -0.158\,PL,$$ with $V_{\max}\approx+0.955P$ just right of the second support and $-1.045P$ just left of the third. The overhang moment is a pure cantilever parabola $-wx^{2}/2$ running from zero at the tip to $-wL^{2}/18$ over the first roller.
P L L 1.5L BMD, ordinates × PL (illustrative) 0.548 0.490 0.231 0.245
Q2(b) — two-bay frame under a lateral load. Hinged outer bases carry zero moment; the fixed centre base takes the largest moment.
  1. (b) Read the boundary conditions off the supports. The two outer bases are drawn with the “typical hinge” circle, so their bending moments are identically zero and the moment diagram in each outer column is a straight line from zero at the base to its value at the beam. The centre base is built in and takes a finite moment. The beam is inextensible, so all three column heads share one sway $\Delta$ and the storey-shear equation $$\sum_{\text{columns}} \frac{M_{\text{top}}+M_{\text{bottom}}}{h} = -P$$ closes the system.
  2. (b) Interpret the resulting diagrams. Since $P$ may be moved along the inextensible beam, the loading is again anti-symmetric, so the two outer columns carry identical moments and the two beam spans carry equal and opposite end moments. Each column shear is constant, and the shear in each beam span is constant because no vertical load acts. Numerically (illustrative $P=1$, $L=1$, $h=1.5$) the centre column takes $0.548\,PL$ at its base and $0.490\,PL$ at its head, the outer columns take $0.231\,PL$ at their heads, and the beams reach $\pm0.245\,PL$ at the centre joint. The centre column carries no axial force — the signature of an anti-symmetric response in a member lying on the axis of symmetry — while the outer columns carry equal and opposite axial forces.
Δ h L 2EIΔ/h² EIΔ/h² constant, so the beam shear is zero BMD for the square portal h = L; support moved left with no joint rotation
Q2(c) — portal whose left-hand base is displaced horizontally with the joint rotation held at zero. The action is a spread of the bases, so the response is symmetric and the beam carries a constant moment.
  1. (c) Recognise that the imposed movement is a symmetric action. Only the relative displacement of the two bases matters, because superposing a rigid-body translation of the whole frame changes nothing. Moving the left base outward by $\Delta$ is therefore identical to spreading the two bases apart by $\Delta$, which is a symmetric action on a symmetric frame. Consequently the two column heads share the movement equally, $u_B=u_C=-\Delta/2$, the two columns bend in mirror image, and the two joint rotations are equal and opposite.
  2. (c) Write one slope-deflection equation and close it. With $k_c=2EI/h$, $k_b=2EI/L$ and the chord rotation $\psi=\Delta/(2h)$ in each column, joint equilibrium at $B$ gives $k_c\!\left(2\theta-3\psi\right)+k_b\theta=0$, so $$\theta=\frac{3\Delta L}{2h\,(2L+h)} .$$ For the square portal drawn ($h=L$) this reduces to $\theta=\Delta/(2L)$ and $$\boxed{M_{\text{base}}=\frac{2EI\Delta}{h^{2}},\qquad M_{\text{column head}}=M_{\text{beam}}=\frac{EI\Delta}{h^{2}},\qquad V_{\text{column}}=\frac{3EI\Delta}{h^{3}} .}$$ The bending moment in the beam is the same at both ends and of the same sign, so the beam carries a constant moment and zero shear — the diagnostic feature that distinguishes a symmetric base spread from the anti-symmetric sway produced by a lateral load, where the beam moment reverses across the span and the beam shear is finite. Each column has one point of contraflexure, one third of the way up from the base.
Final results — key features of the six diagrams
StructureShear force diagramBending moment diagram
(a)linear on the overhang ($0 \to -wL/3$), constant in every other bay, steps of $P$ at the two point loads; peak $\approx +0.955P$ and $-1.045P$ in the third bay ($wL=P$)parabolic on the overhang from zero at the tip; linear elsewhere; hogging $\approx-0.113PL$ and $-0.158PL$ over the interior supports, sagging $\approx+0.205PL$ under the first point load, small sagging moment at the built-in end
(b)constant in each column (sum $=P$) and constant in each beam span zero at both hinged bases; largest at the fixed centre base ($0.548PL$); beam moments equal and opposite about the centre joint
(c)equal and opposite constant shears $3EI\Delta/h^{3}$ in the two columns; zero in the beam$2EI\Delta/h^{2}$ at each base, $EI\Delta/h^{2}$ constant along the beam; one point of contraflexure per column at $h/3$ above the base