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07-Str-A1 · December 2016

Question 5 of 8: Frame Analysis by Slope Deflection

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

Notes on this paper

Paper format. National Exams, December 2016 — 07-Str-A1 Elementary Structural Analysis, 3 hours, CLOSED BOOK (an approved Sharp or Casio calculator is permitted). Six questions constitute a complete paper: Questions 1–5 are compulsory and one only of Questions 6, 7 or 8 is attempted, for 100 marks (6 + 18 + 18 + 20 + 18 + 20). Marks are shown in the left margin. All eight questions are worked below, because the three alternatives exercise three quite different methods — three-hinged-frame statics, influence lines and virtual work — and the complete set is the more useful study resource.

Every structure on this paper is defined by a hand-drawn figure and nothing else: the printed text states the task, the drawing carries the geometry, the loads and the support types.

Sign conventions used throughout. Shear force is positive when the resultant of the forces to the left of a section acts upwards along the positive local normal of the member; bending moment is positive when it sags the member (tension on the underside), and sagging ordinates are plotted above the axis in every diagram. Truss member forces are quoted as T for tension and C for compression. In the slope-deflection work of Question 5 the member-end moments follow the usual convention, clockwise on the member end taken as positive, so that the sagging moment is $+M_{ij}$ at the left end of a member and $-M_{ji}$ at its right end.

Reference texts.

Question 5: Frame Analysis by Slope Deflection (18 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. A horizontal beam 15 m long carrying a rigid column at mid-length, dimensioned 8 m + 6 m + 1 m along the beam.

Given data, Question 5
Member or nodeDescription
Node 1left-hand end of the beam, x = 0, built in (fixed)
Node 2x = 8 m, rigid joint where the column frames into the beam
Node 3x = 14 m, roller support
Node 4x = 15 m, free end of a 1 m overhang
Node 5base of the column, 4 m below node 2, built in (fixed)
Loading12 kN/m over 0 to 8 m; 8 kN/m over 8 to 15 m
StiffnessEI the same in every member; members inextensible

Find. The joint rotations, the member-end moments, the support reactions, and the shear and bending moment diagrams with maximum and minimum ordinates labelled for every member.

12 kN/m8 kN/m123458 m6 m1 m4 mV (kN)+49.41-46.59+30.25-17.75+8M (kN.m)-67.75+33.96-56.5-41.5+15.69-4Column 2-5: constant shear 5.625 kN; moment varies linearly from 15 kN.m at joint 2 to 7.5 kN.m at base 5 (opposite sense).
Question 5: the frame, and the shear and bending moment diagrams along the beam. The step of 15 kN.m in the moment diagram at node 2 is the moment delivered by the column.

Approach. Establish first that the frame cannot sway, so the only unknowns are the rotations at nodes 2 and 3; write the slope-deflection equation for each member end, impose moment equilibrium at those two joints, and back-substitute for the end moments, shears and reactions.

  1. Show that there is no sidesway. The members are inextensible and node 1 is fully fixed, so beam 1-2 pins node 2 horizontally; column 2-5 then pins node 2 vertically against the fixed base at node 5. Beam 2-3 carries the horizontal restraint on to node 3, whose roller removes its vertical freedom. Every joint translation is therefore suppressed and the only unknowns are $\theta_2$ and $\theta_3$. This is what the phrase “all members are inextensible” in the question is there to license.
  2. Compute the fixed-end moments. For a uniformly loaded member, $\text{FEM} = w L^{2} / 12$ at each end, hogging at the left and sagging at the right in the clockwise-positive convention: $$\text{FEM}_{12} = -\frac{(12)(8)^{2}}{12} = -64, \qquad \text{FEM}_{21} = +64\ \text{kN}\cdot\text{m}$$ $$\text{FEM}_{23} = -\frac{(8)(6)^{2}}{12} = -24, \qquad \text{FEM}_{32} = +24\ \text{kN}\cdot\text{m}$$ The column carries no transverse load, so both its fixed-end moments are zero.
  3. Treat the overhang as a known applied moment. The 1 m cantilever beyond the roller is determinate and has no rotational stiffness, so it must never be given a share of the joint balance. It delivers $$M_{34} = -\frac{w a^{2}}{2} = -\frac{(8)(1)^{2}}{2} = -4\ \text{kN}\cdot\text{m}$$ to node 3, together with its 8 kN of load.
  4. Write the slope-deflection equations. With $M_{ij} = \dfrac{2EI}{L}\left( 2\theta_i + \theta_j \right) + \text{FEM}_{ij}$ and $\theta_1 = \theta_5 = 0$, writing $X = EI\theta_2$ and $Y = EI\theta_3$, $$M_{12} = 0.25X - 64, \qquad M_{21} = 0.5X + 64$$ $$M_{23} = \tfrac{2}{3}X + \tfrac{1}{3}Y - 24, \qquad M_{32} = \tfrac{2}{3}Y + \tfrac{1}{3}X + 24$$ $$M_{25} = X, \qquad M_{52} = 0.5X$$
  5. Impose joint equilibrium and solve. At node 2 the three member ends must balance, and at node 3 the beam end must balance the overhang: $$M_{21} + M_{23} + M_{25} = 0 \quad\Rightarrow\quad 2.1667X + 0.3333Y = -40$$ $$M_{32} + M_{34} = 0 \quad\Rightarrow\quad 0.3333X + 0.6667Y = -20$$ $$EI\theta_2 = \boxed{-15.0\ \text{kN}\cdot\text{m}^{2}}, \qquad EI\theta_3 = \boxed{-22.5\ \text{kN}\cdot\text{m}^{2}}$$ Both come out as exact numbers, which is the arithmetic check that the sign of the overhang moment was entered correctly.
  6. Back-substitute for the member-end moments. $$M_{12} = \boxed{-67.75}, \quad M_{21} = \boxed{+56.5}, \quad M_{23} = \boxed{-41.5}$$ $$M_{32} = \boxed{+4.0}, \quad M_{25} = \boxed{-15.0}, \quad M_{52} = \boxed{-7.5}\ \text{kN}\cdot\text{m}$$ Node 2 balances exactly, $56.5 - 41.5 - 15.0 = 0$, and node 3 balances against the overhang, $4.0 - 4.0 = 0$.
  7. Convert the end moments to shears. Using $M_{\text{sag}} = +M_{ij}$ at a left end and $-M_{ji}$ at a right end, the shear at the left end of a uniformly loaded member is $V_i = \left( M_{\text{sag},j} - M_{\text{sag},i} + wL^{2}/2 \right)/L$. On beam 1-2 that gives $V = +49.41$ kN falling to $-46.59$ kN at node 2; on beam 2-3, $+30.25$ kN falling to $-17.75$ kN; on the overhang, $+8$ kN falling to zero; and on the column, a constant $5.625$ kN.
  8. Locate the sagging peaks and assemble the reactions. Zero shear on 1-2 occurs at $x = 49.41/12 = 4.12$ m, where $$M = -67.75 + \frac{(49.41)^{2}}{2(12)} = \boxed{+33.96\ \text{kN}\cdot\text{m}}$$ and on 2-3 at $3.78$ m past node 2, where $$M = -41.5 + \frac{(30.25)^{2}}{2(8)} = \boxed{+15.69\ \text{kN}\cdot\text{m}}$$ The reactions follow from the shear jumps: $$R_1 = \boxed{49.41\ \text{kN}}, \qquad R_3 = 8 - (-17.75) = \boxed{25.75\ \text{kN}}, \qquad R_5 = \boxed{76.84\ \text{kN}}$$ and these sum to $152$ kN, exactly the applied $12(8) + 8(7) = 152$ kN.
Question 5 — member-end moments, reactions and diagram ordinates
MemberEnd moments (kN·m)Shear: max / min (kN)Moment: max / min (kN·m)
1-2 (beam, 8 m, 12 kN/m)M12 = −67.75, M21 = +56.5+49.41 / −46.59+33.96 at x = 4.12 m / −67.75 at node 1
2-3 (beam, 6 m, 8 kN/m)M23 = −41.5, M32 = +4.0+30.25 / −17.75+15.69 at 3.78 m from node 2 / −41.5 at node 2
3-4 (overhang, 1 m)M34 = −4.0+8 / 00 at node 4 / −4.0 at node 3
2-5 (column, 4 m)M25 = −15.0, M52 = −7.55.625 (constant)15.0 at node 2 / 7.5 at node 5, opposite senses
Rotations EIθ2 = −15.0, EIθ3 = −22.5 kN·m2. Reactions R1 = 49.41 kN, R3 = 25.75 kN, R5 = 76.84 kN (sum 152 kN).