NivaarExam PrepOfficial exam papers ↗

07-Str-A1 · May 2013

Question 5 of 8: Frame analysis by slope-deflection, with shear and bending moment diagrams

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

Notes on this paper

Paper format. National Examinations, May 2013 — 07-Str-A1 Elementary Structural Analysis. Three hours, CLOSED BOOK, an approved Sharp or Casio calculator permitted. Six questions constitute a complete paper: candidates answer ALL of Questions 1 to 5 and ONE of Questions 6, 7 or 8. Marks are shown in the left margin (6 + 18 + 16 + 18 + 20 + 22 = 100). All eight questions are solved below, because the three alternatives test different topics and the whole set is useful for study.

Reference texts.

Sign conventions used throughout. For beams and for each individual frame member, shear is positive when the resultant of the forces to the left of (or below) a section acts upward, and bending moment is positive when it sags the member, that is when it puts the inside face of a frame member or the underside of a beam in tension. Truss forces are quoted as T for tension and C for compression. Reactions are drawn in blue and applied loads in red on every figure.

Question 5: Frame analysis by slope-deflection, with shear and bending moment diagrams (20 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 continuous member 1–2–3–4 propped at joint 2 by a short column 2–5.

MemberLengthRelative stiffnessLoadingEnd conditions
1 – 28 mEInonejoint 1 fully fixed
2 – 316 m2EI9 kN/m over the whole spancontinuous at both ends
3 – 44 mEI11 kN point load at the free end 4roller support at joint 3, free at joint 4
2 – 52 mEInonerigid at joint 2, pinned at joint 5

Find. All member end moments, then complete shear force and bending moment diagrams for every member, labelled with the maximum and minimum ordinates.

9 kN/m11 kN123458 m16 m4 m2 mEI2EIEIEI
The frame. Joint 1 is fully fixed, joint 3 is a roller, the 4 m length beyond it is an overhang, and the 2 m column from joint 2 down to the pin at joint 5 is a full frame member, not a simple prop.

Approach. No joint can translate, so the only unknowns are the rotations at joints 2 and 3; write the slope-deflection equations for the four members, impose moment equilibrium at those two joints, and recover the shears and diagrams from the resulting end moments.

Check: joints 2 and 3 are assumed not to translate. This follows from the data as given — the members are stated to be inextensible, joint 1 is fully fixed, so the axially rigid member 1–2 fixes joint 2 horizontally; the axially rigid column 2–5 fixes joint 2 vertically; and the roller at 3 fixes joint 3 vertically while member 2–3 fixes it horizontally. The frame is therefore a no-sway frame and the analysis needs no sway correction.
  1. Fixed-end moments and the overhang moment. Only span 2–3 carries a distributed load, so with the sign convention that a clockwise moment applied by the joint to the member end is positive, $$\begin{aligned} M^{F}_{23} &= -\frac{wL^2}{12} = -\frac{9(16)^2}{12} = -192\ \text{kN}\cdot\text{m}, \\ M^{F}_{32} &= +192\ \text{kN}\cdot\text{m} \end{aligned}$$ The 4 m overhang is statically determinate, so it applies a known moment at joint 3 rather than an unknown one: $$M_{34} = -11(4) = -44\ \text{kN}\cdot\text{m}$$
  2. Write the slope-deflection equations. With $M_{AB} = \dfrac{2EI}{L}\left(2\theta_A + \theta_B\right) + M^{F}_{AB}$ and $\theta_1 = 0$, and with the far end of the column released at the pin so that $M_{52} = 0$ can be used to eliminate $\theta_5$, $$\begin{aligned} M_{12} &= 0.25E\theta_2, \\ M_{21} &= 0.50E\theta_2 \end{aligned}$$ $$\begin{aligned} M_{23} &= 0.50E\theta_2 + 0.25E\theta_3 - 192, \\ M_{32} &= 0.50E\theta_3 + 0.25E\theta_2 + 192 \end{aligned}$$ $$M_{25} = \frac{3EI}{L}\theta_2 = 1.50E\theta_2$$ where the column has been given its reduced pinned-end stiffness $3EI/L$ because joint 5 carries no moment.
  3. Impose equilibrium at the two free joints. At joint 2 three members meet, and at joint 3 the span moment must balance the known overhang moment: $$M_{21} + M_{23} + M_{25} = 0 \;\Rightarrow\; 2.50E\theta_2 + 0.25E\theta_3 = 192$$ $$M_{32} + M_{34} = 0 \;\Rightarrow\; 0.25E\theta_2 + 0.50E\theta_3 = -148$$ Solving the pair, $$\begin{aligned} E\theta_2 &= +112.0\ \text{kN}\cdot\text{m}^2, \\ E\theta_3 &= -352.0\ \text{kN}\cdot\text{m}^2 \end{aligned}$$
  4. Back-substitute for the end moments. $$M_{12} = \boxed{+28.0}, \quad M_{21} = +56.0, \quad M_{23} = -224.0, \quad M_{32} = +44.0, \quad M_{25} = +168.0\ \text{kN}\cdot\text{m}$$ Three independent checks confirm the set: joint 2 balances, $56.0 - 224.0 + 168.0 = 0$; joint 3 balances, $44.0 - 44.0 = 0$; and the carry-over relation for a member whose far end is fixed holds exactly, $M_{12} = \tfrac{1}{2}M_{21} = 28.0$ kN.m. Moment distribution started from the same fixed-end moments converges on the identical figures.
  5. Member end shears. For a member of length $L$ carrying a uniform load $w$, the end shears follow from $V_A = \dfrac{wL}{2} - \dfrac{M_{AB} + M_{BA}}{L}$ and $V_B = wL - V_A$. Hence $$\text{1--2:}\ V = \frac{28.0 + 56.0}{8} = 10.5\ \text{kN (constant)}$$ $$\text{2--3:}\ V_2 = \frac{9(16)}{2} - \frac{-224.0 + 44.0}{16} = 72 + 11.25 = 83.25\ \text{kN}, \quad V_3 = 144 - 83.25 = 60.75\ \text{kN}$$ $$\text{2--5:}\ V = \frac{168.0 + 0}{2} = 84.0\ \text{kN (horizontal)}$$ and the overhang carries a constant 11.0 kN.
  6. Support reactions, as a check on everything above. Assembling the member end shears at each support, $$R_1 = 10.5\ \text{kN downward}, \quad R_3 = 60.75 + 11.0 = 71.75\ \text{kN upward}, \quad R_5 = 10.5 + 83.25 = 93.75\ \text{kN upward}$$ $$\sum F_y:\ -10.5 + 71.75 + 93.75 = 155.0 = 9(16) + 11 \;\checkmark$$ The downward reaction at the fixed end is real, not an error: the stiff column at joint 2 lifts that end of the frame, and member 1–2 has to be held down.
  7. Bending moment ordinates. On member 1–2 the moment runs linearly from $+28.0$ kN.m at the fixed end to $-56.0$ kN.m just left of joint 2, crossing zero at 2.67 m from joint 1. At joint 2 the diagram steps by 168.0 kN.m, the moment carried away down the column, so it restarts at $-224.0$ kN.m. Along the 16 m span, $$M(x) = -224.0 + 83.25x - 4.5x^2$$ whose peak is where the shear vanishes, at $x = 83.25/9 = 9.25$ m: $$M_{max}^{+} = \boxed{+161.03\ \text{kN}\cdot\text{m at } 9.25\ \text{m from joint 2}}$$ The span ends at $-44.0$ kN.m over the roller, which the overhang reproduces exactly as $-11(4)$. The column carries a linear diagram from zero at the pin to 168.0 kN.m at joint 2.
Shear force V (kN) along 1-2-3-4-10.5+83.25-60.75+11.0Bending moment M (kN.m) along 1-2-3-4, sagging positive+28.0 at joint 1-56.0 just left of joint 2-224.0 just right of joint 2+161.03-44.0 at joint 3Column 2-5: bending moment (kN.m) against height above joint 5168.0 at joint 2
Shear force and bending moment along 1-2-3-4, and the bending moment on the column 2-5. Note the step of 168.0 kN.m in the moment diagram at joint 2, which is the moment carried into the column.
MemberEnd moments (kN.m)Shear ordinates (kN)Maximum moment (kN.m)Minimum moment (kN.m)
1 – 2M12 = +28.0, M21 = +56.0-10.5 throughout+28.0 at joint 1-56.0 just left of joint 2
2 – 3M23 = -224.0, M32 = +44.0+83.25 at joint 2 falling to -60.75 at joint 3+161.03 at 9.25 m from joint 2-224.0 just right of joint 2
3 – 4M34 = -44.0, free end+11.0 throughout0 at the free end 4-44.0 at joint 3
2 – 5M25 = +168.0, M52 = 084.0 throughout (horizontal)168.0 at joint 20 at the pin 5
ReactionValue
Joint 1 (fixed)10.5 kN downward, 84.0 kN horizontal, 28.0 kN.m restraining moment
Joint 3 (roller)71.75 kN upward
Joint 5 (pin)93.75 kN upward, 84.0 kN horizontal