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.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 2
(determinacy and stability), Ch. 3–4 (trusses; internal loadings),
Ch. 6 (influence lines), Ch. 8–9 (deflections and virtual work),
Ch. 11–12 (slope-deflection and moment distribution).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3
(equilibrium and determinacy), Ch. 4 (plane trusses), Ch. 5 (beams and frames),
Ch. 7 (deflections by virtual work), Ch. 8 (influence lines), Ch. 16–17
(slope-deflection and moment distribution).
K. Leet, C.-M. Uang and A. Gilbert, Fundamentals of Structural
Analysis, 5th ed. — a parallel treatment of the same syllabus.
C. H. Norris, J. B. Wilbur and S. Utku, Elementary Structural
Analysis, 4th ed. — the classical text after which this exam code is
named; still the clearest source on influence lines for subdivided trusses.
Canadian design context: CSA S16 Design of Steel Structures,
CSA A23.3 Design of Concrete Structures and the
National Building Code of Canada. This is an analysis paper, so no
code clause is needed to answer it, but every result below is expressed in the
SI units those documents use.
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)
Given. A continuous member 1–2–3–4 propped
at joint 2 by a short column 2–5.
Member
Length
Relative stiffness
Loading
End conditions
1 – 2
8 m
EI
none
joint 1 fully fixed
2 – 3
16 m
2EI
9 kN/m over the whole span
continuous at both ends
3 – 4
4 m
EI
11 kN point load at the free end 4
roller support at joint 3, free at joint 4
2 – 5
2 m
EI
none
rigid 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.
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.
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:
$$M_{34} = -11(4) = -44\ \text{kN}\cdot\text{m}$$
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.
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,
$$\begin{aligned} E\theta_2 &= +112.0\ \text{kN}\cdot\text{m}^2, \\ E\theta_3 &= -352.0\ \text{kN}\cdot\text{m}^2 \end{aligned}$$
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.
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.
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.
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 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.
Member
End moments (kN.m)
Shear ordinates (kN)
Maximum moment (kN.m)
Minimum moment (kN.m)
1 – 2
M12 = +28.0, M21 = +56.0
-10.5 throughout
+28.0 at joint 1
-56.0 just left of joint 2
2 – 3
M23 = -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 – 4
M34 = -44.0, free end
+11.0 throughout
0 at the free end 4
-44.0 at joint 3
2 – 5
M25 = +168.0, M52 = 0
84.0 throughout (horizontal)
168.0 at joint 2
0 at the pin 5
Reaction
Value
Joint 1 (fixed)
10.5 kN downward, 84.0 kN horizontal, 28.0 kN.m restraining moment