Question 6 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, May 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 + 15 + 18 + 21 + 22). Marks are shown in the left margin.
All eight questions are worked below, because the three
alternatives exercise three different methods — slope deflection,
virtual work and three-hinged-frame statics — 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 gives the task, the drawing gives 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;
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 6 the member-end moments
follow the usual convention, clockwise on the member end taken as positive.
$EI$ the same for every member; all members inextensible
Find. The shear force and bending moment diagrams for
every member, with the maximum and minimum ordinates labelled.
Approach. Slope deflection. Because the members are
inextensible and node 4 is fixed, nodes 2 and 3 cannot translate horizontally,
and the inextensible columns stop them translating vertically, so there is no
sidesway and the only unknowns are the joint rotations $\theta_2$ and
$\theta_3$. Write the end moments, impose moment equilibrium at those two
joints, solve the two-by-two system, then recover shears from member free
bodies.
Establish that there is no sidesway and count the
unknowns. The beam 1–2–3–4 is inextensible and
node 4 is built in, so nodes 2 and 3 are fixed horizontally; the columns are
inextensible and their bases are on the ground, so nodes 2 and 3 are fixed
vertically. The kinematic unknowns are therefore just $\theta_2$ and
$\theta_3$ — a two-equation problem despite five degrees of static
indeterminacy.
Deal with the overhang first. The 1 m cantilever is
statically determinate and applies a known moment at joint 2:
$$M_{21} = 16.5\,(1) = 16.5\ \text{kN}\cdot\text{m}$$
It has no rotational stiffness, so it must be entered as a fixed applied
moment at the joint and never given a share of the balancing moment.
Write the slope-deflection equations. With
$\mathrm{FEM}_{23} = -wL^2/12 = -64$ and
$\mathrm{FEM}_{32} = +64\ \text{kN}\cdot\text{m}$, and using the modified
form $3EI\theta/L$ for the pin-based column 2–5,
$$\begin{aligned}
M_{23} &= \tfrac{2EI}{8}\left(2\theta_2 + \theta_3\right) - 64, &
M_{32} &= \tfrac{2EI}{8}\left(2\theta_3 + \theta_2\right) + 64\\
M_{34} &= \tfrac{2EI}{4}\left(2\theta_3\right), &
M_{43} &= \tfrac{2EI}{4}\left(\theta_3\right)\\
M_{25} &= \tfrac{3EI}{4}\,\theta_2, &
M_{36} &= \tfrac{2EI}{4}\left(2\theta_3\right)
\end{aligned}$$
with $M_{52} = 0$ at the pin and $M_{63} = \tfrac{2EI}{4}\theta_3$.
Impose joint equilibrium. Writing
$a = EI\theta_2$ and $b = EI\theta_3$, the two joint equations
$M_{21} + M_{23} + M_{25} = 0$ and $M_{32} + M_{34} + M_{36} = 0$ become
$$\begin{aligned}
1.25\,a + 0.25\,b &= 47.5\\
0.25\,a + 2.50\,b &= -64
\end{aligned}$$
$$\boxed{EI\theta_2 = 44.0,\qquad EI\theta_3 = -30.0\ \ \text{kN}\cdot\text{m}^2}$$
The clean values are a good sign that the fixed-end moments and the
overhang sign are right.
Back-substitute for the member end moments.
$$\begin{aligned}
M_{23} &= -49.5, & M_{32} &= +60.0\\
M_{34} &= -30.0, & M_{43} &= -15.0\\
M_{25} &= +33.0, & M_{52} &= 0\\
M_{36} &= -30.0, & M_{63} &= -15.0
\end{aligned}$$
all in $\text{kN}\cdot\text{m}$. Checking the joints,
$16.5 - 49.5 + 33.0 = 0$ at node 2 and
$60.0 - 30.0 - 30.0 = 0$ at node 3.
Convert to bending moments and find the beam shears.
In beam terms the moment at node 2 is $-49.5$ and at node 3 is $-60.0$
$\text{kN}\cdot\text{m}$, both hogging. Free-body equilibrium of member
2–3 gives the end shears
$$V_2 = \frac{M_3 - M_2 + wL^2/2}{L}
= \frac{-60 + 49.5 + 384}{8} = +46.6875\ \text{kN}$$
$$V_3 = V_2 - wL = 46.6875 - 96 = -49.3125\ \text{kN}$$
The shear passes through zero at $x = 46.6875/12 = 3.8906\ \text{m}$ from
node 2, where the sagging peak is
$$M_{\max} = -49.5 + 46.6875(3.8906) - 6(3.8906)^2
= +41.322\ \text{kN}\cdot\text{m}$$
Finish the remaining members. Beam 3–4 carries no
load, so its moment runs linearly from $-30.0$ at node 3 to $+15.0$ at node
4 and its shear is constant at
$(15 + 30)/4 = +11.25\ \text{kN}$. Column 2–5 carries
$33.0\ \text{kN}\cdot\text{m}$ at the head and zero at the pin, so its shear
is $33.0/4 = 8.25\ \text{kN}$; column 3–6 carries $30.0$ at the head
and $15.0$ at the base with the ends bending in opposite senses, so its
shear is $(30 + 15)/4 = 11.25\ \text{kN}$ and its point of contraflexure
sits $2.667\ \text{m}$ below node 3.
Extract the reactions and check global equilibrium.
The jumps in the beam shear give the vertical reactions
$$\begin{aligned}
R_5 &= 46.6875 - (-16.5) = 63.1875\ \text{kN}\ \uparrow\\
R_6 &= 11.25 - (-49.3125) = 60.5625\ \text{kN}\ \uparrow\\
R_4 &= -11.25\ \text{kN}\ \ (\text{i.e. }11.25\ \text{kN downward})
\end{aligned}$$
and $63.1875 + 60.5625 - 11.25 = 112.5\ \text{kN}$, exactly the applied
total $16.5 + 96$. Horizontally the two column shears, 8.25 kN and
11.25 kN, are balanced by a 3.0 kN reaction at the built-in end 4, and the
fixing moment there is the $15.0\ \text{kN}\cdot\text{m}$ already found.
Q6. Base 5 is a pin, base 6 and end 4 are fully fixed. The frame is five times statically indeterminate but only twice kinematically indeterminate, which is what makes slope deflection so economical here.
Q6 shear. Each member is developed on its own axis. The two column ordinates are the horizontal shears carried by those columns; the sign convention within a column is local to it.
Q6 moment. Sagging is plotted above the axis. The peak sagging moment of +41.322 kN·m occurs 3.891 m from node 2, and the largest hogging moment of −60.0 kN·m sits over node 3.
Member
Shear ordinates
Moment ordinates
1–2 (overhang)
$-16.5\ \text{kN}$ throughout
$0 \to -16.5\ \text{kN}\cdot\text{m}$
2–3 (loaded span)
max $+46.6875$, min $-49.3125\ \text{kN}$
$-49.5$ at 2, peak $+41.322$ at $x = 3.891\ \text{m}$, $-60.0$ at 3
3–4
$+11.25\ \text{kN}$ throughout
$-30.0$ at 3, $+15.0\ \text{kN}\cdot\text{m}$ at 4
Column 2–5
$8.25\ \text{kN}$ throughout
$33.0$ at the head, $0$ at the pinned base
Column 3–6
$11.25\ \text{kN}$ throughout
$30.0$ at the head, $15.0\ \text{kN}\cdot\text{m}$ at the fixed base