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.
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 node
Description
Node 1
left-hand end of the beam, x = 0, built in (fixed)
Node 2
x = 8 m, rigid joint where the column frames into the beam
Node 3
x = 14 m, roller support
Node 4
x = 15 m, free end of a 1 m overhang
Node 5
base of the column, 4 m below node 2, built in (fixed)
Loading
12 kN/m over 0 to 8 m; 8 kN/m over 8 to 15 m
Stiffness
EI 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.
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.
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.
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.
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.
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.
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.
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