Question 1 of 9: Structural degrees of freedom for a slope-deflection analysis
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 98-Civ-B1 Advanced Structural
Analysis, National Examinations, May 2013 — 3 hours, closed book (an approved
Sharp or Casio calculator is permitted). Nine questions are printed. The candidate must
answer Question 1 and Question 2, then two of Questions 3–5 and
two of Questions 6–9 — six questions constitute a complete paper
(8 + 12 + 2 × 16 + 2 × 24 =
100 marks). Marks are shown in the left margin of the paper.
All nine questions are solved below, because the set is intended as a study
resource rather than as a three-hour sitting.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — influence lines
(Ch. 6, 8), energy methods and Castigliano's theorems (Ch. 9), the force
(flexibility) method (Ch. 10), slope-deflection (Ch. 11) and moment distribution
(Ch. 12).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 13 slope-deflection
including support settlement and sidesway; Ch. 8 influence lines for trusses.
A. Ghali, A. M. Neville and T. G. Brown, Structural Analysis: A Unified
Classical and Matrix Approach, 7th ed. — Ch. 3–5 force and displacement
methods, lack of fit and prescribed displacements.
J. C. McCormac and S. F. Csernak, Structural Analysis Using Classical and
Matrix Methods, 4th ed. — kinematic indeterminacy and the use of symmetry.
Sign conventions used throughout. Slope-deflection end moments
$M_{ij}$ are the moments the joint applies to the member, clockwise positive;
joint rotations $\theta$ are clockwise positive; the chord rotation
$\psi_{ij}=\Delta/L$ is positive when the member chord rotates clockwise. Bending moment
diagrams are plotted with sagging positive, so that the sagging moment at
end $i$ of member $ij$ is $+M_{ij}$ and at end $j$ it is $-M_{ji}$. All members are
inextensible unless stated otherwise, so axial deformation contributes nothing to the
compatibility equations.
Question 1: Structural degrees of freedom for a slope-deflection analysis (8 marks)
Given. Four plane frames (a)–(d), all with inextensible members of
uniform $EI$, are to be analysed by the slope-deflection method. Frame (a) is a
symmetric two-bay, two-storey frame on three fixed bases carrying a horizontal load $P$ at
each floor; frame (b) is a fixed-base column, an inclined member and a horizontal
member built into a wall, carrying a uniformly distributed load $w$; frame (c) is a
three-column frame in which two inclined members and the middle column form a closed
triangle, loaded by $P$ at the triangle apex and by $P$ at the top of the right-hand column;
frame (d) is a stepped beam-and-column assembly on a pin, a roller and a roller,
carrying $w$ on each horizontal member.
Find. The minimum number of structural (kinematic) degrees of
freedom — independent joint rotations plus independent joint translations — for
each of the four structures.
Q1 — the four structures with the independent degrees of freedom marked. Navy dots are joints whose rotation is an unknown; blue arrows are the independent joint translations (sway).
Approach. Count one rotation for every rigid joint whose moment is
not known in advance, count the independent joint translations that survive the
inextensibility constraints of the members, then delete the rotations that symmetry,
anti-symmetry or a known-zero-moment end makes dependent or redundant.
State the counting rule. The number of structural degrees of freedom is
$$n_{\text{dof}} = n_{\theta} + n_{\Delta},$$
where $n_{\theta}$ counts the independent rotations of the rigid joints and $n_{\Delta}$
counts the independent joint translations. A member end at a simple support (a pin
or a roller carrying only one member) has a known zero moment, so the modified
slope-deflection equation $M_{nf}=\dfrac{3EI}{L}\left(\theta_n-\psi\right)$ eliminates that
rotation and it is not counted. Every inextensible member imposes one constraint on the
translations of its two ends, which is what makes $n_{\Delta}$ far smaller than the raw
count of free joint displacements.
Frame (a): use anti-symmetry. The frame is geometrically symmetric about
the centre column. Because the floor beams are inextensible, a horizontal load applied at a
floor may be redistributed arbitrarily among the joints of that floor without changing the
response — only the total storey shear enters the equilibrium equations, and a
horizontal joint force contributes nothing to joint moment equilibrium. Replacing each
$P$ by $P/2$ at the left column and $P/2$ at the right column produces a loading that
reverses sign under reflection, so the response is anti-symmetric:
mirror-image joints rotate by equal amounts in the same sense, and the centre column
(which lies on the axis) carries zero axial force but is free to bend. Hence
$\theta_{A1}=\theta_{C1}$ and $\theta_{A2}=\theta_{C2}$, leaving four independent rotations
$\theta_{A1},\ \theta_{A2},\ \theta_{B1},\ \theta_{B2}$, plus one sway per storey:
$$\boxed{n_{\text{dof}}^{(a)} = 4 + 2 = 6.}$$
Without the symmetry argument the count would have been $6+2=8$.
Frame (b): chase the inextensibility chain. Both ends of the structure
are built in, so no rotation is eliminated by a zero-moment end and the two kinks give
$\theta_1$ and $\theta_2$. For the translations, let joint 1 (the top of the vertical
column) move by $(a,\,0)$ — the vertical column being inextensible fixes its vertical
displacement — and let joint 2 (the kink at the horizontal member) move by
$(0,\,b)$, because the horizontal member runs into the wall. The inclined member ties the two
together through
$$\left(\mathbf{u}_2-\mathbf{u}_1\right)\cdot\mathbf{e}_{12}=0
\quad\Longrightarrow\quad -a\,c_x + b\,c_y = 0 ,$$
so $b$ follows from $a$ and only one translation is independent:
$$\boxed{n_{\text{dof}}^{(b)} = 2 + 1 = 3.}$$
Frame (c): the closed triangle kills the sway. Four rigid joints rotate:
the triangle apex $A$, the top of the middle column $B$, the point $C$ where the lower
inclined member meets the middle column, and the top of the right-hand column $D$; none of
them is a known-zero-moment end. Members $AB$, $AC$ and $CB$ form a closed inextensible
triangle, so $A$, $B$ and $C$ move as a rigid body — two translations and one
rotation. The left column pins $A$ vertically ($A_y=0$) and the lower part of the middle
column pins $C$ vertically ($C_y=0$); since $A$ and $C$ have different abscissae these two
conditions force both the rigid-body rotation and the rigid-body vertical translation to
vanish, leaving a pure horizontal translation. The right-hand column then fixes $D_y=0$ and
the inextensible top beam fixes $D_x=B_x$, so $D$ carries no independent translation:
$$\boxed{n_{\text{dof}}^{(c)} = 4 + 1 = 5.}$$
A rank count on the seven inextensibility constraints acting on the eight translational
freedoms of $A,B,C,D$ confirms a single independent translation.
Frame (d): delete the zero-moment ends, keep the sway. The pin at the
left end of the upper beam and the roller at the right end of the lower beam are single
member ends carrying zero moment, so their rotations are condensed out by the modified
stiffness. Only the two rigid corners remain, giving $\theta_F$ and $\theta_G$. For the
translations: the upper beam ties $F$ horizontally to the pin, the vertical member ties
$F$ vertically to $G$, and the roller under $G$ fixes $G_y=0$, so $F$ is completely
immobilised — but nothing restrains $G$ horizontally, because the lower beam simply
carries $H$ along with it and the roller at $H$ offers no horizontal reaction. The vertical
member therefore sways:
$$\boxed{n_{\text{dof}}^{(d)} = 2 + 1 = 3.}$$
Final results — minimum structural degrees of freedom