16-Civ-B1 Advanced Structural Analysis · December 2016
Question 8 of 9: Anti-Symmetric Analysis of a Portal Frame
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations,
December 2016 — 98-Civ-B1 Advanced Structural Analysis. Three
hours, CLOSED BOOK (an approved Sharp or Casio calculator is permitted).
Questions 1 and 2 are compulsory (12 and 8 marks); the candidate then
answers TWO of Questions 3–5 (18 marks each) and TWO of
Questions 6–9 (22 marks each), so six questions constitute a complete
paper worth 100 marks. All nine questions are solved here,
because the set is intended as a study resource rather than as an exam script.
Reference texts. R. C. Hibbeler, Structural
Analysis, 10th ed. (Ch. 6 influence lines, Ch. 9 virtual work and
Castigliano's theorems, Ch. 10 force method, Ch. 11 slope-deflection,
Ch. 12 moment distribution, Ch. 16 stiffness method for frames);
A. Kassimali, Structural Analysis, 6th ed.; A. Ghali,
A. M. Neville & T. G. Brown, Structural Analysis: A Unified
Classical and Matrix Approach, 7th ed.; J. C. McCormac,
Structural Analysis: Using Classical and Matrix Methods, 4th ed.
Canadian design context for the same structures: CSA S16, CSA A23.3 and
the National Building Code of Canada 2020.
Sign convention used throughout.
Member-end moments follow the counter-clockwise-positive slope-deflection form
$M_{ij}=\dfrac{2EI}{L}\left(2\theta_i+\theta_j-3\psi_{ij}\right)+\mathrm{FEM}_{ij}$,
with the chord rotation $\psi_{ij}=\left[(\mathbf{D}_j-\mathbf{D}_i)\cdot
\mathbf{e}_2\right]/L$ and $\mathbf{e}_2$ the member axis turned
$+90^\circ$. For a downward uniformly distributed load on a horizontal member,
$\mathrm{FEM}_{ij}=+wL^{2}/12$ and $\mathrm{FEM}_{ji}=-wL^{2}/12$. Sagging
moments are recovered as $M_{\text{sag}}(i)=-M_{ij}$ and
$M_{\text{sag}}(j)=+M_{ji}$, and every bending-moment diagram is plotted on the
tension side of the member.
Question 8: Anti-Symmetric Analysis of a Portal Frame (22 marks)
Given. A symmetric single-bay portal with both bases
built in, loaded by a pair of horizontal forces applied at mid-height of each
column and both pointing the same way.
Given data
Quantity
Symbol
Value
Beam span (joints 2 to 3)
$b$
4.5 m
Column height (joints 1 to 2, 4 to 3)
$h$
6.0 m
Height of each applied load above the base
$h_L$
3.0 m
Applied horizontal load on each column
$P$
12 kN, both to the right
Flexural rigidity of every member
$EI$
the same, inextensible
Find. The member-end moments and the shear force and
bending moment diagrams of every member, with maximum and minimum ordinates.
Question 8: symmetric portal under an anti-symmetric pair of horizontal loads. Both 12 kN forces act to the right at mid-height.
Approach. Establish that the loading is anti-symmetric,
reduce the three unknowns $(\theta_2,\theta_3,\Delta)$ to two by
$\theta_2=\theta_3$, write the joint equation and the storey-shear equation,
and solve the $2\times2$ system.
Classify the loading. Reflecting the frame about its centre
line maps the left column onto the right one and reverses the direction of a
horizontal force. Both applied forces point right, so the reflected load set is
the negative of the original: the loading is anti-symmetric. The
response is therefore anti-symmetric as well — both joints rotate through
the same angle $\theta_2=\theta_3=\theta$, both columns sway through the same
$\Delta$, and the two columns carry identical internal forces. Three unknowns
collapse to two.
Write the column and beam equations. Each column has a
transverse point load at mid-height, so
$\mathrm{FEM}_{12}=+Ph/8=+9.0$ and $\mathrm{FEM}_{21}=-9.0\ \text{kN}\cdot
\text{m}$, and $\psi_{12}=-\Delta/h$. With $\theta_1=0$ at the built-in base,
$$M_{12}=\frac{EI}{3}\left(\theta+\frac{\Delta}{2}\right)+9,\qquad
M_{21}=\frac{EI}{3}\left(2\theta+\frac{\Delta}{2}\right)-9.$$
The beam has $\theta_3=\theta_2=\theta$ and no chord rotation (the columns
are inextensible), so $M_{23}=M_{32}=6EI\theta/4.5=1.3333\,EI\theta$.
Storey-shear equation. The two base shears must equilibrate
the total applied horizontal force of $24$ kN, and by anti-symmetry they are
equal, so each base shear is $12$ kN. Taking moments on one column about its top
joint,
$$M_{12}+M_{21}+6H+36=0\quad\text{with}\quad H=-12
\;\Longrightarrow\;M_{12}+M_{21}=36,$$
which in terms of the unknowns is
$$EI\theta+0.33333\,EI\Delta=36. \tag{ii}$$
Solve. Equations (i) and (ii) give
$$\boxed{EI\theta=-6.0\ \text{kN}\cdot\text{m}^{2},\qquad
EI\Delta=+126.0\ \text{kN}\cdot\text{m}^{3}},$$
so the frame sways $126/EI$ to the right while both joints rotate clockwise.
Back substitution gives the member-end moments
$$M_{12}=M_{43}=+28.0,\qquad M_{21}=M_{34}=+8.0,\qquad
M_{23}=M_{32}=-8.0\ \text{kN}\cdot\text{m}.$$
Bending moment diagram. Each column runs from
$\boxed{28.0\ \text{kN}\cdot\text{m}}$ at the base — the maximum
ordinate anywhere in the frame — linearly to $-8.0$ at the load point
$3.0$ m up, crossing zero at $2.33$ m, and then holds the constant
$-8.0\ \text{kN}\cdot\text{m}$ over the whole upper $3.0$ m because the shear
there is zero. The beam runs linearly from $+8.0$ at joint 2 to $-8.0$ at
joint 3, passing through zero at midspan — the signature of an
anti-symmetric response. Both columns carry identical diagrams, not
mirror images.
Shear force diagram and equilibrium check. Each column
carries $\boxed{12.0\ \text{kN}}$ of shear over its lower 3.0 m and exactly
zero over its upper 3.0 m; the beam carries the constant
$16.0/4.5=3.556$ kN, which is also the axial force in each column
(tension on the left, compression on the right). The overturning check closes
exactly:
$$2(28.0)+3.556(4.5)=56.0+16.0=72.0=24\times3.0\ \text{kN}\cdot\text{m}.$$
Question 8: bending moment diagram (kN.m). Both columns carry identical diagrams, 28.0 at the base and a constant -8.0 above the load point; the beam passes through zero at midspan.
Question 8 — results
Quantity
Value
$EI\theta_2=EI\theta_3$
$-6.0\ \text{kN}\cdot\text{m}^{2}$
$EI\Delta$ (sway to the right)
$+126.0\ \text{kN}\cdot\text{m}^{3}$
Moment at each column base (maximum ordinate)
$28.0\ \text{kN}\cdot\text{m}$
Moment at the load point and along the upper column
$-8.0\ \text{kN}\cdot\text{m}$ (minimum ordinate)
Beam end moments
$\pm 8.0\ \text{kN}\cdot\text{m}$, zero at midspan