16-Civ-B1 Advanced Structural Analysis · December 2016
Question 4 of 9: Least Work Analysis of a Tied Trapezoidal 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 4: Least Work Analysis of a Tied Trapezoidal Frame (18 marks)
Given. A symmetric tied trapezoidal frame, supported by
a pin at joint 2 and a roller at joint 3, with the two free lower ends
joined by a pin-ended tie.
Given data
Quantity
Symbol
Value
Horizontal beam span 2–3
$L_b$
4.0 m
Horizontal projection of each leg
$p$
1.8 m
Vertical rise of each leg
$r$
2.4 m
Length of each inclined leg
$L_s$
3.0 m
Length of the tie 1–4
$L_t$
7.6 m
Uniformly distributed load on 2–3
$w$
6 kN/m
Flexural rigidity of the beam / of each leg
$EI$ / $3EI$
$9280$ / $27840\ \text{kN}\cdot\text{m}^{2}$
Axial rigidity of the tie
$EA$
1900 kN
Find. The force in the tie and hence the maximum
bending moment in the horizontal beam 2–3.
Question 4: symmetric tied frame. The redundant is the tie force T; the two lower joints 1 and 4 are free ends of the inclined legs.
Approach. Take the tie force $T$ as the single
redundant, express every member's bending moment in terms of $T$ and the applied
load, then impose the least-work condition $\partial U/\partial T=0$ and back
substitute.
Count the redundants and use the symmetry. Externally the
frame is determinate: the pin at joint 2 and the roller at joint 3
give three reaction components. Internally the pin-ended tie closes the chain
1–2–3–4 and supplies exactly one redundancy, so the frame is
$\boxed{1}$ degree statically indeterminate with $T$ as the natural redundant.
Because both the structure and the load are symmetric about midspan, the two
legs carry identical moments and only one of them needs integrating.
Reactions are independent of the redundant. The tie pulls
the two free ends towards each other with equal and opposite horizontal forces,
so it contributes nothing to the global equations. Moments about joint 2
give $V_3=w L_b/2=12.0$ kN, and by symmetry $V_2=12.0$ kN with $H_2=0$.
Bending moments in terms of $T$. Each leg is a cantilever
hanging from its support joint, loaded only by the tie force at its free end, so
at a height $y$ above the tie the moment is $M=Ty$; along the leg,
measured by $s$ from the free end, $M_{\text{leg}}=0.8\,Ts$ with
$0\le s\le 3.0$, reaching $2.4\,T$ at the support. For the beam, with
$\xi$ measured from joint 2,
$$M_{\text{beam}}(\xi)=2.4\,T-12\xi+3\xi^{2}
\quad\text{(sagging}\;=\;-M_{\text{beam}}\text{)}.$$
Impose least work. The total complementary energy is
stationary with respect to the redundant, so
$$\frac{\partial U}{\partial T}=
\frac{2}{3EI}\int_0^{3}(0.8Ts)(0.8s)\,\mathrm{d}s
+\frac{1}{EI}\int_0^{4}\left(2.4T-12\xi+3\xi^{2}\right)(2.4)\,\mathrm{d}\xi
+\frac{T L_t}{EA}=0.$$
Evaluating the integrals,
$$\frac{3.84\,T}{EI}+\frac{23.04\,T-76.8}{EI}+\frac{7.6\,T}{EA}=0
\;\Longrightarrow\;
\frac{26.88\,T-76.8}{9280}+\frac{7.6\,T}{1900}=0.$$
Solve for the tie force. Collecting terms,
$0.0028966\,T+0.0040000\,T=0.0082759$, hence
$$\boxed{T=1.20\ \text{kN (tension)}}.$$
Note the two stiffness terms are of the same order: the tie's own extensibility
supplies more than half the flexibility of the redundant path, so it cannot be
treated as rigid.
Maximum moment in the horizontal beam. Substituting
$T=1.20$ kN into the beam expression and converting to sagging moments,
$$M_{\text{sag}}(\xi)=-2.88+12\xi-3\xi^{2},$$
which gives $-2.88\ \text{kN}\cdot\text{m}$ (hogging) at each end and, at
midspan where the shear vanishes,
$$\boxed{M_{\max}=+9.12\ \text{kN}\cdot\text{m}\ \text{sagging at
midspan of }2\text{--}3.}$$
The check is joint 2: the leg delivers $2.4T=2.88\ \text{kN}\cdot
\text{m}$, exactly the beam's end moment, and the pin support carries no moment
of its own.
Question 4 — results
Quantity
Value
Degree of static indeterminacy
1 (the tie force)
Vertical reactions $V_2=V_3$
12.0 kN each
Horizontal reaction $H_2$
0
Force in the tie 1–4
1.20 kN tension
Moment at each end of the beam 2–3
$-2.88\ \text{kN}\cdot\text{m}$ (hogging)
Moment at the top of each inclined leg
$2.88\ \text{kN}\cdot\text{m}$
Maximum bending moment in the horizontal beam
$+9.12\ \text{kN}\cdot\text{m}$ sagging at midspan