16-Civ-B1 Advanced Structural Analysis · December 2019
Question 4 of 9: Castigliano's theorem — vertical deflection of an overhang tip
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examination, December 2019 —
16-Civ-B1 Advanced Structural Analysis, 3 hours, CLOSED BOOK (an
approved Casio or Sharp calculator only). Nine questions on seven pages:
Questions 1 and 2 are compulsory (8 and 12 marks); the candidate then answers
TWO of Questions 3, 4 or 5 (18 marks each) and TWO of Questions 6, 7, 8 or 9
(22 marks each), so six questions make a complete paper of 100 marks. Because
this set is a study resource, all nine questions are solved
here.
Reference texts. R. C. Hibbeler, Structural
Analysis, 10th ed. (Pearson) — Ch. 6 influence lines, Ch. 8–9
deflections and virtual work, Ch. 10 force (flexibility) method, Ch. 11
slope-deflection, Ch. 12 moment distribution, Ch. 15–16 matrix stiffness.
A. Kassimali, Structural Analysis, 6th ed. (Cengage) — Ch. 7
Castigliano and least work, Ch. 8 influence lines, Ch. 13 slope-deflection,
Ch. 17–18 matrix stiffness. A. Ghali, A. M. Neville and T. G. Brown,
Structural Analysis: A Unified Classical and Matrix Approach, 7th ed.
(CRC). Canadian context for the settlement question: NBC 2020 Part 4 and
CSA S6:19 treat differential support settlement as an imposed deformation to be
combined with the permanent loads, so the self-equilibrating moment set computed
in Question 6 is a real design action, not a curiosity.
Sign convention used throughout.
End moments are written counter-clockwise-positive on the member, which is the
convention that matches the standard six-degree-of-freedom element stiffness
matrix; the slope-deflection equation is then
$M_{ij} = \dfrac{2EI}{L}\left(2\theta_i + \theta_j - 3\psi_{ij}\right) +
\mathrm{FEM}_{ij}$ with $\psi$ the counter-clockwise chord rotation and, for a
downward UDL, $\mathrm{FEM}_{ij} = +wL^2/12$, $\mathrm{FEM}_{ji} = -wL^2/12$.
Ordinary sagging bending moments, which is what every diagram below
plots, are recovered as $M_{\text{sag}}(i) = -M_{ij}$ and
$M_{\text{sag}}(j) = +M_{ji}$. Mixing this with the clockwise-positive
convention of some textbooks produces clean-looking integers that are wrong.
Question 4: Castigliano's theorem — vertical deflection of an
overhang tip (18 marks)
Given. Span $a = 3\ \text{m}$ from the pin A to the roller
B; overhang $b = 2\ \text{m}$ from B to the free tip C; UDL
$w = 12\ \text{kN/m}$ over the whole 5 m; $EI = 5000\ \text{kN}\cdot\text{m}^2$
constant.
Find. The vertical deflection $\delta_C$ of the free tip C,
with its direction.
Question 4: pin at A, roller at B, 2 m overhang to the free tip C, with 12 kN/m over the whole 5 m length.
Approach. The beam is statically determinate, so
Castigliano's first theorem can be applied directly: add a dummy vertical load
$Q$ at C, express the bending moment throughout in terms of $Q$, differentiate,
set $Q = 0$ and integrate. The trap is that $Q$ changes both reactions,
so $\partial M/\partial Q$ is non-zero in the back span as well as on the
overhang.
Reactions with the dummy load in place. With $Q$ acting
downwards at C, moments about A give
$$R_B = \frac{w(a+b)\frac{a+b}{2} + Q(a+b)}{a}
= 50.0 + \frac{5}{3}Q ,\qquad
R_A = w(a+b) + Q - R_B = 10.0 - \frac{2}{3}Q .$$
At $Q = 0$ these are $R_A = 10.0\ \text{kN}$ and $R_B = 50.0\ \text{kN}$, which
already tells the story: the overhang is long enough that the pin is close to
lifting.
Moment expressions and their derivatives. In the back span,
with $x$ measured from A,
$$M(x) = R_A x - \tfrac{1}{2}wx^{2},\qquad
\frac{\partial M}{\partial Q} = \frac{\partial R_A}{\partial Q}\,x
= -\frac{2}{3}x \quad (0 \le x \le 3).$$
On the overhang, with $s$ measured back from the free tip,
$$M(s) = -\tfrac{1}{2}ws^{2} - Qs,\qquad
\frac{\partial M}{\partial Q} = -s \quad (0 \le s \le 2).$$
The first of these is the step candidates most often miss: because the dummy
load alters $R_A$, the back span contributes even though $Q$ is not applied
there.
Apply Castigliano's first theorem. Setting $Q = 0$ after
differentiating,
$$\delta_C = \frac{1}{EI}\left[\int_0^{3}\!\left(10x - 6x^{2}\right)
\left(-\tfrac{2}{3}x\right)\mathrm{d}x
+\int_0^{2}\!\left(-6s^{2}\right)\left(-s\right)\mathrm{d}s\right].$$
Evaluate the two integrals. For the back span,
$$-\tfrac{2}{3}\int_0^{3}\!\left(10x^{2} - 6x^{3}\right)\mathrm{d}x
= -\tfrac{2}{3}\left[\frac{10(27)}{3} - \frac{6(81)}{4}\right]
= -\tfrac{2}{3}\left(90 - 121.5\right) = +21.0\ \text{kN}^2\text{m}^3 .$$
For the overhang,
$$6\int_0^{2} s^{3}\,\mathrm{d}s = 6\left(\frac{16}{4}\right)
= +24.0\ \text{kN}^2\text{m}^3 .$$
Both terms are positive, so both act in the same sense as the dummy load: the
tip goes down.
Deflection at C. Adding the two contributions,
$$\delta_C = \frac{21.0 + 24.0}{EI} = \frac{45.0}{5000}
= 9.00\times10^{-3}\ \text{m}$$
$$\boxed{\delta_C = 9.00\ \text{mm downward}}$$
Why the sign is worth checking. On a UDL-loaded
overhanging beam the free tip does not always deflect down. The tip moves
upward whenever the back span sags enough to rotate the beam over the roller
faster than the overhang droops, and the changeover is at the universal ratio
$b/a = 0.4343$, independent of $w$, of $a$ and of $EI$. Here
$b/a = 2/3 = 0.667$ is well past that threshold, so the downward answer is the
expected one — but on a shorter overhang the same arithmetic returns a
negative number and it is not an error.
Supporting diagram values. The bending moment is hogging
across the whole back span (there is no point of contraflexure between A and B
other than the small sagging lobe near the pin): it rises to
$M_{\max} = R_A^{2}/2w = +4.17\ \text{kN}\cdot\text{m}$ at
$x = R_A/w = 0.833\ \text{m}$ from A, falls through zero and reaches
$M_B = -wb^{2}/2 = -24.0\ \text{kN}\cdot\text{m}$ over the roller, then closes
parabolically to zero at the free tip.
Question 4: bending moment diagram. A small sagging lobe near the pin, then hogging to 24.0 kN.m over the roller.