Question 3 of 9: Least-work analysis of a tie-rod-propped beam (Castigliano)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 07-Str-A4 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 3: Least-work analysis of a tie-rod-propped beam (Castigliano) (16 marks)
Find. The force in the tie rod by the least-work theorem, then the
maximum shear force and the maximum bending moment in the beam, and the two diagrams.
Q3 — tie-rod-propped cantilever, and the resulting shear force and bending moment diagrams for the beam.
Approach. The structure is once statically indeterminate; take the rod
force $T$ as the redundant, write the beam moment and the rod energy in terms of $T$, and
impose the least-work condition $\partial U/\partial T = 0$.
Confirm the degree of indeterminacy. The beam is built in at $C$ (three
reaction components), the rod is a two-force member pinned at both ends, and the left end of
the beam is free. Counting reaction components and members against the equations of
equilibrium leaves one redundant, so a single compatibility condition — here supplied
by Castigliano's second theorem in its least-work form — closes the problem.
Resolve the rod force at the joint. The rod runs from $B$ at
$(4,\,0)$ to the wall at $(10,\,8)$, so its direction cosines are
$$c_x=\frac{6}{10}=0.6,\qquad c_y=\frac{8}{10}=0.8 .$$
A tension $T$ therefore lifts the beam at $B$ with a vertical component $0.8T$ and pushes it
towards the wall with a horizontal component $0.6T$. The beam is inextensible, so the
horizontal component does no work and does not enter the compatibility equation.
Write the bending moment as a function of $T$. Measuring $x$ from the
free tip and taking the left-hand free body (sagging positive),
$$M(x) = -\frac{wx^{2}}{2}\quad (0\le x\le 4),\qquad
M(x) = -wa\!\left(x-\tfrac{a}{2}\right)+0.8T\,(x-4)\quad (4\le x\le 10),$$
with $a=4\text{ m}$ and $wa=8\text{ kN}$. Only the second expression depends on the
redundant, and
$$\frac{\partial M}{\partial T}=0.8\,(x-4)\quad\text{on }BC,\qquad
\frac{\partial M}{\partial T}=0\quad\text{on }AB .$$
Apply the least-work theorem. The total strain energy is the beam
bending energy plus the rod axial energy, and the redundant takes the value that minimises
it:
$$\frac{\partial U}{\partial T}
=\frac{1}{EI}\int_{4}^{10} M\,\frac{\partial M}{\partial T}\,dx
+\frac{T L_r}{EA}=0 .$$
Substituting $u=x-4$ and integrating over $0\le u\le 6$,
$$\int_{0}^{6}\Bigl[-8(u+2)+0.8T\,u\Bigr]\,0.8u\,du = 46.08\,T-691.2 .$$
Solve for the rod force. Inserting the rigidities,
$$\frac{46.08\,T-691.2}{1.44\times10^{4}}+\frac{10\,T}{1.25\times10^{4}}=0
\;\Longrightarrow\; 0.0032\,T-0.048+0.0008\,T=0 ,$$
$$\boxed{T = 12.0\ \text{kN (tension)} .}$$
The vertical component is $0.8T=9.60\text{ kN}$ upward and the horizontal component is
$0.6T=7.20\text{ kN}$ towards the wall.
Complete the equilibrium of the beam. The total applied load is
$wa=8.0\text{ kN}$ downward while the rod lifts $9.60\text{ kN}$, so the built-in end must
pull the beam down:
$$R_C = 8.0-9.60 = -1.60\ \text{kN}\ (\text{i.e. }1.60\text{ kN downward}) .$$
The shear (taking upward forces to the left of the section as positive) is therefore
$V=-2x$ over $AB$, reaching $-8.00\text{ kN}$ just left of $B$, and then jumps by
$+9.60\text{ kN}$ to a constant $+1.60\text{ kN}$ over $BC$.
Evaluate the bending moments. On the overhang the moment is the
cantilever parabola $M=-x^{2}$, so at the rod joint
$$M_B = -\frac{2\times4^{2}}{2}=-16.0\ \text{kN}\cdot\text{m} ,$$
and beyond $B$ the moment rises linearly at the constant shear rate:
$$M_C = -16.0 + 1.60\times 6 = -6.40\ \text{kN}\cdot\text{m} .$$
Both are hogging. The largest values are
$$\boxed{\left|M\right|_{\max}=16.0\ \text{kN}\cdot\text{m at }B,\qquad
\left|V\right|_{\max}=8.00\ \text{kN just left of }B .}$$
Final results — Question 3
Quantity
Value
Force in the steel rod
12.0 kN tension
Vertical / horizontal components delivered to the beam at $B$