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16-Civ-B1 Advanced Structural Analysis · May 2013

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. 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.

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)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

Given data
Beam span, free tip $A$ to built-in end $C$$4\text{ m}+6\text{ m}=10\text{ m}$
Uniformly distributed load on $AB$$w = 2\text{ kN/m}$ over the first 4 m
Tie rodfrom $B$ (4 m from the free tip) to the wall, 8 m above the beam
Rod length$L_r=\sqrt{6^{2}+8^{2}} = 10\text{ m}$ (a 6–8–10 triangle)
Beam flexural rigidity$EI = 1.44\times10^{4}\ \text{kN}\cdot\text{m}^{2}$, inextensible
Rod axial rigidity$EA = 1.25\times10^{4}\ \text{kN}$

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.

2 kN/m steel rod beam 4 m 6 m 8 m B A C SFD -8.0 kN +1.6 kN BMD -16.0 kN·m -6.4
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 $\partial U/\partial T = 0$.

  1. 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.
  2. 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.
  3. 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 $$\frac{\partial M}{\partial T}=0.8\,(x-4)\quad\text{on }BC,\qquad \frac{\partial M}{\partial T}=0\quad\text{on }AB .$$
  4. 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 $0\le u\le 6$, $$\int_{0}^{6}\Bigl[-8(u+2)+0.8T\,u\Bigr]\,0.8u\,du = 46.08\,T-691.2 .$$
  5. 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.
  6. 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 $BC$.
  7. 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
QuantityValue
Force in the steel rod12.0 kN tension
Vertical / horizontal components delivered to the beam at $B$ 9.60 kN up / 7.20 kN towards the wall
Reaction at the built-in end $C$1.60 kN downward (hold-down)
Maximum shear in the beam8.00 kN, just left of $B$
Shear in span $BC$+1.60 kN, constant
Maximum bending moment in the beam16.0 kN·m hogging, at $B$
Bending moment at the built-in end $C$6.40 kN·m hogging