22-Mec-A7 Advanced Strength of Materials · May 2013
Question 1 of 8: Beam Displacement by an Energy Method
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Exams, May 2013 — 07-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours; any five of the eight problems constitute a complete paper and all problems are of equal value. All eight problems are solved as a study resource.
Reference texts: A. C. Ugural & S. K. Fenster, Advanced Strength and Applied Elasticity, 4th ed.; A. P. Boresi & R. J. Schmidt, Advanced Mechanics of Materials, 6th ed.; R. C. Hibbeler, Mechanics of Materials, 10th ed.; S. P. Timoshenko & J. M. Gere, Theory of Elastic Stability, 2nd ed.
Question 1: Beam Displacement by an Energy Method (20 marks)
Given. A simply supported beam CA (pin at C, roller at A), span 7 m, carrying the data below.
Given data
Flexural rigidity
E = 200 GPa, I = 185×106 mm4 ⇒ EI = 37 000 kN·m2
Uniform load (over C–B)
w = 5 kN/m, on 0 ≤ x ≤ 4 m
Applied couple at A
M = 11 kN·m (clockwise, at x = 7 m)
Point of interest
B at x = 4 m (distributed-load cut-off)
Find. The vertical displacement of point B, using an energy (unit-load / Castigliano) method.
Simply supported beam: UDL over span C–B (4 m) and an applied couple at roller A; deflection sought at B.
Approach. Compute the reactions, write the real bending moment M(x); apply a virtual unit downward load at B to obtain m(x); the deflection follows from the unit-load form of the strain-energy theorem, δB = ∫ M m /(EI) dx.
Support reactions. With the clockwise couple taken as negative, vertical equilibrium and moments about C give
$$R_A=\frac{w\!\cdot\!4\,(2)-M}{7}=\frac{20(2)-11}{7}=7.286\ \text{kN},\qquad R_C=20-R_A=12.714\ \text{kN}.$$
Real bending moment. Measuring x from C,
$$M(x)=\begin{cases}12.714\,x-2.5\,x^{2}, & 0\le x\le 4\\[2pt]12.714\,x-20\,(x-2), & 4\le x\le 7\end{cases}$$
which correctly returns $M(7)=-11$ kN·m at the applied couple.
Virtual system. Remove the real loads and apply a unit downward force at B (x = 4). Its reactions are $\bar r_C=\tfrac{3}{7}$, $\bar r_A=\tfrac{4}{7}$, so
$$m(x)=\begin{cases}\tfrac{3}{7}\,x, & 0\le x\le 4\\[2pt]\tfrac{4}{7}\,(7-x), & 4\le x\le 7.\end{cases}$$
Evaluate the integral. Combining the two spans,
$$\int_0^{7}\! M\,m\;dx=\int_0^{4}\!\Big(12.714x-2.5x^{2}\Big)\tfrac{3}{7}x\,dx+\int_4^{7}\!\Big(-7.286x+40\Big)\tfrac{4}{7}(7-x)\,dx=56.86\ \text{kN}\cdot\text{m}^{3}.$$
Deflection. Dividing by the flexural rigidity,
$$\delta_B=\frac{1}{EI}\int_0^{7}M\,m\,dx=\frac{56.86}{37\,000}=1.537\times10^{-3}\ \text{m}.$$
$$\boxed{\delta_B \approx 1.54\ \text{mm (downward)}}$$
Question 1 — results
Quantity
Value
Reactions RC, RA
12.71 kN, 7.29 kN
∫ M m dx
56.86 kN·m3
Displacement of B
1.54 mm downward
Check: the applied couple is read from the figure as clockwise; a counter-clockwise couple would give RA = 4.14 kN and δB ≈ 2.6 mm. The clockwise reading is used throughout.