22-Mec-A7 Advanced Strength of Materials · December 2013
Question 4 of 7: Beam Deflection at B by Castigliano’s Theorem
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Exams, December 2013 — 07-Mech-A7 Advanced Strength of Materials. Open-book, 3 hours; any five of the seven problems constitute a complete paper and all problems are of equal value. All seven problems are solved as a study resource.
Reference texts. R.C. Hibbeler, Mechanics of Materials, 10th ed. (thermal & indeterminate axial members Ch. 4, plane stress/strain Ch. 9–10, energy methods Ch. 14); A.P. Boresi & R.J. Schmidt, Advanced Mechanics of Materials, 6th ed. (thick-walled cylinders Ch. 11, thin-walled open sections & torsional buckling Ch. 6&12); J.M. Gere & B.J. Goodno, Mechanics of Materials (strain rosettes, columns). Yield criteria follow the von Mises and Tresca formulations standard to these texts.
Question 4: Beam Deflection at B by Castigliano’s Theorem (20 marks)
Given. A simply supported beam C–A (span 9 m) with a full-span UDL and an end couple, deflection sought at the interior point B.
Given data
Flexural rigidity
E = 210 GPa, I = 285×106 mm4 ⇒ EI = 59 850 kN·m2
Uniform load
w = 10 kN/m over the entire span 0 ≤ x ≤ 9 m
Applied couple at A
M = 20 kN·m (clockwise, at x = 9 m)
Point of interest
B at x = 5 m from C
Find. The vertical displacement of point B.
Full-span UDL plus an end couple at roller A; deflection sought at interior point B (x = 5 m).
Approach. Castigliano’s deflection theorem δB = ∫ (M/EI)(∂M/∂Q) dx is applied with a dummy load Q at B. Since no real point load acts at B, the operation is equivalent to the unit-load method: form M(x), the sensitivity ∂M/∂Q, integrate, then set Q = 0.
Support reactions. Taking the clockwise couple as negative and moments about C,
$$R_A=\frac{w L^{2}/2+M}{L}=\frac{10(9)^2/2+20}{9}=47.22\ \text{kN},\qquad R_C=wL-R_A=42.78\ \text{kN}.$$
Real bending moment. Measuring x from C (the end couple enters only through the reactions),
$$M(x)=R_Cx-\tfrac{w}{2}x^{2}=42.78\,x-5\,x^{2},$$
which correctly returns $M(9)=-20$ kN·m at the applied couple.
Sensitivity to a dummy load at B. A downward Q at x = 5 raises $\partial R_C/\partial Q=\tfrac{4}{9}$, giving
$$\frac{\partial M}{\partial Q}=\begin{cases}\tfrac{4}{9}\,x, & 0\le x\le 5\\[2pt]\tfrac{4}{9}\,x-(x-5)=\tfrac{5}{9}(9-x), & 5\le x\le 9.\end{cases}$$
Evaluate the integral. Combining the two spans,
$$\int_0^{9} M\,\frac{\partial M}{\partial Q}\,dx=\int_0^{5}(42.78x-5x^{2})\tfrac{4}{9}x\,dx+\int_5^{9}(42.78x-5x^{2})\tfrac{5}{9}(9-x)\,dx=738.0\ \text{kN}\cdot\text{m}^{3}.$$
Deflection. Dividing by EI,
$$\boxed{\delta_B=\frac{738.0}{59\,850}=0.01233\ \text{m}=12.3\ \text{mm (downward).}}$$