The tapered cantilever beam AB shown in the figure has thin-walled, hollow circular cross sections of constant
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The diameters at the ends A and B are dA and dB = 2dA, respectively. Thus, the diameter d and moment of inertia I at distance x from the free end are, respectively,
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in which IA is the moment of inertia at end A of the beam. Determine the equation of the deflection curve and the deflection δA at the free end of the beam due to the load P.
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