Problem 9.7-7 The tapered cantilever beam AB shown in the figure has thin-walled, hollow circular cross sections of constant thickness t. The diameters at the ends A and B are d and dg = 2da, respectively. Thus, the diameter d and moment of inertia I at distance x from the free end are, respectively, da dg= 2da d = * (L + x) L d (L + x)³ 8L3 (L + x)3 8 L in which I, is the moment of inertia at end A of the beam. Determine the equation of the deflection curve and the deflection 8 , at the free end of the beam due to the load P.

Problem 9.7-7 The tapered cantilever beam AB shown in the figure has thin-walled, hollow circular cross sections of constant thickness t. The diameters at the ends A and B are d and dg = 2da, respectively. Thus, the diameter d and moment of inertia I at distance x from the free end are, respectively, da dg= 2da d = * (L + x) L d (L + x)³ 8L3 (L + x)3 8 L in which I, is the moment of inertia at end A of the beam. Determine the equation of the deflection curve and the deflection 8 , at the free end of the beam due to the load P.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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