The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. Determine the displacement of end A with respect to endD and the normal stress in each section. The cross-sectional area and modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at B and C. Aluminum Соpper Steel Ey = 70 GPa AAB= 58 mm? Ecu = 126 GPa Anc = 77 mm? Eg = 200 GPa Acp= 39 mm? 16 kN 8 kN 9kN 7 kN 16 kN 8 kN 450 mm -300 mm- 400 mm

The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. Determine the displacement of end A with respect to endD and the normal stress in each section. The cross-sectional area and modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at B and C. Aluminum Соpper Steel Ey = 70 GPa AAB= 58 mm? Ecu = 126 GPa Anc = 77 mm? Eg = 200 GPa Acp= 39 mm? 16 kN 8 kN 9kN 7 kN 16 kN 8 kN 450 mm -300 mm- 400 mm

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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