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1.0 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 end 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. Also, determine the displacement of B with respect to C of the composite shaft.

1.0 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 end 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. Also, determine the displacement of B with respect to C of the composite shaft.

Structural Analysis
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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1.0 The composite shaf, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. Determine the displacement of end A with respect to end 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. Also, determine the displacement of B with respect to C of the composite shaft. Aluminum Copper Eeu = 18(10°) ksi ABC = 0.12 in? Steel E = 10(103) ksi AAB = 0.09 in? E = 29(103) ksi AcD = 0.06 in? 3.75 kip 2.00 kip 3.00 kip 1.50 kip BL 3.75kip D 2.00kip 18 in.- 12 in.- 16 in:
Transcribed Image Text:1.0 The composite shaf, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. Determine the displacement of end A with respect to end 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. Also, determine the displacement of B with respect to C of the composite shaft. Aluminum Copper Eeu = 18(10°) ksi ABC = 0.12 in? Steel E = 10(103) ksi AAB = 0.09 in? E = 29(103) ksi AcD = 0.06 in? 3.75 kip 2.00 kip 3.00 kip 1.50 kip BL 3.75kip D 2.00kip 18 in.- 12 in.- 16 in:
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