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
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ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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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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