2. 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 D 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 El=10(10³) ksi AAB=0.09 in² 2.00 kip A 18 in.- Copper Ecu=18(10³) ksi ABC = 0.12 in² 3.50 kip 3.50 kip -12 in. Steel Est = 29(10³) ksi ACD= 0.06 in² 1.75 kip 1.75 kip 16 in- 1.50 kip
2. 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 D 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 El=10(10³) ksi AAB=0.09 in² 2.00 kip A 18 in.- Copper Ecu=18(10³) ksi ABC = 0.12 in² 3.50 kip 3.50 kip -12 in. Steel Est = 29(10³) ksi ACD= 0.06 in² 1.75 kip 1.75 kip 16 in- 1.50 kip
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
Related questions
Question
![2. 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 D 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
El=10(10³) ksi
AAB=0.09 in²
2.00 kip
A
18 in.-
Copper
Ecu=18(10³) ksi
ABC = 0.12 in²
3.50 kip
3.50 kip
-12 in.
Steel
Est = 29(10³) ksi
ACD= 0.06 in²
1.75 kip
1.75 kip
16 in-
1.50 kip](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F819d3e0a-e266-4033-850c-e43fe39a5a37%2F73bdcc94-c7b6-464c-a922-78238755163a%2Frmhk66_processed.jpeg&w=3840&q=75)
Transcribed Image Text:2. 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 D 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
El=10(10³) ksi
AAB=0.09 in²
2.00 kip
A
18 in.-
Copper
Ecu=18(10³) ksi
ABC = 0.12 in²
3.50 kip
3.50 kip
-12 in.
Steel
Est = 29(10³) ksi
ACD= 0.06 in²
1.75 kip
1.75 kip
16 in-
1.50 kip
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