Problem 4.4 The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. The cross-sectional areas of sections AB, BC, and CD are AAB=0.08 in². Apc = 0.11 in², and Acp = 0.06 in², respectively. The modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at B and C. (Figure 1) Figure Aluminum E10(10) ksi 2.00 kip Steel Copper E=18(10³) ksi E₁=29(10³) ksi -18 in- 3.50 kip 3.50 kip < 1 of 1 -12 in- 1.75 kip 1+ + 1.75 kip -16 in 150 kip 24 Y Part A SB/c Value Determine the displacement of B with respect to C of the composite shaft. Express your answer to three significant figures and include the appropriate units. Submit Provide Feedback Request Answer Units < 1 of 7 ? > Review Next >
Problem 4.4 The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. The cross-sectional areas of sections AB, BC, and CD are AAB=0.08 in². Apc = 0.11 in², and Acp = 0.06 in², respectively. The modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at B and C. (Figure 1) Figure Aluminum E10(10) ksi 2.00 kip Steel Copper E=18(10³) ksi E₁=29(10³) ksi -18 in- 3.50 kip 3.50 kip < 1 of 1 -12 in- 1.75 kip 1+ + 1.75 kip -16 in 150 kip 24 Y Part A SB/c Value Determine the displacement of B with respect to C of the composite shaft. Express your answer to three significant figures and include the appropriate units. Submit Provide Feedback Request Answer Units < 1 of 7 ? > Review Next >
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Question
The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. The cross-sectional areas of sections AB, BC, and CD are AAB = 0.08 in², ABC = 0.11 in², and Acp = 0.06 in², respectively. The modulus of elasticity for each section are shown in the figure. Neglect the size of the collars at B and C.
![Problem 4.4
The composite shaft, consisting of aluminum, copper,
and steel sections, is subjected to the loading shown.
The cross-sectional areas of sections AB, BC, and
CD are AAB=0.08 in². Apc = 0.11 in², and Acp =
0.06 in², respectively. The modulus of elasticity for
each section are shown in the figure. Neglect the size of
the collars at B and C.
(Figure 1)
Figure
Aluminum
E10(10) ksi
2.00 kip
-18 in
Steel
Copper
E=18(10³) ksi E₁=29(10³) ksi
3.50 kip
< 1 of 1
1.75 kip
1+
+
3.50 kip 1.75 kip
-12 in- -16 in
1.50 kip
▾ Part A
SB/C Value
Determine the displacement of B with respect to C of the composite shaft.
Express your answer to three significant figures and include the appropriate units.
Submit
Provide Feedback
Request Answer
Units
< 1 of 7
?
Review
Next >](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F88b4235c-2b0d-4459-88fc-1ffa51a7c481%2F76dedeee-c1e8-4559-b7cd-59356c2ecf22%2F7z2vga_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Problem 4.4
The composite shaft, consisting of aluminum, copper,
and steel sections, is subjected to the loading shown.
The cross-sectional areas of sections AB, BC, and
CD are AAB=0.08 in². Apc = 0.11 in², and Acp =
0.06 in², respectively. The modulus of elasticity for
each section are shown in the figure. Neglect the size of
the collars at B and C.
(Figure 1)
Figure
Aluminum
E10(10) ksi
2.00 kip
-18 in
Steel
Copper
E=18(10³) ksi E₁=29(10³) ksi
3.50 kip
< 1 of 1
1.75 kip
1+
+
3.50 kip 1.75 kip
-12 in- -16 in
1.50 kip
▾ Part A
SB/C Value
Determine the displacement of B with respect to C of the composite shaft.
Express your answer to three significant figures and include the appropriate units.
Submit
Provide Feedback
Request Answer
Units
< 1 of 7
?
Review
Next >
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