The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. The cross-se

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The composite shaft, consisting of aluminum, copper, and steel sections, is subjected to the loading shown. The cross-se

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The Composite Shaft Consisting Of Aluminum Copper And Steel Sections Is Subjected To The Loading Shown The Cross Se 1
The Composite Shaft Consisting Of Aluminum Copper And Steel Sections Is Subjected To The Loading Shown The Cross Se 1 (70.02 KiB) Viewed 34 times
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 = 0.07 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 E = 10(10³) ksi 2.00 kip A -18 in- Copper Steel Eu=18(10³) ksi E = 29(10³) ksi B 3.50 kip 1.75 kip 1 of 1 > c 1.75 kip 3.50 kip -12 in-16 in 1.50 kip Part A Determine the normal stress in section AB. Express your answer to three significant figures and include the appropriate units. Enter negative value in the case of compression and positive value in the case of tension. AB= 16 0 Part B Submit Previous Answers Request Answer OBC= μÀ ← Submit ksi X Incorrect; Try Again; 6 attempts remaining - 55 ***** Determine the normal stress in section BC. Express your answer to three significant figures and include the appropriate units. Enter negative value in the case of compression and positive value in the case of tension. μÅ 3 ksi ? www Previous Answers Request Answer ? X Incorrect; Try Again; 9 attempts remaining
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 = 0.07 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 E = 10(10³) ksi 2.00 kip A -18 in- Copper Eu=18(10³) ksi B 3.50 kip 13.50 kip -12 in- Steel Est = 29(10³) ksi 1.75 kip 1.75 kip 1 of 1 > 16 in- 1.50 kip ← D Submit X Incorrect; Try Again; 9 attempts remaining Part C Determine the normal stress in section CD. Express your answer to three significant figures and include the appropriate units. Enter negative value in the case of compression and positive value in the case of tension. Submit Previous Answers Request Answer Part D OCD = Value CO Submit μA Request Answer O ■* Provide Feedback Determine the displacement of end A with respect to end D. Express your answer to three significant figures and include the appropriate units. SA/D = Value μà Request Answer Units Pearson ? Units ? Next >
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