The composite shaft shown consists of a 0.2-in.-thick

Chapter 3, Problem 3.53

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The composite shaft shown consists of a 0.2-in.-thick brass jacket \(\left(G=5.6 \times 10^{6} \mathrm{psi}\right)\) bonded to a 1.2-in.-diameter steel core \(\left(G_{\text {steel }}=11.2 \times 10^{6} \mathrm{psi}\right)\). Knowing that the shaft is subjected to \(5 \text { kip·in. }\) torques, determine (a) the maximum shearing stress in the brass jacket, (b) the maximum shearing stress in the steel core, (c) the angle of twist of end B relative to end A.

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