A torque T = 40 kip-in. is applied at end A of the composite shaft shown. Knowing that the modulus of rigidity is 11.2 x 10° psi for steel and 4 x 10° psi for aluminum, determine (a) the maximum shearing stress in the steel core, (b) the maximum stress in the alu- minum shell, (c) the angle of twist at A. 3 in. 2 in. Steel- 100 in. Aluminum

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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3.53 plz
3.53 A torque T = 40 kip-in. is applied at end A of the composite shaft
shown. Knowing that the modulus of rigidity is 11.2 x 10° psi for
steel and 4 x 10° psi for aluminum, determine (a) the maximum
shearing stress in the steel core, (b) the maximum stress in the alu-
minum shell, (c) the angle of twist at A.
3 in.
2 in.
Steel
100 in.
Aluminum
Fig. P3.53 and P3.54
Transcribed Image Text:3.53 A torque T = 40 kip-in. is applied at end A of the composite shaft shown. Knowing that the modulus of rigidity is 11.2 x 10° psi for steel and 4 x 10° psi for aluminum, determine (a) the maximum shearing stress in the steel core, (b) the maximum stress in the alu- minum shell, (c) the angle of twist at A. 3 in. 2 in. Steel 100 in. Aluminum Fig. P3.53 and P3.54
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