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3.51 The solid cylinders AB and BC are bonded together at B and are attached to fixed supports at A and C. Knowing that the modulus of rigidity is 3.7 x 10° psi for aluminum and 5.6 x 10° psi for brass, determine the maximum shearing stress (a) in cylinder AB, (b) in cylinder BC. Aluminum

3.51 The solid cylinders AB and BC are bonded together at B and are attached to fixed supports at A and C. Knowing that the modulus of rigidity is 3.7 x 10° psi for aluminum and 5.6 x 10° psi for brass, determine the maximum shearing stress (a) in cylinder AB, (b) in cylinder BC. Aluminum

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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3.51 plz
3.51 The solid cylinders AB and BC are bonded together at B and are attached to fixed supports at A and C. Knowing that the modulus of rigidity is 3.7 x 10° psi for aluminum and 5.6 x 10° psi for brass, determine the maximum shearing stress (a) in cylinder AB, (b) in cylinder BC. Aluminum 12 in. 1.5 in. 3.52 Solve Prob. 3.51, assuming that cylinder AB is made of steel, for which G = 11.2 × 10° psi. T= 12.5 kip-in. 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 × 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. Brass 18 in. 2.0 in. Fig. P3.51 3 in.
Transcribed Image Text:3.51 The solid cylinders AB and BC are bonded together at B and are attached to fixed supports at A and C. Knowing that the modulus of rigidity is 3.7 x 10° psi for aluminum and 5.6 x 10° psi for brass, determine the maximum shearing stress (a) in cylinder AB, (b) in cylinder BC. Aluminum 12 in. 1.5 in. 3.52 Solve Prob. 3.51, assuming that cylinder AB is made of steel, for which G = 11.2 × 10° psi. T= 12.5 kip-in. 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 × 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. Brass 18 in. 2.0 in. Fig. P3.51 3 in.
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