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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 × 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 Aluminum Fig. P3.53 and P3.54 100 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 × 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 Aluminum Fig. P3.53 and P3.54 100 in.

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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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 × 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 Aluminum Fig. P3.53 and P3.54 100 in.
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 × 10 psi for steel and 4 × 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 Aluminum Fig. P3.53 and P3.54 100 in.
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