The composite shaft shown consists of a 0.2-in.-thick brass jacket (G = 5.6 × 10° psi) bonded to a 1.2-in.-diameter steel core (Gsteel = 11.2 x 10° psi). Knowing that the shaft is subjected to 5-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. 6ft B Brass jacket 1.2 in. - Steel core 0.2 in.
The composite shaft shown consists of a 0.2-in.-thick brass jacket (G = 5.6 × 10° psi) bonded to a 1.2-in.-diameter steel core (Gsteel = 11.2 x 10° psi). Knowing that the shaft is subjected to 5-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. 6ft B Brass jacket 1.2 in. - Steel core 0.2 in.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Step 1
Given :
- A composite shaft consist of 2 in thick brass jacket.
- Diameter of steel core is ,d=1.2 in.
- The shaft is subjected torque ,T=5 kipin
- Inner diameter of brass is d=1.2 in.
- Outer diameter of brass jacket D=1.2 in+0.4 in =1.6 in .
- Modulus of rigidity of the brass is, G brass=5.6106psi.
- Modulus of rigidity of brass is ,Gsteel=11.2106 psi.
Part a:
The formula of maximum shear stress in brass jacket given by:
Therefore maximum shear stress in the brass jacket is 9.094 kip/in2 .
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