PROBLEM 3.52 A 4 kNm torque T is applied at end A of the composite shaft shown. Knowing that the shear modulus is 77 GPa for the steel and 27 GPa for the aluminium, determine (a) the maximum shear stress in the steel core, (b) the maximum shear stress in the aluminium jacket, and (c) the angle of twist at A. [Ans. (a) 73.6 MPa (b) 34.4 MPa (c) 5.07°] Hint: angle of twist at end A is same for core and jacket 72 mm 54 mm 2.5 m Steel core Aluminium jacket Fig. P3.52 and P3.53 22 14/04/20

Elements Of Electromagnetics
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PROBLEM 3.52
A 4 kNm torque T is applied at end A of the composite shaft shown.
Knowing that the shear modulus is 77 GPa for the steel and 27 GPa
for the aluminium, determine (a) the maximum shear stress in the
steel core, (b) the maximum shear stress in the aluminium jacket,
and (c) the angle of twist at A.
[Ans. (a) 73.6 MPa (b) 34.4 MPa (c) 5.07°]
Hint: angle of twist at
72 mm
end A is same for core
and jacket
54 mm
A
2.5 m
Steel core
Aluminium jacket
Fig. P3.52 and P3.53
22:35
BANG & OLUFSEN
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Transcribed Image Text:PROBLEM 3.52 A 4 kNm torque T is applied at end A of the composite shaft shown. Knowing that the shear modulus is 77 GPa for the steel and 27 GPa for the aluminium, determine (a) the maximum shear stress in the steel core, (b) the maximum shear stress in the aluminium jacket, and (c) the angle of twist at A. [Ans. (a) 73.6 MPa (b) 34.4 MPa (c) 5.07°] Hint: angle of twist at 72 mm end A is same for core and jacket 54 mm A 2.5 m Steel core Aluminium jacket Fig. P3.52 and P3.53 22:35 BANG & OLUFSEN delete home end og up pg dn num backspace 4 lock Q WE T U 080 home pg up
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