04 For the composite section shown in Fig.P4-04 a torque T = 8,000 N.m is applied at end B. If G = 79 GPa for steel and 26 GPa for aluminum, đetermine (a) the maximum shearing stress in the steel core, (b) the maximum shearing stress in the aluminum shell, and the angle of twist at B. -80 mm 60 mm Steel Aluminum Fig. -04 2.50 m

Structural Analysis
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ISBN:9781337630931
Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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04 For the composite section shown in Fig.P4-04 a torque
T = 8,000 N.m is applied at end B. IfG = 79 GPa for steel
and 26 GPa for aluminum, determine (a) the maximum shearing
stress in the steel core, (b) the maximum shearing stress in
the aluminum shell, and the angle of twist at B.
80 mm
*60 mm
Steel
Aluminum
Fig.
-04
B
2.50 m
Transcribed Image Text:04 For the composite section shown in Fig.P4-04 a torque T = 8,000 N.m is applied at end B. IfG = 79 GPa for steel and 26 GPa for aluminum, determine (a) the maximum shearing stress in the steel core, (b) the maximum shearing stress in the aluminum shell, and the angle of twist at B. 80 mm *60 mm Steel Aluminum Fig. -04 B 2.50 m
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