SOM The torsional assembly shown in figure below consists of a solid bronze (Gg = 45 GPa) shaft CDand a hollow aluminum alloy (GA = 28 GPa) shaft EF that has a steel (Gs = 80 GPa) core. The endsC and F are fixed to rigid walls, and the steel core of shaft EF is connected to the flange at E sothat the aluminum and steel parts act as a unit. The two flanges D and E are bolted together, andthe bolt clearance permits flange D to rotate through 0.03 rad before EF carries any of the load.Determine the maximum shearing stress in each of the shaft materials when the torque T = 54kN-m is applied to flange D. Hint: Ototali = OC/D + D/E + 0E/F = 0Answer: Shear stress of aluminium, bronze and steel are 52.9 MPa, 100.0 MPa and 75.6 MPa,respectively120 mm2 mBronzeDT= 54 kN-mE120 mmSteel60 mm1.4 mAlum, alloy4

It is asked to find shear stress in Aluminium, Bronze and Steel.

The torsional assembly shown in figure below consists of a solid bronze (GB = 45 GPa) shaft C and a hollow aluminum alloy (GA = 28 GPa) shaft EF that has a steel (Gs = 80 GPa) core. The en C and F are fixed to rigid walls, and the steel core of shaft EF is connected to the flange at E that the aluminum and steel parts act as a unit. The two flanges D and E are bolted together, ar the bolt clearance permits flange D to rotate through 0.03 rad before EF carries any of the loa Determine the maximum shearing stress in each of the shaft materials when the torque T = 5 kN-m is applied to flange D. Hint: 0total = 0C/D + 0D/E + 8E/F = 0 Answer: Shear stress of aluminium, bronze and steel are 52.9 MPa, 100.0 MPa and 75.6 MPC respectively

The torsional assembly shown in figure below consists of a solid bronze (GB = 45 GPa) shaft C and a hollow aluminum alloy (GA = 28 GPa) shaft EF that has a steel (Gs = 80 GPa) core. The en C and F are fixed to rigid walls, and the steel core of shaft EF is connected to the flange at E that the aluminum and steel parts act as a unit. The two flanges D and E are bolted together, ar the bolt clearance permits flange D to rotate through 0.03 rad before EF carries any of the loa Determine the maximum shearing stress in each of the shaft materials when the torque T = 5 kN-m is applied to flange D. Hint: 0total = 0C/D + 0D/E + 8E/F = 0 Answer: Shear stress of aluminium, bronze and steel are 52.9 MPa, 100.0 MPa and 75.6 MPC respectively

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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