The composite shaft shownconsists of asolid brass segment (1) and a solid aluminum segment (2) that areconnected at flange B and securely attached to rigid walls atA and C. Brass segment (1) has a diameter of 18 mm, a length ofL₁ 235 mm, and a shear modulus of 39 GPa. Aluminum segment(2) has a diameter of 24 mm, a length of L₂ = 165 mm, and a shearmodulus of 28 GPa. If a concentrated torque of 270 N-m is applied toflange B, determine(a) the maximum shear stress magnitudes in segments (1) and (2).(b) the rotation angle of flange B relative to support A.N235 mm(1)B165 mmPartial Ans: Max shear stress in Member 1 is 55.7 MPa270 N-m(2)

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The composite shaft shown consists of a solid brass segment (1) and a solid aluminum segment (2) that are connected at flange B and securely attached to rigid walls at A and C. Brass segment (1) has a diameter of 18 mm, a length of L₁ 235 mm, and a shear modulus of 39 GPa. Aluminum segment (2) has a diameter of 24 mm, a length of L2 = 165 mm, and a shear modulus of 28 GPa. If a concentrated torque of 270 N-m is applied to flange B, determine (a) the maximum shear stress magnitudes in segments (1) and (2). (b) the rotation angle of flange B relative to support A. z 235 mm (1) B 165 mm 270 N-m (2)

The composite shaft shown consists of a solid brass segment (1) and a solid aluminum segment (2) that are connected at flange B and securely attached to rigid walls at A and C. Brass segment (1) has a diameter of 18 mm, a length of L₁ 235 mm, and a shear modulus of 39 GPa. Aluminum segment (2) has a diameter of 24 mm, a length of L2 = 165 mm, and a shear modulus of 28 GPa. If a concentrated torque of 270 N-m is applied to flange B, determine (a) the maximum shear stress magnitudes in segments (1) and (2). (b) the rotation angle of flange B relative to support A. z 235 mm (1) B 165 mm 270 N-m (2)

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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