A composite assembly consisting of a steel [G = 80 GPa] core (2) connected by rigid plates at the ends of an aluminum [G = 28 GPa]tube(1) is shown. The cross-sectional dimensions of the assembly are shown in the second figure. Assume l = 210 mm, D1= 51, d1 = 35 mm, d2= 21 mm. If a torque of T = 1000 N-m is applied to the composite assembly, determine(a) the maximum shear stress in the aluminum tube and in the steel core.(b) the rotation angle of end B relative to end A.A(1)(2)BL.(1)diDAnswers:(a) Talum =i! MPaTsteel =i! MPa(b) Фв — ФА 3! rad

Given data, Steel G = 80 GPa Aluminum G = 28 Gpa L = 210 mm D1 = 51 mm d1 = 35 mm d2 = 21 mm T =…

A composite assembly consisting of a steel (G = 80 GPa] core (2) connected by rigid plates at the ends of an aluminum [G = 28 GPa] tube (1) is shown. The cross-sectional dimensions of the assembly are shown in the second figure. Assume L = 210 mm, D1 = 51,dy = 35 mm, d2 = 21 mm. If a torque of T = 1000 N-m is applied to the composite assembly, determine (a) the maximum shear stress in the aluminum tube and in thesteel core. (b) the rotation angle of end B relative to end A. A (1) (2) T B L (1) d2 D1 Answers: (a) Talum MPa Tsteel = ! MPa (b) PB - PA = ! rad

A composite assembly consisting of a steel (G = 80 GPa] core (2) connected by rigid plates at the ends of an aluminum [G = 28 GPa] tube (1) is shown. The cross-sectional dimensions of the assembly are shown in the second figure. Assume L = 210 mm, D1 = 51,dy = 35 mm, d2 = 21 mm. If a torque of T = 1000 N-m is applied to the composite assembly, determine (a) the maximum shear stress in the aluminum tube and in thesteel core. (b) the rotation angle of end B relative to end A. A (1) (2) T B L (1) d2 D1 Answers: (a) Talum MPa Tsteel = ! MPa (b) PB - PA = ! rad

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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