Q1A cantilever composite beam is formed by bonding together brass bar (EB = 100 GPa) andaluminium (EA = 70 GPa) with cross section and loading at free end as shown in Figure Q1.Parameter x, y, and z are given by:X=0Y=0Z=2(a)Determine the centroid and the moment of inertia of the composite section.(b)Calculate the maximum tensile and compressive stresses in the brass and aluminium.brass5x mm(10 mm20mm|4y mm0.5(4y) mmM=2.z kN.m4y mmaluminiumFigure Q1|

Above figure is composite beam having different Modulus of elasticity, hence a relation is required…

A cantilever composite beam is formed by bonding together brass bar (EB = 100 GPa) and aluminium (EA = 70 GPa) with cross section and loading at free end as shown in Figure Q1. Parameter x, y, and z are given by: Q1 X=0 Y=0 Z=2 (a) Determine the centroid and the moment of inertia of the composite section. (b) Calculate the maximum tensile and compressive stresses in the brass and aluminium.

A cantilever composite beam is formed by bonding together brass bar (EB = 100 GPa) and aluminium (EA = 70 GPa) with cross section and loading at free end as shown in Figure Q1. Parameter x, y, and z are given by: Q1 X=0 Y=0 Z=2 (a) Determine the centroid and the moment of inertia of the composite section. (b) Calculate the maximum tensile and compressive stresses in the brass and aluminium.

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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