Q2: A composite component consists of a glass fiber and an epoxy matrix. The glass fiber weight fraction is triple of the epoxy weight fraction. Use the given properties of epoxy and glass to determine 1. The composite axial modulus, transverse modulus, major Poisson's ratio, and in- plane shear modulus 2. If the total load is 24 kN and the applied stress is 60 MPa in this axial direction, compute the cross-sectional area of the composite and the magnitude of the load carried by each of the fiber and matrix phases Given: Glass py-2.5 g/cm'. Ey-Ey-80 GPa, vy-0.2, G-38 GPa epoxy P 1.2 g/cm. EE-3.5 GPa vy-0.3, G-1.35 GPa

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Q2: A composite component consists of a glass fiber and an epoxy matrix. The
glass fiber weight fraction is triple of the epoxy weight fraction. Use the given
properties of epoxy and glass to determine:
1. The composite axial modulus, transverse modulus, major Poisson's ratio, and in-
plane shear modulus
2. If the total load is 24 kN and the applied stress is 60 MPa in this axial direction,
compute the cross-sectional area of the composite and the magnitude of the load
carried by each of the fiber and matrix phases.
Given: Glass py-2.5 g/cm'. Ey-Ey-80 GPa, vy-0.2, G-38 GPa
epoxy P 1.2 g/cm³, E-, E-3.5 GP, vy-0.3, G-1.35 GPa
Transcribed Image Text:Q2: A composite component consists of a glass fiber and an epoxy matrix. The glass fiber weight fraction is triple of the epoxy weight fraction. Use the given properties of epoxy and glass to determine: 1. The composite axial modulus, transverse modulus, major Poisson's ratio, and in- plane shear modulus 2. If the total load is 24 kN and the applied stress is 60 MPa in this axial direction, compute the cross-sectional area of the composite and the magnitude of the load carried by each of the fiber and matrix phases. Given: Glass py-2.5 g/cm'. Ey-Ey-80 GPa, vy-0.2, G-38 GPa epoxy P 1.2 g/cm³, E-, E-3.5 GP, vy-0.3, G-1.35 GPa
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