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

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

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Q2: A composite material has a cross-sectional area of 1150 mm². The fibers carried a stress of 200 MPa and a force of 78600 N and the total longitudinal strain is (1.56 x 10³). The matrix carried a stress of 6.18 MPa. i. Find force carried by the matrix. ii. Find the modulus of elasticity in the longitudinal direction and the modulus of elasticity for the fiber and the matrix.
FIND: MODULUS OF ELASTICITY
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