The properties of continuous carbon fiber reinforced epoxy composite laminate are as follows: Elasticity Modulus E...

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The properties of continuous carbon fiber reinforced epoxy composite laminate are as follows: Elasticity Modulus E (GPa) shear modulus G(GPa) Poisson's ratio v Fiber (Ev)252 (E)-30 25 0.32 Epoxy 3,8 2 0.28 Please make the following calculations assuming that it contains no voids and that the fiber volume ratio is 0.6. (a). Calculate the longitudinal modulus, Poisson's ratio, transverse modulus and in-plane shear modulus of the composite. (b). Under a longitudinal force in a composite laminate, determine the proportions in which the axial forces are shared by the fibers and the matrix. (c). Assume the cross-section of the fibers to be circular and determine the maximum possible longitudinal modulus, Poisson's ratio, transverse modulus and in-plane shear modulus of the composite. (D). Please compare the values you found in this question with the values you found in the previous question. The properties of continuous carbon fiber reinforced epoxy composite laminate are as follows: Elasticity Modulus E (GPa) shear modulus G(GPa) Poisson's ratio v Fiber (Ev)252 (E)-30 25 0.32 Epoxy 3,8 2 0.28 Please make the following calculations assuming that it contains no voids and that the fiber volume ratio is 0.6. (a). Calculate the longitudinal modulus, Poisson's ratio, transverse modulus and in-plane shear modulus of the composite. (b). Under a longitudinal force in a composite laminate, determine the proportions in which the axial forces are shared by the fibers and the matrix. (c). Assume the cross-section of the fibers to be circular and determine the maximum possible longitudinal modulus, Poisson's ratio, transverse modulus and in-plane shear modulus of the composite. (D). Please compare the values you found in this question with the values you found in the previous question.