Consider an eight-layer [45/0/90]s graphite-reinforced laminate. Compute and plot the components of the A matrix of...

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Consider an eight-layer [45/0/90]s graphite-reinforced laminate. Compute and plot the components of the A matrix of this laminate as it is rotated an angle & in its plane ([45+ /0+ /90+ ]s) at an increment of o=5. Consider the range laminate). - /2 +/2 (this laminate is referred to as a quasi-isotropic A. Plot Aij (i, j = 1,2,6) as a function of p. B. Is the A matrix dependent of o? C. Compare the effective engineering shear modulus, Gxy, with the one calculated from the following expression? Ex Gxy 2(1+ry) Here are the effective Engineering Properties of a Laminate: A11A22 - A2 = A22 H A11A22 - A2 = A11 H A66 Gxy = H A12 Vxy == A22 A12 Vyx = A11 Consider an eight-layer [45/0/90]s graphite-reinforced laminate. Compute and plot the components of the A matrix of this laminate as it is rotated an angle & in its plane ([45+ /0+ /90+ ]s) at an increment of o=5. Consider the range laminate). - /2 +/2 (this laminate is referred to as a quasi-isotropic A. Plot Aij (i, j = 1,2,6) as a function of p. B. Is the A matrix dependent of o? C. Compare the effective engineering shear modulus, Gxy, with the one calculated from the following expression? Ex Gxy 2(1+ry) Here are the effective Engineering Properties of a Laminate: A11A22 - A2 = A22 H A11A22 - A2 = A11 H A66 Gxy = H A12 Vxy == A22 A12 Vyx = A11