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Consider a Kevlar-epoxy composite (table of lamina properties in the notes) laminate with the stacking sequence [0/90/0]T where each lamina is 0.01 inches thick.4y(a) Sketch this laminate geometry including fiber orientation angles, thicknesses, layer numbers, and x-y-z coordinate system. (b) Is this laminate symmetric? Why or why not? (c) Calculate [Qbar] for each lamina. Hint 1: some may be the same depending on fiber orientation angle. Hint 2: rotating a lamina 90 degrees is the same as inter

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