What is the in-pane shear modulus of the fiber G12f. for a unidirectional carbon/epoxy composite with the in-plane shear modulus of G12=7.6GPa. Assume ==8.5 and the matrix shear modulus and fiber volume ratio to be Gm=1.31GPa, and Vf=0.45, respectively (10) 2. Consider a composite material with E1=E2=E and V12=V21≅0 (woven composite), and determine following: a) The (Vxy)max in terms of E and G12 and b) The corresponding angle θ where the maximum in (a) occurs (2)