Response to the following:
Calculate the [A] matrix of the RVE in Problem 1 at location x = aw/4, y = af/2.
Problem 1: Calculate the reduced stiffness matrix [Q] in laminate coordinates of the fill and warp tows in Problem 2 at location x = aw/4, y = af /2. Compare with the output of 9.16, and make comments.
Problem 2: Calculate the compliance matrix [S] in laminate coordinates at x = aw/4, y = af/2, for the fill and warp tows of sample type 5 in Table.
