•Consider the fiber-reinforced matrix composite (Carbon fiber). •Find out and show material constants (E1, E2, n12, etc.

[answerhappygod]

•Consider the fiber-reinforced matrix composite (Carbon
fiber).
•Find out and show material constants (E1, E2, n12, etc.) for
your composite material.
•Construct stiffness and compliance matrices for this specific
example.
•Assume that you have a plane stress loading on 2-D example
shown below, material being your composite. After assigning proper
values (up to you) for stress tensors, calculate the corresponding
global strains.
•As the last step, considering your composite consists of only
45 degrees laminas, calculate transformed compliance and stiffness
matrices.