Response to the following problem:
Compute the [A], [B], [D], and [H] matrices for the following laminates. All laminae are 1.0 mm thick. Comment on the coupling of the constitutive equations for each case.
one lamina of aluminum (E = 71 GPα, v = 0.3)
one lamina [0]; carbon-epoxy (AS4-3501-6).
[30]; carbon-epoxy
[0/90]T; carbon-epoxy
[0/90]S; carbon-epoxy
[±30]S; carbon-epoxy