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.
(a) one lamina of aluminum (E = 71 GP a, ν = 0.3)
(b) one lamina [0]; carbon-epoxy (AS4-3501-6).
(c) [30]; carbon-epoxy
(d) [0/90]T ; carbon-epoxy
(e) [0/90]S; carbon-epoxy
(f ) [±30]S; carbon-epoxy