Discussion
Which of these is NOT a limitation of classical laminate theory?
Answer: C
Correct answer: It cannot compute the in-plane stiffness of a laminate
Computing the in-plane stiffness is exactly what classical laminate theory does best - the A matrix is its principal output and it is reliable. The other three are genuine limitations: no free-edge interlaminar stresses, an assumed perfect bond between plies, and plane stress in each ply, the last of which is the source of the first.
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