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SYMMETRIC laminate (about the mid-plane) is required to:
A{'text': 'Reduce weight', 'label': 'A'}
B{'text': "Eliminate BENDING-EXTENSION coupling — so in-plane loads don't cause out-of-plane bending", 'label': 'B'}
C{'text': 'Increase strength only', 'label': 'C'}
D{'text': 'Make it cheaper', 'label': 'D'}
Answer & Solution
Correct answer: B. {'text': "Eliminate BENDING-EXTENSION coupling — so in-plane loads don't cause out-of-plane bending", 'label': 'B'}
Symmetric stacking ⇒ B-matrix in classical lamination theory vanishes. In-plane loads produce only in-plane strains, no bending; bending moments produce only curvature, no in-plane strain. Critical for predictable behavior.
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