GATE_AE_2027_MOCK_01_Q64
GATE 2027 Aerospace Engineering All-India Master Mock 01 (Foundation & Standard Core Calibration)
MCQ · 2 Marks
Aerospace Structures • Aerospace Materials & Fatigue • Composite Materials & Laminate Theory
In a symmetric cross-ply $[0/90]_s$ laminate, which of the following terms in the classical laminate $[A][B][D]$ stiffness matrices is strictly EQUAL TO ZERO?
(A) All coupling stiffness terms $B_{ij} = 0$, and in-plane shear coupling terms $A_{16} = A_{26} = 0$
(B) The extensional modulus term $A_{11}$
(C) The bending stiffness term $D_{22}$
(D) The transverse shear term $A_{44}$
Answer Key:
A
Step-by-Step Verified Solution
### Solution: Symmetry eliminates $[B]$ entirely ($B_{ij} = 0$). Cross-ply ($0^\circ$ and $90^\circ$ only) eliminates shear-extension coupling ($A_{16} = A_{26} = 0$) and bend-twist coupling ($D_{16} = D_{26} = 0$). Correct: A.