GATE AE 2011 • Q32 NAT • 1 Mark

Aerospace Structures

Structural Mechanics

Subtopic: Thin-Walled Shells & Buckling

Question Statement:

(A) 0 and 0ab (B) 0 and 0ab (C) 0 and 0ab  (D) 0 and 0ab The solution of 32tdy y etdt  with initial condition 1 ) 0 (y is given by (A) 21 (3 )9 tet  (B) 2 9 52( 2 2 )tet t 

Official Answer Key:

0.0

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2011 Q.32)** **1. Governing Concept & Syllabus Domain**: This question pertains to **Structural Mechanics** under *Aerospace Structures* (1 Mark, NAT). **2. Analytical Calculation**: - Substituting aerodynamic parameters into governing Structural Mechanics equation. **3. Final Answer**: Acceptable official numerical value is **0.0**.

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