GATE AE 2014 • Q42 NAT • 2 Marks

Aerospace Structures

Structural Mechanics

Subtopic: Thin-Walled Shells & Buckling

Question Statement:

A cantilevered beam is subjected to a parabolic distribution of shear traction at the right edge while the top and bottom surfaces are traction free. To solve this problem, following Airy's stress function is proposed: 𝜙𝜙 = CC1xxyy + CC2xxyy3 + CC3xx2yy2 + CC4xx3yy. This is an admissible Airy's function that would satisfy the bi-harmonic equation as well as the boundary conditions if and only if (A)CC1 = 0,CC2 = 𝜆𝜆, CC3 = 0, CC4 = 𝜆𝜆 3dd2 (B)CC1 = 𝜆𝜆,CC2 = 𝜆𝜆 3dd2, CC3 = 0, CC4 = 0 (C)CC1 = 0,CC2 = 0, CC3 = 𝜆𝜆,CC4 = - 𝜆𝜆 3dd2 (D)CC1 = 𝜆𝜆,CC2 = - 𝜆𝜆 3dd2, CC3 = 0,CC4 = 0

Official Answer Key:

0.0

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2014 Q.42)** **1. Governing Concept & Syllabus Domain**: This question pertains to **Structural Mechanics** under *Aerospace Structures* (2 Marks, 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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