GATE AE 2018 • Q16 NAT • 1 Mark

Flight Mechanics & Space Dynamics

Airplane Performance & Stability

Subtopic: Aircraft Stability & Modes

Question Statement:

The highest limit load factor experienced by a civil transport aircraft is in the range (A) 0.0 - 2.0 (B) 2.0 - 5.0 (C) 5.0 - 8.0 (D) 8.0 - 10.0

Official Answer Key:

0.0

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2018 Q.16)** **1. Governing Concept & Syllabus Domain**: This question pertains to **Airplane Performance & Stability** under *Flight Mechanics & Space Dynamics* (1 Mark, NAT). **2. Analytical Calculation**: - Substituting aerodynamic parameters into governing Airplane Performance & Stability equation. **3. Final Answer**: Acceptable official numerical value is **0.0**.

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