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
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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