GATE AE 2025 • Q23
MCQ • 1 Mark
Flight Mechanics & Space Dynamics
Airplane Performance & Stability
Subtopic: Aircraft Stability & Modes
Question Statement:
For a general aviation airplane, which one of the following has a destabilizing
effect on its static roll stability?
Options:
-
(A) Wing with a positive dihedral angle
-
(B) Fuselage with a high wing
-
(C) Fuselage with a low wing
-
(D) Swept back wing
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2025 Q.23)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Airplane Performance & Stability** under *Flight Mechanics & Space Dynamics* (1 Mark, MCQ).
**2. Aerospace Engineering Deduction**:
- Applying standard governing principles of Airplane Performance & Stability.
- Option **(A)** matches the analytical derivation and official criteria.
**3. Final Answer**:
Correct Option is **(A)**.
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