Maneuverability in aircraft design refers to an aircraft’s ability to perform various maneuvers, such as turns, rolls, and pitch changes. There isn’t a single formula for maneuverability, as it’s a complex aspect influenced by multiple factors, including control surfaces, aerodynamics, and engine performance.
However, one crucial parameter often considered in maneuverability analysis is the “turning radius.” The formula for turning radius (R) is:
- V is the velocity of the aircraft.
- g is the acceleration due to gravity (approximately 9.81 m/s²).
- ϕ is the bank angle of the aircraft during the turn.