Angular velocity for a high-performance fighter calculator

Angular velocity for a high-performance fighter refers to the rate at which the aircraft rotates around its center of mass. It is a measure of how quickly the aircraft changes its orientation or attitude in space. Angular velocity is typically measured in radians per second (rad/s) or degrees per second (°/s). The formula to calculate Angular velocity for high-performance aircraft as follows:

Where:

• $\omega$ is the angular velocity (in radians per second),
• $g$ is the acceleration due to gravity (approximately 9.81 m/s²),
• $\rho$ is the air density (in kilograms per cubic meter),
• CL​ is the lift coefficient (dimensionless),
• $W$ is the weight of the aircraft (in newtons),
• $S$ is the wing area (in square meters),
• $n$ is the load factor (dimensionless).
• W/S is the wing loading (N/m²).