Rate of Turn Formula:
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The Rate of Turn formula calculates the angular velocity at which an aircraft turns, expressed in degrees per second. It is a fundamental equation in aviation that relates bank angle and flight velocity to the aircraft's turning performance.
The calculator uses the Rate of Turn formula:
Where:
Explanation: The formula demonstrates that turn rate is directly proportional to the tangent of the bank angle and inversely proportional to flight velocity. The constant 1091 converts the result to degrees per second.
Details: Accurate turn rate calculation is crucial for flight planning, navigation, and aircraft performance analysis. It helps pilots determine the time required to complete turns and is essential for instrument flight procedures and air traffic control coordination.
Tips: Enter bank angle in radians and flight velocity in knots. Both values must be positive numbers. For best results, ensure bank angle values are within reasonable flight parameters (typically 0-60 degrees converted to radians).
Q1: Why is the constant 1091 used in the formula?
A: The constant 1091 incorporates conversion factors to ensure the result is in degrees per second, accounting for the relationship between angular velocity, bank angle, and airspeed.
Q2: What are typical turn rate values for aircraft?
A: Typical turn rates vary by aircraft type. Commercial aircraft typically turn at 1.5-3° per second, while fighter aircraft can achieve much higher turn rates of 15-25° per second.
Q3: How does bank angle affect turn rate?
A: Increasing bank angle increases turn rate exponentially due to the tangent function in the formula. However, practical limits exist due to structural and physiological constraints.
Q4: Why is flight velocity in the denominator?
A: Higher velocities require more time to complete a turn, resulting in a lower turn rate. This inverse relationship ensures the formula accounts for the increased turning radius at higher speeds.
Q5: Are there limitations to this formula?
A: The formula assumes coordinated turns and level flight. It may not account for factors like wind, aircraft weight, or specific aerodynamic characteristics that can affect actual turn performance.