How to Calculate Flight path angle at given rate of climb?
Flight path angle at given rate of climb calculator uses Flight Path Angle = asin(Rate of Climb/Velocity) to calculate the Flight Path Angle, The Flight path angle at given rate of climb is given by the inverse sine of the rate of climb and velocity of the aircraft. Flight Path Angle is denoted by γ symbol.
How to calculate Flight path angle at given rate of climb using this online calculator? To use this online calculator for Flight path angle at given rate of climb, enter Rate of Climb (RC) & Velocity (v) and hit the calculate button. Here is how the Flight path angle at given rate of climb calculation can be explained with given input values -> 0.06199 = asin(3.71976/60).