How to Calculate Velocity of aircraft at given rate of climb?
Velocity of aircraft at given rate of climb calculator uses Velocity = Rate of Climb/sin(Flight Path Angle) to calculate the Velocity, The Velocity of aircraft at given rate of climb is typically determined by the balance between thrust and drag forces, as well as the aircraft's weight and the angle of climb, this equation suggests that the required velocity for the rate of climb is inversely proportional to the sine of the flight path angle. Velocity is denoted by v symbol.
How to calculate Velocity of aircraft at given rate of climb using this online calculator? To use this online calculator for Velocity of aircraft at given rate of climb, enter Rate of Climb (RC) & Flight Path Angle (γ) and hit the calculate button. Here is how the Velocity of aircraft at given rate of climb calculation can be explained with given input values -> 59.99004 = 3.71976/sin(0.062).