Rate of Climb evaluator uses Rate of Climb = Velocity*sin(Flight Path Angle) to evaluate the Rate of Climb, The Rate of Climb is the vertical speed at which an aircraft ascends. This formula calculates the rate of climb based on the aircraft's velocity and the sine of the flight path angle during the climb. Understanding and applying this formula is essential for pilots and engineers to optimize ascent performance, ensuring efficient and safe climb operations. Rate of Climb is denoted by RC symbol.
How to evaluate Rate of Climb using this online evaluator? To use this online evaluator for Rate of Climb, enter Velocity (v) & Flight Path Angle (γ) and hit the calculate button.