How to Calculate Lift in Accelerated Flight?
Lift in Accelerated Flight calculator uses Lift Force = Mass of Aircraft*[g]*cos(Flight Path Angle)+Mass of Aircraft*Velocity^2/Radius of Curvature-Thrust*sin(Thrust Angle) to calculate the Lift Force, The Lift in Accelerated Flight is a function of the weight of aircraft, flight velocity, the thrust of aircraft, thrust angle, flight path angle, and radius of curvature of the curved path. Lift Force is denoted by FL symbol.
How to calculate Lift in Accelerated Flight using this online calculator? To use this online calculator for Lift in Accelerated Flight, enter Mass of Aircraft (m), Flight Path Angle (γ), Velocity (v), Radius of Curvature (Rcurvature), Thrust (T) & Thrust Angle (σT) and hit the calculate button. Here is how the Lift in Accelerated Flight calculation can be explained with given input values -> 4971.961 = 20*[g]*cos(0.062)+20*60^2/radius_of_curvature_eom-700*sin(0.034).