How to Calculate Lift in an accelerated flight?
Lift in an accelerated flight calculator uses Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle)) to calculate the Lift force, The Lift in an 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 and is denoted by L symbol.
How to calculate Lift in an accelerated flight using this online calculator? To use this online calculator for Lift in an accelerated flight, enter Mass (m), Flight path angle (θ), Velocity (v), Radius of Curvature (r), Thrust force (Ft) and Thrust angle (α_{T}) and hit the calculate button. Here is how the Lift in an accelerated flight calculation can be explained with given input values -> 8855.083 = (35.45*[g]*cos(2.00535228295826))+(35.45*(60^2)/15)-(10*sin(2.00535228295826)).