What is a wingover?
A wingover is a manoeuvre that provides a fast, 180-degree turn with a minimal turn radius. It consists of a quarter loop into a vertical climb, letting the speed fall as altitude increases, and then a flat-turn over the top, diving to complete a quarter loop at the original altitude, but going in the opposite direction.
How to Calculate Radius of turn for given lift coefficient?
Radius of turn for given lift coefficient calculator uses Turn Radius = 2*Aircraft weight/(Freestream density*Reference Area*[g]*Lift Coefficient) to calculate the Turn Radius, The Radius of turn for given lift coefficient of an aircraft is a function of the aircraft's weight and altitude. Turn Radius is denoted by R symbol.
How to calculate Radius of turn for given lift coefficient using this online calculator? To use this online calculator for Radius of turn for given lift coefficient, enter Aircraft weight (W), Freestream density (ฯโ), Reference Area (S) & Lift Coefficient (CL) and hit the calculate button. Here is how the Radius of turn for given lift coefficient calculation can be explained with given input values -> 294.9525 = 2*Weight_of_aircraft_/(1.225*5.08*[g]*0.002).