How to Calculate Radius of turn for a given lift coefficient?
Radius of turn for a given lift coefficient calculator uses Turn Radius=2*Weight/(Freestream density*Reference Area*[g]*lift coefficient) to calculate the Turn Radius, The Radius of turn for a given lift coefficient of an aircraft is a function of the aircraft's weight and altitude. Turn Radius and is denoted by R symbol.
How to calculate Radius of turn for a given lift coefficient using this online calculator? To use this online calculator for Radius of turn for a given lift coefficient, enter Weight (W), Freestream density (ρ_{∞}), Reference Area (S) and lift coefficient (C_{L}) and hit the calculate button. Here is how the Radius of turn for a given lift coefficient calculation can be explained with given input values -> 0.332969 = 2*100/(1.225*5*[g]*10).