How to Calculate Lift Coefficient for given Turn Radius?
Lift Coefficient for given Turn Radius calculator uses Lift Coefficient = Aircraft weight/(0.5*Freestream density*Reference Area*[g]*Turn Radius) to calculate the Lift Coefficient, The Lift Coefficient for given turn radius of an aircraft is a function of the altitude and weight of the aircraft. Lift Coefficient is denoted by CL symbol.
How to calculate Lift Coefficient for given Turn Radius using this online calculator? To use this online calculator for Lift Coefficient for given Turn Radius, enter Aircraft weight (W), Freestream density (ฯโ), Reference Area (S) & Turn Radius (R) and hit the calculate button. Here is how the Lift Coefficient for given Turn Radius calculation can be explained with given input values -> 0.001966 = Weight_of_aircraft_/(0.5*1.225*5.08*[g]*300).