How to Calculate Lift Coefficient for given turn rate?
Lift Coefficient for given turn rate calculator uses Lift Coefficient = 2*Aircraft weight*(Turn Rate^2)/(([g]^2)*Freestream density*Load factor*Reference Area) to calculate the Lift Coefficient, The Lift Coefficient for given turn rate of an aircraft depends on its weight, altitude, and load factor. Lift Coefficient is denoted by CL symbol.
How to calculate Lift Coefficient for given turn rate using this online calculator? To use this online calculator for Lift Coefficient for given turn rate, enter Aircraft weight (W), Turn Rate (ฯ), Freestream density (ฯโ), Load factor (n) & Reference Area (S) and hit the calculate button. Here is how the Lift Coefficient for given turn rate calculation can be explained with given input values -> 0.013743 = 2*1800*(0.0198967534727316^2)/(([g]^2)*1.225*1.2*5.08).