How to Calculate Lift Coefficient for a given turn rate?
Lift Coefficient for a given turn rate calculator uses lift coefficient=2*Weight*(Turn Rate^2)/(([g]^2)*Freestream density*Load factor*Reference Area) to calculate the lift coefficient, The Lift Coefficient for a given turn rate of an aircraft depends on its weight, altitude and load factor. lift coefficient and is denoted by C_{L} symbol.
How to calculate Lift Coefficient for a given turn rate using this online calculator? To use this online calculator for Lift Coefficient for a given turn rate, enter Weight (W), Turn Rate (ω), Freestream density (ρ_{∞}), Load factor (n) and Reference Area (S) and hit the calculate button. Here is how the Lift Coefficient for a given turn rate calculation can be explained with given input values -> 0.000776 = 2*100*(0.05235987755982^2)/(([g]^2)*1.225*1.2*5).