How to Calculate Turn rate for a given lift coefficient?
Turn rate for a given lift coefficient calculator uses Turn Rate=[g]*(sqrt((Reference Area*Freestream density*lift coefficient*Load factor)/(2*Weight))) to calculate the Turn Rate, The Turn rate for a given lift coefficient of an aircraft depends upon the altitude, load factor and weight of the aircraft. Turn Rate and is denoted by ω symbol.
How to calculate Turn rate for a given lift coefficient using this online calculator? To use this online calculator for Turn rate for a given lift coefficient, enter Reference Area (S), Freestream density (ρ_{∞}), lift coefficient (C_{L}), Load factor (n) and Weight (W) and hit the calculate button. Here is how the Turn rate for a given lift coefficient calculation can be explained with given input values -> 340.6214 = [g]*(sqrt((5*1.225*10*1.2)/(2*100))).