How to Calculate Rolling moment coefficient?
Rolling moment coefficient calculator uses Rolling moment coefficient = Rolling moment/(Dynamic Pressure*Reference Area*Characteristic length) to calculate the Rolling moment coefficient, The Rolling moment coefficient for an aircraft is the function of the rolling moment, dynamic pressure, reference area, and characteristic length. Rolling moment coefficient is denoted by C𝒍 symbol.
How to calculate Rolling moment coefficient using this online calculator? To use this online calculator for Rolling moment coefficient, enter Rolling moment (𝑳), Dynamic Pressure (q), Reference Area (S) & Characteristic length (𝓁) and hit the calculate button. Here is how the Rolling moment coefficient calculation can be explained with given input values -> 0.016404 = 0.5/(10*5.08*0.6).