How to Calculate Roll Control Power?
Roll Control Power calculator uses Roll Control Power = (2*Derivative of Wing Lift Coefficient*Flap Effectiveness Parameter)/(Wing Area*Wingspan)*int(Chord*x,x,Initial Length,Final Length) to calculate the Roll Control Power, The Roll control power formula is defined as a function of the aircraft's configuration and airspeed. Roll Control Power is denoted by Clδα symbol.
How to calculate Roll Control Power using this online calculator? To use this online calculator for Roll Control Power, enter Derivative of Wing Lift Coefficient (Clαw), Flap Effectiveness Parameter (τ), Wing Area (S), Wingspan (b), Chord (c), Initial Length (y1) & Final Length (y2) and hit the calculate button. Here is how the Roll Control Power calculation can be explained with given input values -> 0.015634 = (2*0.23*0.66)/(17*200)*int(2.1*x,x,1.5,12).