How to Calculate Power required for given aerodynamic coefficients?
Power required for given aerodynamic coefficients calculator uses Power=Weight*Freestream Velocity*Drag Coefficient/lift coefficient to calculate the Power, The Power required for given aerodynamic coefficients in a steady, level flight is a function of the weight and freestream velocity of the aircraft. Power and is denoted by P symbol.
How to calculate Power required for given aerodynamic coefficients using this online calculator? To use this online calculator for Power required for given aerodynamic coefficients, enter Weight (W), Freestream Velocity (V_{∞}), Drag Coefficient (C_{D}) and lift coefficient (C_{L}) and hit the calculate button. Here is how the Power required for given aerodynamic coefficients calculation can be explained with given input values -> 100000 = 100*100*100/10.