How to Calculate Maximum Lift coefficient for given stall velocity?
Maximum Lift coefficient for given stall velocity calculator uses Maximum Lift Coefficient=2*Weight/(Freestream density*Reference Area*(Stall Velocity^2)) to calculate the Maximum Lift Coefficient, The Maximum Lift coefficient for given stall velocity of an aircraft depends upon the instantaneous weight and altitude of the aircraft. Maximum Lift Coefficient and is denoted by C_{L,max} symbol.
How to calculate Maximum Lift coefficient for given stall velocity using this online calculator? To use this online calculator for Maximum Lift coefficient for given stall velocity, enter Weight (W), Freestream density (ρ_{∞}), Reference Area (S) and Stall Velocity (V_{stall}) and hit the calculate button. Here is how the Maximum Lift coefficient for given stall velocity calculation can be explained with given input values -> 0.003265 = 2*100/(1.225*5*(100^2)).