How to Calculate Average Blade Lift Coefficient?
Average Blade Lift Coefficient calculator uses Blade Lift Coefficient = 6*Thrust Coefficient/Rotor Solidity to calculate the Blade Lift Coefficient, The Average Blade Lift Coefficient formula is the mean lift coefficient of blades and is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body. Blade Lift Coefficient is denoted by Cl symbol.
How to calculate Average Blade Lift Coefficient using this online calculator? To use this online calculator for Average Blade Lift Coefficient, enter Thrust Coefficient (CT) & Rotor Solidity (σ) and hit the calculate button. Here is how the Average Blade Lift Coefficient calculation can be explained with given input values -> 4 = 6*0.04/Solodity_of_rotor_helicopter.