Lift for Rotating Wings Calculator

The Lift for Rotating Wings accounts for the lift generated by a rotating wing or rotor, such as those used in helicopters

• $L$ is the lift force,
• $\rho$ is the air density,
• $A$ is the disc area,
• $\Omega$ is the angular velocity of the rotor,
• $r$ is the radius from the center of rotation to the location where lift is being measured,
• $V$ is the velocity of the air at the location of the rotor.