Lift equation calculator

The lift equation in aerodynamics relates the lift force $L$ generated by an object to various factors such as its shape, size, air density, velocity, and the angle of attack. The basic form of the lift equation is:

Where:

• $L$ is the lift force,
• CL​ is the lift coefficient (depends on the object’s shape and angle of attack),
• $\rho$ is the air density,
• $A$ is the reference area (typically the wing area for aircraft),
• $V$ is the velocity of the object relative to the air.