Lift Force Calculator

Calculate aerodynamic lift using the lift equation.

Lift Force Calculator: Aerodynamics

Calculate the aerodynamic lift generated by a wing or airfoil. Essential for aerospace and fluid dynamics.

How Planes Fly

Lift is the force that opposes the weight of an object in a fluid (like air). It is generated by the pressure difference between the top and bottom of a wing.

Lift Equation

L = 0.5 * ρ * v² * A * Cl

Where ρ is air density, v is velocity, A is wing area, and Cl is the coefficient of lift.

Frequently Asked Questions