Lift Formula For Aircraft. We have seen that lift changes linearly with area, density, camber, and small angles, and as the. Lift calculation and formula the lift equation.

The lift equation states that lift l is equal to the lift coefficient cl times the density rho ( ρ ) times half of the velocity v squared times the wing area a. The principles of flight are the aerodynamics dealing with the motion of air and forces acting on an aircraft.