Lift is the aerodynamic force generated by an airfoil or an aircraft wing as a result of the flow of air over its surface. It counteracts gravity, providing the means for an aircraft to overcome its weight and attain sustained flight. Acting perpendicular to the relative airflow, the lift force is pivotal in keeping the aircraft aloft and managing its altitude. Generally, a rise in dynamic pressure leads to a corresponding increase in lift force, assuming factors such as the lift coefficient remain unchanged. The formula to calculate lift as follows:
Where:
- CL is the coefficient of Lift,
- q is the Dynamic pressure in Pa.