The coefficient of lift (CL) is a dimensionless value that represents the lift generated by an aerodynamic object, such as an airfoil, wing, or any other lifting surface, relative to the properties of the object and the flow conditions. It is a fundamental concept in aerodynamics and plays a crucial role in the design and analysis of aircraft and other flying objects.
- CL: Coefficient of lift
- W: Weight of the aircraft.
- ρ∞ Freestream density
- V∞: Freestream velocity
- S: Reference area