What is the result of lift and centrifugal forces acting on the rotor blades?

The phenomenon of coning occurs when the rotor blades of a helicopter are subjected to lift and centrifugal forces. As the rotor blades spin, the lift generated causes them to rise, while the centrifugal force pulls them outward away from the rotor hub. When these two forces are combined, they create an upward angle of the blades at their tips, resulting in a conical shape; this is referred to as coning.

Coning is a normal and expected behavior in rotor dynamics, indicative of the inherent stresses and forces at play during flight. It is essential for maintaining the stability and efficiency of rotorcraft operations. Understanding coning is crucial for pilots and engineers when analyzing rotor performance and ensuring safe flight operations. Recognizing this phenomenon helps in addressing the dynamics of rotor systems and contributes to the overall understanding of helicopter aerodynamics.